Eximkey - India Export Import Policy 2004 2013 Exim Policy
DGFT

APPENDIX-3

Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) export of which is regulated

Export of Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) listed below shall be permitted only against an export licence issued in this behalf unless export is prohibited or is permitted without licence subject to fulfillment of conditions, if any, as indicated under/against any specific category or item.

Provisions of Chapter IV A of the FT(D&R) Act,1992 as amended in 2010 shall apply to the goods, services and technologies specified in the list below.

Supply of SCOMET Items from DTA to SEZ

No export permission is required for supply of SCOMET items from DTA to SEZ. However, all supplies of SCOMET items from DTA to SEZ will be reported to the Development Commissioner of the respective SEZ by the supplier in the prescribed proforma (Annexure 1) within one (1) week of the supplies getting effected. An annual report of such supplies from DTA to SEZ shall be sent to SCOMET Cell, DGFT (Hqrs), Department of Commerce, Udyog Bhawan, Maulana Azad Road, New Delhi-110011, by the Development Commissioner (DC), SEZ in the prescribed proforma (Annexure 2) . Report by the DC, SEZ to be filed by 15th May of every financial year for the supplies effected during the preceding financial year.

Export of SCOMET Items from SEZ to outside the country

Export permission is required if the SCOMET items are to be physically exported outside the country from SEZ i.e. to another country (Refer Rule 26 of the SEZ Rules, 2006).

It is mandatory for all companies and their subsidiaries registered in India and all other business entities operating in India and involved in the manufacture, processing and use of Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) listed below to obtain permission of the Central Government before entering into any arrangement or understanding that involves an obligation to facilitate or undertake site visits, on-site verification or access to records/ documentation, by foreign Governments or foreign third parties, either acting directly or through an Indian party or parties. Requests for such permissions shall be considered in the manner in which requests for export/import licence are considered.

Provided that where obligations involving site visits, on-site verification or access to records/ documentation by foreign governments or foreign third parties are to be undertaken pursuant to a bilateral agreement or a multilateral treaty to which India is a party, the provisions of the relevant agreement or treaty shall apply.

Exporters are advised to refer to the relevant guidelines relating to the export of SCOMET items in the Handbook of Procedures (Vol.I), as issued from time to time.

Glossary: Expressions used in the SCOMET List have the following meanings:

“Accuracy” usually measured in terms of inaccuracy, means the maximum deviation, positive or negative, of an indicated value from an accepted standard or true value.

“Active flight control systems” are systems that function to prevent undesirable “aircraft” and missile motions or structural loads by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control.

“Aircraft”: A fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tilt-wing airborne vehicle.

“Angular position deviation” means the maximum difference between angular position and the actual, very accurately measured angular position after the work piece mount of the table has been turned out of its initial position.

“Composite” means a “matrix” and an additional phase or additional phases consisting of particles, whiskers, fibres or any combination thereof, present for a specific purpose or purposes.

“Composite theoretical performance” (“CTP”) is a measure of computational performance given in millions of theoretical operations per second (Mtops), calculated using the aggregation of computing elements (CE).

“Contouring control” means two or more “numerically controlled” motions operating in accordance with instructions that specify the next required position and the required feed rates to that position. These feed rates are varied in relation to each other so that a desired contour is generated.

“CTP” is equivalent to “composite theoretical performance

“Designed or modified” describes equipment, parts or components which, as a result of “development,” or modification, have become endowed with specified properties that make them fit for a particular application.

“Development”: Activity related to all phases prior to “production” such as design, design research, design analysis, design concepts, assembly and testing of prototypes, pilot production schemes, design data, process of transforming design data into a product, configuration design, integration design, layouts.

“Digital computer” means equipment which can, in the form of one or more discrete variables, perform all of the following:

a. Accept data;

b. Store data or instructions in fixed or alterable (writable) storage devices;

c. Process data by means of a stored sequence of instructions which is modifiable; and

d. Provide output of data.

N.B.: Modifications of a stored sequence of instructions include replacement of fixed storage devices, but not a physical change in wiring or interconnections.

“Explosives”: Solid, liquid or gaseous substances or mixtures of substances which, in their application as primary, booster, or main charges in warheads, demolition and other applications, are required to detonate.

“Fibrous or filamentary materials” include:

a. Continuous “monofilaments”;

b. Continuous “yarns” and “rovings”;

c. “Tapes”, fabrics, random mats and braids;

d. Chopped fibres, staple fibres and coherent fibre blankets;

e. Whiskers, either monocrystalline or polycrystalline, of any length;

f. Aromatic polyamide pulp.

“Hybrid computer” means equipment which can perform all of the following:

a. Accept data;

b. Process data, in both analogue and digital representations; and

c. Provide output of data.

“Image enhancement” means the processing of externally derived information-bearing images by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform). This does not include algorithms using only linear or rotational transformation of a single image, such as translation, feature extraction, registration or false coloration.

“Information security” is all the means and functions ensuring the accessibility, confidentiality or integrity of information or communications, excluding the means and functions intended to safeguard against malfunctions. This includes cryptography, ‘cryptanalysis’, protection against compromising emanations and computer security.

N.B.: ‘Cryptanalysis’: analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text.

“Insulation” is applied to the components of a rocket motor, i.e. the case, nozzle, inlets, case closures, and includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.

“Interior lining” is suited for the bond interface between the solid propellant and the case or insulating liner. Usually a liquid polymer based dispersion of refractory or insulating materials, e.g. carbon filled hydroxyl terminated polybutadiene (HTPB) or other polymer with added curing agents sprayed or screeded over a case interior.

“Isolated live cultures” includes live cultures in dormant form and in dried preparations.

“Isostatic presses” mean equipment capable of pressurising a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a workpiece or material.

“Laser”: An assembly of components which produce both spatially and temporally coherent light that is amplified by stimulated emission of radiation.

“Linearity” (usually measured in terms of non-linearity) means the maximum deviation of the actual characteristic (average of upscale and downscale readings), positive or negative, from a straight line so positioned as to equalise and minimise the maximum deviations.

“Matrix” means a substantially continuous phase that fills the space between particles, whiskers or fibres.

“Measurement uncertainty” is the characteristic parameter which specifies in what range around the output value the correct value of the measurable variable lies with a confidence level of 95 %. It includes the uncorrected systematic deviations, the uncorrected backlash and the random deviations.

“Microcircuit”: A device in which a number of passive and/or active elements are considered as indivisibly associated on or within a continuous structure to perform the function of a circuit.

“Microprogrammes”: A sequence of elementary instructions maintained in a special storage, the execution of which is initiated by the introduction of its reference instruction register.

“Missiles” means complete rocket systems and unmanned aerial vehicle systems.

“Modified” in the context of “software” describes “software” which has been intentionally changed such that it has properties that make it fit for specified purposes or applications. Its properties may also make it suitable for purposes or applications other than those for which it was “modified.”

“Monofilament” or filament is the smallest increment of fibre, usually several micrometres in diameter.

“Monolithic integrated circuit” means a combination of passive or active ‘circuit elements’ or both which:

a. Are formed by means of diffusion processes, implantation processes or deposition processes in or on a single semiconducting piece of material, a so-called ‘chip’;

b. Can be considered as indivisibly associated; and

c. Perform the function(s) of a circuit.

N.B.: ‘Circuit element’ is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

“Neural computer” means a computational device designed or modified to mimic the behaviour of a neuron or a collection of neurons, i.e., a computational device which is distinguished by its hardware capability to modulate the weights and numbers of the interconnections of a multiplicity of computational components based on previous data.

“Numerical control” means the automatic control of a process performed by a device that makes use of numeric data usually introduced as the operation is in progress.

“Optical integrated circuit” means a “monolithic integrated circuit” or a hybrid integrated circuit, containing one or more parts designed to function as a photo sensor or photo emitter or to perform (an) optical or (an) electro-optical function(s).

“Precursors”: Speciality chemicals used in the manufacture of explosives.

“Pressure transducers” are devices that convert pressure measurements into an electrical signal.

“Production” means all production stages (e.g., product engineering, manufacture, integration, assembly (mounting), inspection, testing, quality assurance);

“Production equipment”: Tooling, templates, jigs, mandrels, moulds, dies, fixtures, alignment mechanisms, test equipment, other machinery and components therefor, limited to those specially designed or modified for “development” or for one or more phases of “production”.

“Production facilities”: Equipment and specially designed “software” therefor integrated into installations for “development” or for one or more phases of “production”.

“Programmes”: A sequence of instructions to carry out a process in, or convertible into, a form executable by an electronic computer.

“Propellants”: Substances or mixtures that react chemically to produce large volumes of hot gases at controlled rates to perform mechanical work.

“Public domain” means a domain that has no restrictions upon dissemination of information within or from it; the existence of any legal rights to the intellectual property in that information does not remove the information from being in “public domain”.

“Radiation hardened”: Means that the component or equipment is designed or rated to withstand radiation levels which meet or exceed a total radiation dose of 5 x 103 Gy or 5 x 105 rads (Si).

“Required”: As applied to “technology”, refers to only that portion of “technology” which is peculiarly responsible for achieving or exceeding the controlled performance levels, characteristics or functions. Such “required” “technology” may be shared by different products.

“Resolution” means the least increment of a measuring device; or on digital instruments, the least significant bit.

“Roving” is a bundle (typically 12-120) of approximately parallel ‘strands’.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

“Settling time” means the time required for the output to come within one-half bit of the final value when switching between any two levels of the converter.

“Signal processing” means the processing of externally derived information-bearing signals by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform).

“Software”: A collection of one or more “programmes”, or “micro-programmes”, fixed in any tangible medium of expression. However, unless otherwise provided for against any item on the SCOMET List, the List does not control “software” which is either in the public domain or is generally available to the public by being :

a. Sold from stock at retail selling points without restriction, by means of:

1. Over-the-counter transactions;

2. Mail order transactions; or

3. Telephone call transactions; and

b. Designed for installation by the user without further substantial support by the supplier.

“Space qualified”: Products designed, manufactured and tested to meet the special electrical, mechanical or environmental requirements for use in the launch and deployment of satellites or high altitude flight systems operating at altitudes of 100 km or higher.

“Stability” means the standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable temperature conditions. This can be expressed as a function of time.

“Specially designed” qualifies the description of equipment, parts, components or “software” which, as a result of “development”, have unique properties that distinguish them for certain predetermined purposes. For example, a piece of equipment that is “specially designed” will only be considered so if it has no other function or use. Thus a piece of manufacturing equipment that is “specially designed” to produce a certain type of component will only be considered such if it is not capable of producing other types of components.

“Tape” is a material constructed of interlaced or unidirectional “monofilaments”, ‘strands’, “rovings”, “tows”, or “yarns”, etc., usually preimpregnated with resin.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

“Technology” means, except as otherwise provided for against any item in the SCOMET List, information (including information embodied in “software”) other than information in the “public domain”, that is capable of being used in:

a. the development, production or use of any goods or software;

b. the development of, or the carrying out of, an industrial or commercial activity or the provision of a service of any kind.

Explanation: When technology is described wholly or partly by reference to the uses to which it (or the goods to which it relates) may be put, it shall include services which are provided or used, or which are capable of being used, in the development, production or use of such technology or goods.

“Tow” is a bundle of “monofilaments”, usually approximately parallel.

“Toxins” means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of “microorganisms”.

“Unmanned Aerial Vehicle” (“UAV”) means any aircraft capable of initiating flight and sustaining controlled flight and navigation without any human presence on board.

“Usable in,” “usable for,” “usable as” or “capable of” qualifies the description of equipment, parts, components, materials, technology or “software” which are suitable for a particular purpose. There is no requirement that the equipment, parts, components, technology or “software” should have been configured, modified or specified for that particular purpose. (Contrast with “specially designed” – see above).

“Use” includes operation; installation (including on site installation); maintenance; repair; overhaul; refurbishing.

“Vaccine” is a medicinal product in a pharmaceutical formulation licensed by, or having marketing or clinical trial authorisation from, the regulatory authorities of either the country of manufacture or of use, which is intended to stimulate a protective immunological response in humans or animals in order to prevent disease in those to whom or to which it is administered.

“Yarn” is a bundle of twisted ‘strands’.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

Items on the SCOMET List are organized in the following categories.
 

Category 0 Nuclear materials, nuclear-related other materials, equipment and technology
Note: Export of these items is regulated under the Atomic Energy Act, 1962 and rules framed, and notifications/orders issued there under from time-to-time by the Department of Atomic Energy. The licensing authority for items in this category is the Department of Atomic Energy. An application for licence to export shall be made in writing to the Joint Secretary (I&M), Department of Atomic Energy, Anushakti Bhavan, CSM Marg, Mumbai 400 001
0A PRESCRIBED SUBSTANCES
Note: Any radioactive material in Category 0A shall additionally attract the provisions of Radiation Protection Rules, 2004 made under the Atomic Energy Act, 1962 and the provisions of Section-16 of the Atomic Energy Act, 1962.
0A1 Source Material
0A101 Uranium containing the mixture of isotopes occurring in nature.
0A102 Uranium depleted in the isotope 235.
0A103 Thorium.
0A104 Any of the materials specified above in 0A101, 0A102, or 0A103 in the form of metal, alloy, chemical compound, or concentrate.
0A105 Any other material containing one or more of the foregoing.

Note 1: Source material includes uranium and thorium ores or concentrates.

Note 2: Exports of following items, for the use only in non-nuclear activities, to a given recipient country, within a period of one calendar year, not exceeding the limits specified below, are not controlled:

a. Uranium (containing the mixture of isotopes in nature): 100 kilograms.
b. Depleted uranium (uranium depleted in the isotope 235 below that occurring in nature): 1000 kilograms.
c. Thorium: 1000 kilograms.

 
Note 3: 0A1 does not control following –

i. Uranium and thorium ores, mineral concentrates or other materials that contain less than 300 parts per million (ppm) of uranium or/and thorium;

ii. Alloys containing less than 5 % thorium;

iii. Ceramic products containing thorium, which have been manufactured for non-nuclear use.
0A2 Special Fissionable Material
0A201 Plutonium-239.
0A202 Uranium-233.
0A203 Uranium enriched in the isotopes 235 or 233.
0A204 Neptunium.
0A205 Any material containing one or more of the foregoing.
0A206 Such other fissionable material determined by the Central Government from time to time.

Technical note:

The term “uranium enriched in the isotopes 235 or 233” means uranium containing the isotopes 235 or 233 or both in an amount such that the abundance ratio of the sum of these isotopes to the isotope 238 is greater than the ratio of the isotope 235 to the isotope 238 occurring in nature.

Note:

1. The term “special fissionable material” does not include source material.

2. Any quantity of special fissionable material is prescribed substance.

3. 0A2 does not control -

a. Plutonium with an isotopic concentration of plutonium-238 exceeding 80%, and

b. Special fissionable material when used in gram quantities or less as a sensing component in instruments.
0A3 Other Materials

‘Other Materials’ means non-nuclear materials for reactors, nuclear related dualuse materials indicated below and such materials as determined by the Central Government from time to time.
0A301 Deuterium and heavy water

Deuterium, heavy water (deuterium oxide) and any other deuterium compound, in which the ratio of deuterium to hydrogen atoms exceeds 1:5000,

a. for use in a nuclear reactor in quantities exceeding 5 kilograms of deuterium atoms in one consignment or 25 kilograms of deuterium atoms, for any one recipient country within a period of one calendar year;

b. for use in a non-nuclear activity in quantities exceeding 200 kilograms of deuterium atoms, for any one recipient country within a period of one calendar year.
0A302 Nuclear grade graphite

Nuclear grade graphite having a purity level better than 5 parts per million (ppm) boron equivalent and with a density greater than 1.5 gram/cc -

a. for use in a nuclear reactor or any other nuclear activities in quantities exceeding 1 kilogram;

b. for use in non-nuclear activities in quantities exceeding 30 metric tons for any one recipient country within a period of one calendar year.

Note: The item 0A302 does not cover graphite powder.
0A303 Zirconium with hafnium content of less than 1 part to 500 parts of zirconium by weight (i.e. less than 2000 ppm) in the form of metal, alloys containing more than 50% zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.
0A304 Beryllium metal, its compounds, alloys containing more than 50% beryllium by weight, manufactures thereof, and waste or scrap of any of the foregoing and its minerals / concentrates including beryl but excluding:

a. beryllium windows used for x-ray machines or for bore-hole logging devices, and

b. beryl in the form of emerald, aquamarine or ‘cut & polished’ semiprecious stones for use in jewellery.
0A305 Lithium enriched in the Lithium-6 (6Li) isotope to greater than its natural isotopic abundance (i.e. more than 7.5%) and the products or devices containing enriched lithium such as elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.
0A306 Niobium and Tantalum, their metals, alloys and minerals including columbite and tantalite.
0A307 [Reserved]
0A308 Tritium, tritium compounds or mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, except when utilized in such quantities and for such purposes as for organic labelled compounds, Gas Filled Light Sources and as Tritiated Water for radiotracer studies.
0A309 Hafnium

Hafnium metal, alloys containing more than 60% hafnium by weight, hafnium compounds containing more than 60% hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.
0A310 Radium-226

Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing, except medical applicators and a product or device containing less than 0.37 GBq (10mCi) of Ra-226 in any form.
0A311 Boron

Boron enriched in the Boron-10 (10B) isotope to greater than its natural isotopic abundance as follows:

Elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
0A312 Helium-3

Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.

Note: A product or device containing less than 1gm of Helium-3 is excluded.
0A313 ‘Radionuclides’ appropriate for making neutron sources based on alpha-n reaction, in the following forms:
a. Elemental;
b. Compounds having a total activity of 37 GBq per kg or greater;
c. Mixtures having a total activity of 37 GBq per kg or greater;
d. Products or devices containing any of the foregoing.

Radionuclides controlled by this item include:

Actinium-225 Actinium-227 Californium-253
Curium-240 Curium-241 Curium-242
Curium-243 Curium244 Einsteinium-253
Einsteinium254 Gadolinium-148 Plutonium-236
Plutonium-238 Polonium-209 Polonium-210
Polonium-208 Radium-223 Thorium-228
Thorium-227 Uranium-230 Uranium-232

 
0B Prescribed Equipment
0B001 Nuclear Reactors; associated equipment, components, and systems especially designed, prepared, or adapted or used or intended to be used in such reactors including but not limited to:-

a. Complete nuclear reactors

b. Nuclear reactor vessels

c. Nuclear reactor fuel charging and discharging machines

d. Nuclear reactor control rods and equipment

e. Nuclear reactor pressure tubes

f. Nuclear fuel cladding: Zirconium metal tubes or zirconium alloy tubes (or assemblies of tubes), in which hafnium to zirconium ratio is 1:500 or less, for use as nuclear fuel cladding

g. Primary coolant pumps or circulators

h. Nuclear reactor internals

i. Heat exchangers (steam generators) for use in the primary or intermediate coolant circuit of a nuclear reactor

j. Neutron detectors

k. External thermal shields.
0B002 Plants for processing, production, concentration, conversion or recovery of Prescribed Substances (such as uranium, plutonium, thorium, deuterium, heavy water, tritium, lithium); associated equipment, components and systems especially designed, prepared or adapted or used or intended to be used in such plants including but not limited to:

a. Plants for production or concentration of deuterium, heavy water or deuterium compounds-

1. Water - Hydrogen Sulphide Exchange Towers with diameters of 1.5 m or greater and capable of operating at pressures greater than or equal to 2 MPa (300 psi), especially designed or prepared for heavy water production.

2. Especially designed or prepared blowers and compressors for hydrogen-sulphide gas circulation. These blowers or compressors have a throughput capacity greater than or equal to 56 m3/second (120,000 SCFM) while operating at pressures greater than or equal to 1.8 MPa (260 psi) suction and have seals designed for wet H2S service

3. Ammonia-Hydrogen Exchange Towers greater than or equal to 35 m in height with diameters of 1.5 m to 2.5 m capable of operating at pressures greater than 15 MPa especially designed or prepared for heavy water production

4. Tower Internals and Stage Pumps: Tower internals and stage pumps especially designed or prepared for heavy water production. Tower internals include especially designed stage contactors which promote intimate gas/liquid contact. Stage pumps include especially designed submersible pumps for circulation of liquid ammonia within a contacting stage internal to the stage towers.

5. Ammonia Crackers with operating pressures greater than or equal to 3 MPa especially designed or prepared for heavy water production.

6. Infrared Absorption Analyzers capable of ‘on-line’ hydrogen/deuterium ratio analysis

7. Catalytic Burners for conversion of enriched deuterium gas into heavy water

8. Complete heavy water upgrade systems or columns therefor

9. Ammonia synthesis converters or synthesis units for heavy water production utilizing the ammonia-hydrogen exchange process.

b. Plants for the conversion of uranium

1. Systems for the conversion of uranium ore concentrates to UO3;
2. Systems for the conversion of UO3 to UF6;
3. Systems for the conversion of UO3 to UO2;
4. Systems for the conversion of UO2 to UF4;
5. Systems for the conversion of UF4 to UF6;
6. Systems for the conversion of UF4 to uranium metal;
7. Systems for the conversion of UF6 to UO2;
8. Systems for the conversion of UF6 to UF4;
9. Systems for the conversion of UO2 to UCl4.

c. Plants for the conversion of plutonium
1. systems for the conversion of plutonium nitrate to oxide
2. systems for plutonium metal production

d. Tritium facilities or plants for the production, recovery, extraction, concentration or handling of tritium and equipment therefor including hydrogen or helium refrigeration units; and hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.

e. Lithium isotope separation facilities or plants, and systems and equipment therefor as follows -

1. Facilities or plants for the separation of lithium isotopes;

2. Equipment for the separation of lithium isotopes based on the lithiummercury amalgam process, as follows:

a) Packed liquid-liquid exchange columns especially designed for lithium amalgams;

b) Mercury or lithium amalgam pumps;

c) Lithium amalgam electrolysis cells;

d) Evaporators for concentrated lithium hydroxide solution;

3. Ion exchange systems especially designed for lithium isotope separation, and especially designed component parts therefor;

4. Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers) especially designed for lithium isotope separation, and especially designed component parts therefor.
 
0B003 Plants for reprocessing of irradiated nuclear fuel and equipment, components and systems especially designed, prepared or adapted or used or intended to be used in such plants, including but not limited to:

a. Irradiated fuel element chopping machines designed for remote operation

b. Dissolvers capable of withstanding hot and highly corrosive liquid for dissolution of irradiated nuclear fuel and which can be remotely loaded and maintained

c. Solvent extractors and solvent extraction equipment resistant to the corrosive effect of nitric acid

d. Chemical holding or storage vessels resistant to the corrosive effect of nitric acid

e. Neutron measurement systems for integration and use with automated process control systems for the reprocessing of irradiated fuel elements.

f. Industrial equipment including assemblies and components as follows:

1. High density (lead glass or other) radiation shielding windows

2. Radiation hardened TV cameras, or lenses therefor

3. ‘Robots’ or ‘end effectors’ especially designed for handling high explosives; and control units therefor

4. Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells
0B004 Plants for treatment, handling, storage and transportation of radioactive wastes from nuclear reactors or from plants for processing Source Materials or Special Fissionable Materials or from nuclear reprocessing plants; irradiated nuclear fuel; Special Fissionable Materials, and equipment especially designed, prepared, adapted, or intended to be used therefor.
0B005 All systems, associated equipment, components for separation or enrichment of isotopes of uranium, plutonium, lithium, boron or other elements, other than analytical instruments, especially designed, prepared, adapted, used or intended to be used therefor as follows:

a. Gas centrifuges and assemblies and components especially designed or prepared for use in gas Centrifuges

1. Gas centrifuges;

2. Complete rotor assemblies; Thin-walled cylinders, or a number of interconnected thin-walled cylinders, manufactured from one or more of the high strength-to-density ratio materials described in the Note-1 in 0B005.a. If interconnected, the cylinders are joined together by flexible bellows or rings as described in 0B005.a.4. The rotor is fitted with an internal baffle(s) and end caps, as described in 0B005.a.5 and 0B005.a.6.

3. Rotor tube cylinders: Especially designed or prepared thin-walled cylinders with thickness of 12 mm or less, a diameter of between 75 mm and 650 mm, and manufactured from one or more of ‘high strength-to-density ratio materials’ described in the Note-1 in 0B005.a;

4. Rings or bellows: Rings or bellows with wall thickness of 3 mm or less and a diameter of between 75 mm and 650 mm especially designed to give local support to a rotor tube or to join together a number of rotor tubes, made from ‘high strength-to-density ratio materials’ described in the Note-1 in 0B005.a.

5. Baffles: Disc-shaped components of between 75 mm and 650 mm diameter especially designed or prepared for mounting inside a rotor tube, in order to isolate the take-off chamber from the main separation chamber and manufactured from ‘high strength-to-density ratio materials’ described in the Note-1 in 0B005.a.

6. Top or bottom caps: Especially designed or prepared disc-shaped components of between 75 mm and 400 mm diameter especially designed or prepared to fit the ends of a rotor tube, and so contain the UF6 within the rotor tube, and in some cases to support, retain or contain as an integrated part an element of the upper bearing (top cap) or to carry the rotating elements of the motor and lower bearing (bottom cap), and manufactured from ‘high strength-to-density ratio materials’ described in the Note-1 in 0B005.a;

7. Especially prepared Magnetic Suspension Bearings with both of the following attributes:

a. Bearing assemblies consisting of an annular magnet suspended within a housing made of or protected by “materials resistant to corrosion by UF6” (see Note 3 of 0B005) containing a damping medium and having the magnet coupling with a pole piece or second magnet fitted to the top cap of the rotor;

b. Active magnetic bearings especially designed or prepared for use with gas centrifuges. These bearings usually have the following characteristics: i) Designed to keep centred a rotor spinning at 600 Hz or more; and ii) Associated to a reliable electrical power supply and/or to an uninterruptible power supply (UPS) unit in order to function for more than one hour.

8. Bearings / Dampers: Especially designed or prepared bearings comprising a pivot/cup assembly mounted on a damper. The pivot is normally a hardened steel shaft with a hemisphere at one end with a means of attachment to the bottom cap described in 0B005.a.6 at the other. The shaft may however have a hydrodynamic bearing attached. The cup is pellet-shaped with a hemispherical indentation in one surface. These components are often supplied separately to the damper.

9. Molecular pumps: Molecular pumps are high vacuum pumps consisting of especially designed or prepared cylinders having internally machined or extruded helical grooves and internally machined bores. Typical dimensions are as follows: 75 mm to 650 mm internal diameter, 10 mm or more wall thickness, with the length equal to or greater than the diameter. The grooves are typically rectangular in cross-section and 2 mm or more in depth.

10. Ring-shaped motor stators: Especially designed or prepared ring-shaped stators for high speed multiphase AC hysteresis (or reluctance) motors for synchronous operation within a vacuum at a frequency of 600 Hz or greater and a power of 40 VA or greater. The stators may consist of multi-phase windings on a laminated low loss iron core comprised of thin layers typically 2.0 mm thick or less.

11. Centrifuge housing/recipients to contain the rotor tube assembly of a gas centrifuge consisting of rigid cylinder of wall thickness up to 30 mm with precision machined ends that are parallel to each other and perpendicular to the cylinder's longitudinal axis to within 0,05 degrees or less.

12. Scoops consisting of tubes for the extraction of UF6 gas from within the rotor tube by a Pitot tube action and capable of being fixed to the central gas extraction system.

Note 1: The high strength-to-density ratio materials used for centrifuge rotating components include the following:

(a) Maraging steel capable of an ultimate tensile strength of 1.95 GPa or more;

(b) Aluminium alloys capable of an ultimate tensile strength of 0.46 GPa or more;

(c) Filamentary materials suitable for use in composite structures and having a specific modulus of 3.18 X 106 m or greater and a specific ultimate tensile strength of 7.62 X 104 m or greater.

Note 2: 'Specific Modulus' is the Young's Modulus in N/m2 divided by the specific weight in N/m3; 'Specific Ultimate Tensile Strength' is the ultimate tensile strength in N/m2 divided by the specific weight in N/ m3.

b. Especially designed or prepared auxiliary systems, equipment and components for gas centrifuge enrichment plants

1. Machine header piping systems for handling UF6 within the centrifuge cascades;

2. Frequency changers (converters or inverters) especially designed or prepared to supply motor stators for gas centrifuge enrichment, having all of the following characteristics, and especially designed components therefor:

a. A multiphase frequency output of 600 Hz or greater; and

b. High stability (with frequency control better than 0.2 %).

c. Especially designed or prepared assemblies and components for use in gaseous diffusion enrichment

1. Gaseous diffusion barriers and barrier materials resistant to corrosion by UF6 described in the Note-3 in 0B005;

2. Gaseous diffuser housings made of or protected by materials resistant to corrosion by UF6 described in the Note-3 in 0B005;

3. Compressors (positive displacement, centrifugal and axial flow types) or gas blowers with a suction volume capacity of 1 m3 /min or more of UF6, discharge pressure up to 500 kPa and having a pressure ratio of 10:1 or less designed for long term operation in the UF6 environment and made of or protected by materials resistant to corrosion by UF6 described in the Note-3 in 0B005.

d. Especially designed or prepared auxiliary systems, equipment and components for use in gaseous diffusion enrichment:

Piping systems and header systems for handling UF6 within the gaseous diffusion cascades.

e. Especially designed or prepared systems, equipment and components for use in aerodynamic enrichment plants:

1. Especially designed or prepared separation nozzles and assemblies thereof. The separation nozzles consist of slit-shaped, curved channels having a radius of curvature less than 1 mm, made of materials resistant to corrosion by UF6 described in the Note-3 in 0B005 and having a knife-edge within the nozzle that separates the gas flowing through the nozzle into two fractions;

2. Especially designed or prepared vortex tubes and assemblies thereof. The vortex tubes are cylindrical or tapered, made of or protected by materials resistant to corrosion by UF6 described in the Note-3 in 0B005 and with one or more tangential inlets. The tubes may be equipped with nozzle type appendages at either or both ends;

3. Especially designed or prepared compressors or gas-blowers made of or protected by materials resistant to corrosion by the UF6 (see the Note-3 in 0B005) / carrier gas (hydrogen or helium) mixture;

4. Especially designed or prepared separation element housings made of or protected by materials resistant to corrosion by UF6 described in the Note-3 in 0B005, for containing vortex tubes or separation nozzles;

5. Especially designed or prepared header-piping systems, made of or protected by materials resistant to corrosion by UF6 described in the Note-3 in 0B005, for handling UF6 within the aerodynamic cascades;

6. UF6/carrier gas separation systems for separating UF6 from carrier gas (hydrogen or helium).

f. Especially designed or prepared systems, equipment and components for use in chemical exchange or ion exchange enrichment plants.

1. Countercurrent Liquid-liquid exchange columns (Chemical exchange), having mechanical power input, especially designed or prepared for uranium enrichment using the chemical exchange process. For corrosion resistance to concentrated hydrochloric acid solutions, these columns and their internals are normally made of or protected by materials resistant to corrosion by concentrated hydrochloric acid solutions. The stage residence time of the columns is normally designed to be 30 seconds or less.

2. Liquid-liquid centrifugal contactors (Chemical exchange), especially designed or prepared for uranium enrichment using the chemical exchange process. Such contractors are made of or protected by materials resistant to corrosion by concentrated hydrochloric acid solutions, The stage residence time of the columns is normally designed to be 30 seconds or less.

3. Uranium reduction systems and equipment (Chemical exchange):

a. Especially designed or prepared electrochemical reduction cells to reduce uranium from one valence state to another for uranium enrichment using the chemical exchange process. The cell materials in contact with process solutions must be corrosion resistant to concentrated hydrochloric acid solutions;

b. Especially designed or prepared systems consisting of solvent extraction equipment and pumps or other transfer devices at the product end of the cascade for taking the U+4 out of the organic stream.

4. Feed preparation systems (Chemical exchange) consisting of dissolution, solvent extraction and/or ion exchange equipment for producing high-purity uranium chloride.

5. Uranium oxidation systems (Chemical exchange) for oxidation of U+3 to U+4

6. Fast-reacting ion exchange resins/adsorbents (Ion exchange):

Fast-reacting ion-exchange resins or adsorbents, especially designed or prepared for uranium enrichment using the chemical exchange process, including porous macroreticular resins, and/or pellicular structures and other composite structures in any suitable form including particles or fibres chemically resistant to concentrated hydrochloric acid solutions.

7. Ion exchange columns (Ion exchange):

Cylindrical columns for containing and supporting packed beds of ion exchange resin/adsorbent and made of or protected by materials resistant to corrosion by concentrated hydrochloric acid solutions.

8. Ion exchange reflux systems (Ion exchange):

Chemical or electrochemical oxidation or reduction systems for regeneration of the chemical oxidizing or reducing agent(s) used in ion exchange enrichment cascades.

g. Especially designed or prepared systems, equipment and components for use in laser-based enrichment plants.

1. Uranium vaporization systems (atomic vapour based methods)

2. Liquid or vapour uranium metal handling systems and components (atomic vapour based methods)

3. Uranium metal ‘product’ and ‘tails’ collector assemblies (atomic vapour based methods)

4. Separator module housings (atomic vapour based methods)

5. Supersonic expansion nozzles (molecular based methods)

6. ‘Product’ or ‘tails’ collectors (molecular based methods)

7. UF6/carrier gas compressors (molecular based methods)

8. Rotary shaft seals (molecular based methods)

9. Fluorination systems (molecular based methods)

10. UF6/carrier gas separation systems (molecular based methods)

11. ‘Lasers’ or ‘laser systems or components’ for the separation of uranium isotopes.

h. Especially designed or prepared systems, equipment and components for use in plasma separation enrichment plants

1. Microwave power sources and antennae: Especially designed or prepared microwave power sources and antennae for producing or accelerating ions and having the following characteristics: greater than 30 GHz frequency and greater than 50 kW mean power output for ion production.

2. Radio frequency ion excitation coils for frequencies of more than 100 kHz

3. Uranium plasma generation systems

4. Uranium metal ‘product’ and ‘tails’ collector assemblies made of or protected by materials resistant to the heat and corrosion of uranium metal vapour.

5. Separator module housings (cylindrical vessels) for containing the uranium plasma source, radio-frequency drive coil and the ‘product’ and ‘tails’ collectors.

i. Especially designed or prepared systems, equipment and components for use in electromagnetic enrichment plants.

1. Electromagnetic isotope separators for separation of uranium isotopes and equipment and components therefor, including ion sources (consisting of a vapour source, ionizer, and beam accelerator), ion collectors (consisting of collector plates), vacuum housings and magnet pole pieces;

2. High voltage power supplies for ion sources: Especially designed or prepared high-voltage power supplies for ion sources, having all of the following characteristics: capable of continuous operation, output voltage of 20,000 V or greater, output current of 1 A or greater, and voltage regulation of better than 0.01% over a time period of 8 hours

3. High-power, direct current magnet power supplies: Especially designed or prepared high-power, direct current magnet power supplies having all of the following characteristics: capable of continuously producing a current output of 500 A or greater at a voltage of 100 V or greater and with a current or voltage regulation better than 0.01% over a period of 8 hours.

j. Especially designed or prepared other equipment and components for use in enrichment plants:

1. Feed systems / product and tails withdrawal systems such as feed autoclaves, ovens, or systems, desublimers, cold traps or pumps, solidification or liquefaction stations, ‘product’ or ‘tails’ stations used for handling UF6;

2. Special shut-off valves, control valves, bellow sealed valves, manual or automated, shut-off or control, made of or protected by materials resistant to corrosion by UF6;

3. UF6 mass spectrometers / ion sources capable of taking on-line samples from UF6 gas stream; ;

4. Rotary shaft seals for compressors or blowers;

5. Heat exchangers made of or protected by “materials resistant to corrosion by UF6”;

6. Vacuum systems including vacuum manifolds, vacuum headers and vacuum pumps made of, or protected by, materials resistant to corrosion by UF6.

Notes to 0B005:

1: Controls under 0B005 also apply to the plants and equipment that are intended for isotope separation of other elements.

2: “Other elements” means all elements other than hydrogen, uranium and plutonium.

3: Materials resistant to corrosion by UF6 include copper, copper alloys, stainless steel, aluminium, aluminium oxide, aluminium alloys, nickel or alloys containing 60% or more nickel and fluorinated hydrocarbon polymers.
0B006 Plants for the fabrication of nuclear reactor fuel elements, and equipment especially designed or prepared therefor including but not limited to:

a. fully automatic pellet inspection stations especially designed or prepared for checking final dimensions and surface defects of the fuel pellets;

b. automatic welding machines especially designed or prepared for welding end caps onto the fuel pins (or rods);

c. automatic test and inspection stations especially designed or prepared for checking the integrity of completed fuel pins (or rods);

d. systems especially designed or prepared to manufacture nuclear fuel cladding.

Item ‘c’ typically includes equipment for: 1) x-ray examination of pin (or rod) end cap welds, 2) helium leak detection from pressurized pins (or rods), and 3) gammaray scanning of the pins (or rods) to check for correct loading of the fuel pellets inside.
 
0B007 Plants or systems for production, handling, storage and transportation of Radioisotopes in quantities exceeding 100 Curies (3.7 X 1012 Becquerel).
0B008 Neutron generators including neutron chain reacting assemblies and fusion assemblies of all kinds for producing fissile materials.
0C Technology and software

Technology and software for the development, production or use of prescribed substances or prescribed equipment specified in 0A or 0B.
(Above SCOMET Category 0 and the entries has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- Category 0 Nuclear materials, nuclear-related other materials, equipment and technology
0A Prescribed Substances
0A1 Source Material
0A2 Special Fissionable Material
0A3 Other Materials
0B Prescribed Equipment
0C Technology]
Category 1 Toxic chemical agents and other chemicals
1A Prohibited chemicals
1B Chemicals permitted only to States party to the Chemical Weapons Convention
1C Chemicals permitted also to States not party to the Chemical Weapons Convention
Category 2 Micro-organisms, toxins
2A Bacteria
2B Fungi
2C Parasites
2D Viruses
2E Rickettsials
2F Toxins
2G Plant pathogens
2H Genetically Modified Organisms
Category 3 Materials, Materials Processing Equipment and related technologies
3A Materials
3A1 Special materials
3A2 Structural materials
3A3 Rocket propellants and constituent chemicals
3A4 High explosives
3A5 Stealth materials
3B Materials processing and production equipment, related technology and specially designed components and accessories therefor.
3C [Reserved]
3D Chemical and biomaterial manufacturing and handling equipment and facilities
Category 4 Nuclear-related other equipment and technology, not controlled under Category 0
4A Equipment, assemblies, components including test and production equipment
4B Equipment, assemblies, components including test and measurement equipment usable in development of nuclear explosive devices
4C Technology
Category 5 Aerospace systems, equipment, including production and test equipment, related technology and specially designed components and accessories therefor.
5A Rocket systems
5A1 Systems
5A2 Production and test equipment
5A3 Technology
5B Unmanned aerial vehicles
5C Avionics and navigation systems
5D Manned-aircraft, aero-engines, related equipment and components
5E Micro-light aircraft and powered ‘hang-gliders’
Category 6 [Reserved]
Category 7 Electronics, computers, and information technology including information security
7A Electronics
7B Electronic test equipment
7C Computers
7D Information technology including information security
7E [Reserved]
[OLD- Category 0 Nuclear materials, nuclear-related other materials, equipment and technology

Note: Export of these items is regulated under the Atomic Energy Act, 1962 and rules framed, and notifications/orders issued thereunder from time-to-time by the Department of Atomic Energy. The licensing authority for items in this category is the Department of Atomic Energy. An application for licences to export prescribed equipment or/an prescribed substances shall be made in writing to the Joint Secretary, Department of Atomic Energy, Anushakti Bhavan, CSM Marg, Mumbai 400 001.
0A Prescribed Substances

Note: Any radioactive material in Category 0A shall additionally attract the provisions of Radiation Protection Rules, 2004 made under the Atomic Energy Act, 1962 and the provisions of Section-16 of the Atomic Energy Act, 1962.
0A1 Source Material
0A101 Uranium containing the mixture of isotopes occurring in nature.
0A102 Uranium depleted in the isotope 235.
0A103 Thorium.
0A104 Any of the foregoing in the form of metal, alloy, chemical compound, or concentrate or any substance.
0A105 Any other material containing one or more of the foregoing.
Prescribed quantitative limits: as given below and in any period of 12 months:
a. Uranium (containing the mixture of isotopes in nature) exceeding 100 kilograms.
b. Depleted uranium (uranium depleted in the isotope 235 below that occurring in nature) exceeding 1000 kilograms.
c. Thorium exceeding 1000 kilograms.
0A2 Special Fissionable Material
0A201 Plutonium-239.
0A202 Uranium-233.
0A203 Uranium enriched in the isotopes 235 or 233.
0A204 Neptunium.
0A205 Any material containing one or more of the foregoing.
0A206 Such other fissionable material determined by the Central Government from time to time, but the term “special fissionable material” does not include source material.
Note: Any quantity of special fissionable material is prescribed substance.
0A3 Other Materials

‘Other Materials’ means non-nuclear materials for reactors, nuclear related dual-use materials indicated below and such materials as determined by the Central Government from time to time.
0A301 Deuterium, heavy water (deuterium oxide) and any other deuterium compound, in which the ratio of deuterium to hydrogen atoms exceeds 1:5000, in quantities exceeding 5 kilograms of deuterium in one consignment or 25 kilograms of deuterium in any period of 12 months.
0A302 Nuclear grade graphite / carbon, having a purity level better than 5 parts per million (ppm) boron equivalent and with a density greater than 1.5 gram/cc in quantities exceeding 30 metric tons in any period of 12 months.
0A303 Zirconium with hafnium content of less than 1 part to 500 parts of zirconium by weight (i.e. less than 2000 ppm) in the form of metal, its alloys, compounds, manufactures thereof, waste or scrap of any of the foregoing.
0A304 Beryllium, its compounds, alloys and its minerals / concentrates including Beryl but excluding:
a. beryllium windows used for x-ray machines and gamma ray detectors and
b. beryl in the form of emeralds or aquamarines.
0A305 Lithium enriched in the Lithium-6 (6Li) isotope to greater than its natural isotopic abundance (i.e. more than 7.5%) and the products or devices containing enriched lithium such as elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.
0A306 Niobium and Tantalum, their metals, alloys and minerals including columbite and tantalite.
0A307 Titanium alloys having both of the following characteristics:
a. ‘Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20 degrees C); and
b. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.
Technical note: The phrase ‘capable of’ encompasses titanium alloys before or after heat treatment.
0A308 Tritium, tritium compounds or mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, except when utilized in such quantities and for such purposes as for organic labelled compounds, Gas Filled Light Sources and as Tritiated Water for radiotracer studies.
0A309 Hafnium: (CAS 7440-58-6)

Hafnium metal, alloys containing more than 60% hafnium by weight, hafnium compounds containing more than 60% hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.
0A310 Radium-226:

Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing, except medical applicators and a product or device containing less than 0.37 GBq (10mCi) of Ra-226 in any form.
0A311 Boron (CAS 7740-42-8)

Boron enriched in the Boron-10 (10B) isotope to greater than its natural isotopic abundance as follows:
Elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
0A312 Helium-3
Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.
Note: A product or device containing less than 1gm of Helium-3 is excluded.
0A313 Alpha–emitting radionuclides:
Alpha–emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, in the following forms:
a. Elemental;
b. Compounds having a total alpha activity of 37 GBq per kg or greater;
c. Mixtures having a total alpha activity of 37 GBq per kg or greater;
d. Products or devices containing any of the foregoing.
 
Alpha emitters controlled by this item include:

Actinium-225 Actinium-227 Americium-242m
Californium-248 Californium-250 Californium-252
Californium-253 Californium-254 Curium-240
Curium-241 Curium-242 Curium-243
Curium244 Einsteinium-252 Einsteinium-253
Einsteinium254 Einsteinium-255 Fermium-257
Gadolinium-148 Mendelevium-258 Neptunium-235
Plutonium-236 Plutonium-237 Plutonium-238
Plutonium-241 Polonium-209 Polonium-210
Polonium-208 Radium-223 Thorium-228
Thorium-227 Uranium-230 Uranium-232
0B Prescribed Equipment
0B001 Nuclear Reactors; associated equipment, components, and systems specially designed, prepared, or adapted or used or intended to be used in such reactors:-

a. Complete nuclear reactors
b. Nuclear reactor vessels
c. Nuclear reactor fuel charging and discharging machines
d. Nuclear reactor control rods and equipment
e. Nuclear reactor pressure tubes
f. Zirconium tubes and assemblies of tubes in which hafnium to zirconium ratio is 1:500 or less
g. Primary coolant pumps
h. Nuclear reactor internals
i. Heat exchangers (steam generators) for use in the primary coolant circuit of a nuclear reactor
j. Neutron detection and measuring instruments for determining neutron flux levels within the core of a nuclear reactor.
0B002 Plants for processing, production, concentration, conversion or recovery of Prescribed Substances (such as uranium, plutonium, thorium, deuterium, heavy water, tritium, lithium); associated equipment, components and systems specially designed, prepared or adapted or used or intended to be used in such plants including but not limited to:

a. Plants for production or concentration of deuterium, heavy water-
1. Water - Hydrogen Sulphide Exchange Towers
2. Blowers and Compressors for hydrogen-sulphide gas circulation
3. Ammonia-Hydrogen Exchange Towers greater than or equal to 35 m in height with diameters of 1.5 m to 2.5 m
4. Tower Internals and Stage Pumps
5. Ammonia Crackers with operating pressures greater than or equal to 3 MPa
6. Infrared Absorption Analyzers capable of ‘on-line’ hydrogen/ deuterium ratio analysis
7. Catalytic Burners for conversion of enriched deuterium gas into heavy water
8. Complete heavy water upgrade systems or columns therefor
b. Plants for the conversion of uranium
c. Plants for the conversion of plutonium
d. Tritium facilities or plants, and equipment therefor
e. Lithium isotope separation facilities or plants, and equipment therefor
0B003 Plants for reprocessing of irradiated nuclear fuel and equipment, components and systems specially designed, prepared or adapted or used or intended to be used in such plants, including but not limited to:
a. Irradiated fuel element chopping machines designed for remote operation
b. Dissolvers capable of withstanding hot and highly corrosive liquid for dissolution of irradiated nuclear fuel and which can be remotely loaded and maintained
c. Solvent extractors and solvent extraction equipment resistant to the corrosive effect of nitric acid
d. Chemical holding or storage vessels resistant to the corrosive effect of nitric acid
e. Industrial equipment including assemblies and components as follows:
1. High density (lead glass or other) radiation shielding windows
2. Radiation hardened TV cameras, or lenses therefor
3. ‘Robots’ or ‘end effectors’ specially designed for handling high explosives; and control units therefor
4. Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells
0B004 Plants for treatment, handling, storage and transportation of radioactive wastes from nuclear reactors or from plants for processing Source Materials or Special Fissionable Materials or from nuclear reprocessing plants; irradiated nuclear fuel; Special Fissionable Materials, and equipment specially designed, prepared, adapted, or intended to be used therefor.
0B005 All systems, associated equipment, components for separation or enrichment of isotopes of uranium, plutonium, lithium or boron, other than analytical instruments, specially designed, prepared, adapted, used or intended to be used therefor as follows:
a. Gas centrifuges and assemblies and components specially designed or prepared for use in gas Centrifuges
b. Specially designed or prepared auxiliary systems, equipment and components for gas centrifuge enrichment plants
c. Specially designed or prepared assemblies and components for use in gaseous diffusion enrichment
d. Specially designed or prepared auxiliary systems, equipment and components for use in gaseous diffusion enrichment
e. Specially designed or prepared systems, equipment and components for use in aerodynamic enrichment plants
f. Specially designed or prepared systems, equipment and components for use in chemical exchange or ion exchange enrichment plants.
g. Specially designed or prepared systems, equipment and components for use in laser-based enrichment plants.
h. Specially designed or prepared systems, equipment and components for use in plasma separation enrichment plants.
i. Specially designed or prepared systems, equipment and components for use in electromagnetic enrichment plants.
0B006 Plants for the fabrication of nuclear reactor fuel elements, and equipment specially designed or prepared therefor including but not limited to:
a. fully automatic pellet inspection stations specially designed or prepared for checking final dimensions and surface defects of the fuel pellets;
b. automatic welding machines specially designed or prepared for welding end caps onto the fuel pins (or rods);
c. automatic test and inspection stations specially designed or prepared for checking the integrity of completed fuel pins (or rods).
Item ‘c’ typically includes equipment for: 1) x-ray examination of pin (or rod) end cap welds, 2) helium leak detection from pressurized pins (or rods), and 3) gamma-ray scanning of the pins (or rods) to check for correct loading of the fuel pellets inside.
0B007 Plants or systems for production, handling, storage and transportation of Radioisotopes in quantities exceeding 100 Curies (3.7 X 10 12 Becquerel).
0B008 Neutron generators including neutron chain reacting assemblies and fusion assemblies of all kinds for producing fissile materials
0C Technology
Technology and software for the development, production or use of prescribed substances or prescribed equipment specified in 0A or 0B.]
Category 1 Toxic chemical agents and other chemicals
1A Export of the following chemicals is prohibited:
(This corresponds to Schedule 1 to the Chemical Weapons Convention (CWC))

Note: Where reference is made below to groups of di-alkylated chemicals, followed by a list of alkyl groups in parentheses, all chemicals possible by all possible combinations and alkyl groups listed in parentheses are considered prohibited unless explicitly exempted.
(1).O-Alky ( e.g. Sarin: O-Isopropy1 methylphosphonofluoridate
Soman: O-Pinacolyl methylphosphonofluoridate

(2).O-Alkyl, ( e.g. Tabun: O-Ethyl N,N,-dimethyl phosphoramidocyanidate

(3).O-Alkyl (H or < C10, incl. cycloalkyl) S-2-Dialkyl (Me, Et, n-Pr or i-Pr)-aminoethyl alkyl (Me, Et, n-Pr or i-Pr) phosphonothiolates and corresponding alkylated or protonated salts
e.g. VX: O-Ethyl S-2 diisopropylaminoethyl methyl phosphonothiolate

(4).Sulphur mustards:
2-Chloroethylchloromethylsulphide
Mustard gas: Bis (2-chloroethyl) sulphide
Bis (2-chloroethylthio) methane
Sesquimustard:1,2-Bis (2-chloroethylthio) ethane
1,3-Bis (2-chloroethylthio)-n-propane
1,4-Bis (2-chloroethylthio)-n-butane
1,5-Bis (2-chloroethylthio)-n-Pentane
Bis (2-Chloroethylthiomethyl) ether
O-Mustard: Bis (2-Chloroethylthiomethyl) ether

(5).Lewisites:
Lewisite 1: 2-Chlorovinyldichloroarsine
Lewisite 2: Bis (2-Chlorovinyl) chloroarsine
Lewisite 3: Tris (2-Chlorovinyl) arsine

(6).Nitrogen mustards:
HN1: Bis (2-chloroethyl) ethylamine
HN2: Bis (2-chloroethyl) Chloroarsine
HN3: Tris (2-chloroethyl) amine

(7).Saxitoxin

(8).Ricin

(9).Alkyl (Me, Et, n-Pr or I-Pr) phosphonyldifluorides
e.g. DF: Methyl phosphonyldifluoride

(10).O-Alkyl (H or < C10, incl. cycloalkyl) O-2 dialkyl (Me, Et, n-Pr or i-Pr)-aminoethylalkyl (Me, Et N-Pr or i-Pr) phosphonites and corresponding alkylated or protonated salts
e.g.QL: O-Ethyl O-2-diisopropylaminoethyl methyl phosphonite

(11).Chlorosarin: O-Isopropyl methylphosphonochloridate

(12).Chlorosoman: O-Pinacolyl methylphosphonochloridate
1B Export of chemicals listed in 1B below is permitted only to States party to the Chemical Weapons Convention
(This corresponds to Schedule 2 to the Chemicals Weapons Convention)
Note to exporter:
(a) A list of States Parties can be obtained from the Disarmament & International Security Affairs Division of the Ministry of External Affairs (Room No. 40G, South Block, New Delhi) or at the official website of the Organization for the Prohibition of Chemical Weapons at www.opcw.org.
(b) A general permission valid for a period of two years may be applied for export of chemicals in this category. This permission shall be subject to the condition that for each export consignment, exporters shall, within 30 days of exports, notify the details to the National Authority, Chemical Weapons Convention, Cabinet Secretariat ; Ministry of External Affairs (D&ISA); Department of Chemicals and Petrochemicals and the Directorate General of Foreign Trade and submit to DGFT, a copy of Bill of Entry into the destination State Party within 30 days of delivery.
Note: Where reference is made below to groups of dialkylated chemicals, followed by a list of alkyl groups in parentheses, all chemicals possible by all possible combinations and alkyl groups listed in parentheses are included unless explicitly exempted.
1. Amiton 0,0-Diethyl S-[2-(diethylamino) ethyl)] phosphorothiolate and corresponding alkylated or protonated salts
2. PFIB: 1,1,3,3,3,-Pentafluoro-2-(trifluoromethyl)1-propene
3. BZ: 3-Quinuclidinyl benzilate
4. Chemicals, except for those listed in Schedule 1, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms,
e.g.Methylphosphonyl dichloride
Dimethyl methylphosphonate
Exemption:- Fonofos: O-Ethyl S-phenyl ethylphosphonothiolothionate
5. N, N-Dialkyl (ME, Et, n-Pr or i-Pr) phosphoramidic dihalides
6. Dialkyl (Me, Et, n-Pr or i-Pr) N, N-dialkyl (Me, Et, n-Pr or i-Pr)-phosphoramidates
7. Arsenic trichloride
8. 2,2-Diphenyl-2 hydroxyacetic acid
9. Quinuclidine-3-ol
10. N,H-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethyl-2 -chlorides and corresponding protonated salts
11. N, N-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethane-2-ols and corresponding protonated salts
Exemptions: N,N-Dimethylaminoethanol and corresponding protonated salts
N,N-Diethylaminoethanol and corresponding protonated salts
12. N, N-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethane-2-thiols and corresponding protonated salts
13. Thiodiglycol: Bis(2-hydroxyethyl) sulphide
14. Pinacolyl alcohol: 3,3-Dimethylbutane-2-ol
A List of commercially important Schedule-2 Chemicals of CWC is given below :

Sl. No. Name of Chemical Entry into Schedule CAS (Chemical Abstract Service) Numbers ITC(HS) codes
1. 2-Chloro N, N-Di-isopropyl ethylamine 2B10 4261-68-1 29211911
2. Diethyl amino Ethanethiol 2B12 100-38-9 29221910
3. O, O, Dimethyl Methyl Phosphonate 2B04 756-79-6 29209045
4. 2-Hydroxy N, N-Diisopropyl Ethylamine 2B11 96-80-0 29221111
5. N, N-Diethyl Amino ethyl Chloride Hydrochloride 2B10 869-24-9 29221112
6. Di-ethyl Amino ethanethiol Hydrochloride 2B12 1942-52-5 29221113
7. Di-Methyl Amino ethyl chloride Hydrochloride 2B10 4584-46-7 29221114
8. Di-Methyl Amino ethanethiol 2B12 108-02-1 29221115
9. Di-Methyl Amino ethanethiol Hydrochloride 2B12 13242-44-9 29221116
10. Phosphorothioic acid, S [2-(diethylamino) ethyl] O, O – diethyl ester 2A01 78-53-5 29201910
11. 1-Propene, 1,1, 3, 3, 3, - Pentafluoro – 2- (trifluoromethyl) (PFIB) 2A02 382-21-8 29033911
12. Benzeneacetic acid, alphahydroxy – alpha-phenyl, 1 – azabicyclo [2.2.2.] oct-3-yl ester 2A03 6581-06-2 29392050
13. Phosphonic Acid, Methyl-compound with (aminoimino methyl) urea (1: 1) 2B04 84402-58-4 29209047
14. 1-Propanaminium N, N, N-trimethyl – 3- [1-oxo-9 octadecenyl) amino]-. (Z)- methyl methylphosphonate 2B04 70055-71-9 29209048
15. Phosphonic acid, [methyl bis (5-ethyl-2-methyl-2-oxido-1, 3, 2- dioxaphosphorinan-5-yl) methyl] ester 2B04 42595-45-9 29209051
16. Phosphonic acid, [methyl-(5-ethyl-2-methyl 2-oxido-1,3,2-dioxaphosphorinan-5-yl) methyl] ester 2B04 41203-81-0 29209052
17. Phosphonic acid, propyl-dimethyl ester 2B04 18755-43-6 29209053
18. Phosphonous acid, methyl-diethyl ester 2B04 15715-41-0 29209054
19. Phosphonic acid, ethyl- 2B04 6779-09-5 29209055
20. Phosphonic acid, propyl- 2B04 4672-38-2 29209056
21. Phosphinic acid, methyl- 2B04 4206-94-4 29209057
22. Phosphonochloridic acid, methyl-, methyl ester 2B04 1066-52-0 29209058
23. Phosphonothioic dichloride, ethyl- 2B04 993-43-1 29209061
24. Phosphonic acid methyl- 2B04 993-13-5 29209062
25. Phosphonic acid, methyl-, dimethyl ester 2B04 756-79-6 29209063
26. Phosphonic dichloride, methyl- 2B04 676-97-1 29209064
27. Phosphonous dichloride, methyl- 2B04 676-83-5 29209065
28. Phosphonic acid, ethyl-, diethyl ester 2B04 78-38-6 29209066
29. Arsenous trichloride 2B07 7784-34-1 28121060
30. Benzeneacetic acid, alpha-hydroxy-alpha-phenyl 2B08 76-93-7 29181910
31. 1-Azabicyclo (2.2.2.) octan-3-ol 2B09 1619-34-7 29333930
32. Ethanamine, 2-Chloro-N, N-dimethyl- 2B10 107-99-3 29211914
33. Ethanol, 2-[bis(1-methylethyl ) amino ]- 2B11 96-80-0 29221920
34. Ethanethiol, 2-(diethylamino)- 2B12 100-38-9 29221930
35. Ethanol, 2, 2’-thiobis- 2B13 111-48-8 29309091
36. 2-Butanol, 3, 3-dimethyl- 2B14 464-07-3 29051910
1C Export of Chemicals as specified below is allowed to State Parties to the CWC without an export licence subject to the condition that the exporter shall notify within 30 days of export to the National Authority, Chemicals Weapons Convention, Cabinet Secretariat; the Ministry of External Affairs (D&ISA); the Department of Chemicals & Petro-chemicals, and the DGFT of such exports in the prescribed format (Aayat Niryat Form ) along with the End-Use Certificate and submit to the DGFT a copy of the bill of entry into the destination State Party within 30 days of delivery. Export of chemicals as specified below to states not party to the Chemical Weapons Convention shall continue to be restricted and will be allowed only against an export licence, and in that case also exporters shall submit to the DGFT a copy of the bill of entry into the destination country within 30 days of export.
Sl.No. Name of Chemical Entry into Schedule CAS Numbers ITC (HS) codes
1. Phosgene : ( Carbonyl dichloride) 3A01 75-44-5 28121010
2. Cyanogen chloride [(CN) C1] 3A02 506-77-4 28530091
3. Hydrocyanic acid 3A03 74-90-8 28111910
4. Chloropicrin:Trichloronitro-Methane 3A04 76-06-2 29049080
5. Phosphorus Oxychloride 3B05 10025-87-3 28121030
6. Phosphorus trichloride 3B06 7719-12-2 28121021
7. Phosphorous Pentachloride 3B07 10026-13-8 28121022
8. Trimethyl Phosphite 3B08 121-45-9 29209041
9. Triethyl Phosphite 3B09 122-52-1 29209042
10. Dimethyl Phosphite 3B10 868-85-9 29209043
11. Diethyl Phosphite 3B11 762-04-9 29209044
12. Sulphur monochloride 3B12 10025-67-9 28121042
13. Sulphur dichloride 3B13 10545-99-0 28121043
14. Thionyl Chloride 3B14 7719-09-7 28121047
15. Ethyldiethanolamine 3B15 139-87-7 29221211
16. Methyldiethanolamine 3B16 105-59-9 29221212
17. Triethanolamine 3B17 102-71-6 29221300
Category 2 Micro-organisms, toxins
2A Bacteria, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2A001 Bacillus anthracis
2A002 Bordetella bronchoseptica
2A003 Brucella abortus,
2A004 Brucella melitensis
2A005 Brucella suis
2A006 Chlamydia psittaci
2A007 Clostridium botulinum
2A008 Clostridium perfringes
2A009 Corynebacterium diphtheriae
2A010 Francisella tularensis
2A011 Klebsiella pneumoniae
2A012 Legionlla pneumophila
2A013 Leptospira interrogans - all serotypes reported in India
2A014 Mycobacterium bovis
2A015 Mycobacterium tuberculosis
2A016 Mycoplasma mycoides - var mycoides
2A017 Mycoplasma mycoides - var Capri
2A018 Neisseria meningitidis
2A019 Paseturella multicoda type B
2A020 Pseudomonas mallei
2A021 Pseudomonas pseudomallei
2A022 Salmonella paratyphi
2A023 Shigella dysenteriae
2A024 Staphylococcus aureus
2A025 Streptococcus pneumoniae
2A026 Vibrio cholerae elter
2A027 Vibrio Cholerae 0139
2A028 Yersinia pestis
2A029 Enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing serotypes
2A030 Mycoplasma capricolum subspecies capripneumoniae (‘strain F38’)
2A031 Salmonella typhi”
2B Fungi, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2B001 Blastomyces dermatitidis
2B002 Coccidiodes immitis
2B003 Histoplasma capulatum
2B004 Nocardia asteroides
2B005 Paracoccidioides braziliensis
2B006 Coccidiodes posadasii
2C Parasites, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2C001 Entamoeba histolytica
2C002 Babesia microti
2C003 Babesia divergens
2C004 Blostidium coli
2C005 Cryptosporidium spp.
2C006 Leishmania species
2C007 Naegleria australiensis
2C008 Naegleria fowleri
2C009 Plasmodium falciparum
2C010 Pneumocystis carinii
2C011 Schistosoma mansoni
2C012 Schistosoma japonicum
2C013 Schistosoma hemotobium
2C014 Toxoplasma gondii
2C015 Trichinella spiralis
2C016 Trypanosoma bruiei
2D Viruses, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2D001 African Horse Sickness virus
2D002 African Swine Fever virus
2D003 Avian influenza virus
2D004 Blue tongue virus
2D005 Camel pox virus
2D006 Chikungunya virus
2D007 Crimean-Congo hemorrhagic fever virus
2D008 Dengue virus
2D009 Eastern equine encephalitis virus
2D010 Ebola fever virus
2D011 Encephalomyocarditis virus (EMC)
2D012 Foot and Mouth Disease virus (all serotypes and subtypes)
2D013 Guanirito virus
2D014 Goatpox virus
2D015 Hantaan virus
2D016 Herpes virus simiae (monkey B virus)
2D017 Herpes ateles, Herpes saimiri
2D018 HIV- 1 & HIV-2 and other strains of SIV
2D019 Hog cholera virus
2D020 Human T-cell Leukemia virus
2D021 Junin virus
2D022 Japanese encephalitis virus
2D023 Kyasanur Forest Disease virus and Central European encephalitis viruses.
2D024 Korean hemorrhagic fever virus
2D025 Lymphocytic choriomeningitis virus (LCM)
2D026 Lassa virus
2D027 Marburg virus
2D028 Murrey valley encephalitis virus
2D029 Marchupo virus
2D030 Mason-pfizer monkey virus
2D031 Monkey pox virus
2D032 Newcastle disease virus
2D033 Omsk hemorrhagic fever virus
2D034 Peste des petits ruminant virus
2D035 Porcine enterovirus type I
2D036 Powassan virus
2D037 Rabies virus -all strains
2D038 Respiratory syncitial virus
2D039 Rift Valley Fever virus
2D040 Rinderpest virus
2D041 Sabia virus
2D042 Sheep pox (field strain)
2D043 Sin Nombre virus
2D044 Smallpox virus
2D045 St.Louis encephalitis virus
2D046 Swine Fever virus
2D047 Tick-borne encephalitis virus (Russian Spring Summer Encephalitis virus)
2D048 Teschen disease virus (Porcine entero virus type 1)
2D049 Variola virus
2D050 Venezuelan encephalitis virus
2D051 Vesicular stomatitis virus
2D052 Western encephalitis virus
2D053 Yellow fever virus, 17 D vaccine strain
2D054 Andes virus
2D055 Chapare virus
2D056 Choclo virus
2D057 Dobrava-Belgrade virus
2D058 Herpes virus (Aujeszky's disease)
2D059 Hendra virus (Equine morbillivirus)
2D060 Laguna Negra virus
2D061 Louping ill virus
2D062 Lujo virus
2D063 Lumpy skin disease virus
2D064 Lassa fever virus
2D065 Nipah virus
2D066 Oropouche virus
2D067 Porcine enterovirus type 9 (synonym: swine vesicular disease virus)
2D068 Rocio virus
2D069 Seoul virus
2E Rickettsials, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2E001 Coxiella burnetti
2E002 Rickettsiae rickettsii
2E003 Rickettsia quintana
2E004 Rickettsia prowazebi
2F Toxins
2F001 Abrins
2F002 Aflatoxins
2F003 Anatoxins
2F004 Botulinum toxin (s) (clostradium botulinum)
2F005 Bungarotoxins
2F006 Clostridium perfringens toxins
2F007 Corynebacterium diphtheriae toxins
2F008 Cyanginosins (Microcystins) (Microcystic aeuginosa)
2F009 Enterotoxin (Staphylococcus aureus)
2F010 Neurotoxin (Shigella dysenteriae)
2F011 Ricins
2F012 Shigatoxins
2F013 Saxitoxins
2F014 Trichothecene mycotoxins
2F015 Tetanus toxin (clostridium tetani)
2F016 Tetrodotoxin (Spheroides rufripes)
2F017 Verrucologen (M. verrucadia)
2F018 Cholera toxin
2F019 Conotoxin
2F020 Diacetoxyscirpenol toxin
2F021 HT-2 toxin
2F022 Modeccin toxin
2F023 T-2 toxin
2F024 Verotoxin and shiga-like ribosome inactivating proteins
2F025 Viscum Albut Lectin 1 (Viscumin)
2F026 Volkensin toxin
2G Plant pathogens
2G001 Bemisia tabaci
2G002 Colletotrichum coffeanum var. virulans
2G003 Clavicep purpurea
2G004 Dothistroma pini (Scirrhia pini)
2G005 Erwinia amylovora
2G006 Frankliniella occidentalis
2G007 Microcyclus ulei
2G008 Peronospora hyoscyami de Bary f.sp. tabacina (Adam) skalicky
2G009 Phytophthora infestans
2G010 Puccinia graminis
2G011 Puccinia erianthi
2G012 Puccinia striiformiis (Puccinia glumarum)
2G013 Pyricularia oryzae
2G014 Pseudomonas solanacearum
2G015 Peronospora hyscyami de Bary
2G016 Ralstonia solanacearum
2G017 Sugar cane Fiji disease virus
2G018 Sclerotinia sclerotiorum
2G019 Tilletia indica
2G020 Thrips palmi
2G021 Ustilago Maydis
2G022 Xanthomonas albilineans
2G023 Xanthomonas campestris pv citri
2G024 Xanthomonas campestris pv oryzae
2G025 Clavibacter michiganensis subsp. sepedonicus
2G026 Cochliobolus miyabeanus
2G027 Andean potato latent virus (Potato Andean latent tymovirus)
2G028 Potato spindle tuber viroid
2H Genetically Modified Organisms
2H001 Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity and are derived from organisms specified above in 2A, 2B, 2C, 2D, 2E and 2H.

Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences coding for any of the toxins specified above in 2F.
Category 3 Materials, Materials Processing Equipment and related technologies
3A Materials
3A1 Special Materials
3A101 Zirconium, beryllium, magnesium, and alloys of these in particle size less than 60 µm
3A102 Maraging steel in any form in which any linear dimension exceeds 75 mm, or in the form of sheet, plate or tubing with a wall or plate thickness equal or less than 5 mm.
3A103 Tungsten , molybdenum, and alloys of those metals in particulate form and a particle size of 50 x10-6 m (50 μm) or less;
(Above SCOMET 3A103 has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- 3A103 Tungsten (CAS 12070-12-1), molybdenum(CAS 1317-33-5), and alloys of those metals in the form of uniform spherical or atomized particles of size less than 500 µm]
3A104 Germanium
3A105 Gallium
3A106 Indium
3A107 Titanium-stabilised Duplex Stainless Steel (Ti-DSS)
(Above SCOMET 3A107 has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- 3A107 Titanium alloys including Titanium-stabilised Duplex Stainless Steel (Ti-DSS) (other than as specified at 0A307)]
3A108 Aluminium alloys in any form ‘capable of acquiring’ an ultimate tensile strength of 460 MPa or more at 293 K (20 degrees C)

Note: The phrase ‘capable of acquiring’ encompasses alloys before or after heat treatment
3A109 Bismuth having a purity of 99.99% or greater by weight and containing less than 10 parts per million by weight of silver
3A110 Calcium containing less than 1000 parts per million by weight of metallic impurities other than magnesium and containing less than 10 parts per million by weight of Boron
3A111 Chlorine trifluoride (ClF3)
3A112 Magnesium containing less than 200 parts per million by weight of metallic impurities other than calcium and containing less than 10 parts per million by weight of boron
3A113 (a) Tungsten, tungsten carbide, and alloys containing more than 90% tungsten by weight in forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm and a mass greater than 20 kg.

(b) Tungsten materials in the solid form usable for the fabrication of missile components in complete rocket systems of 5A and unmanned aerial vehicles of 5B, having all of the following:

1. Any of the following material compositions:

i. Tungsten and alloys containing 97% by weight or more of tungsten;

ii. Copper infiltrated tungsten containing 80% by weight or more of tungsten; or

iii. Silver infiltrated tungsten containing 80% by weight or more of tungsten; and

2. Able to be machined to any of the following products:

i. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

ii. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

iii. Blocks having a size of 120 mm x 120 mm x 50 mm or greater.
3A114 a. Nickel powder of purity 99.0% or greater by weight; and having a mean particle size of less than 10 μm measured by the ASTM B 330 standard;

b. Porous nickel metal produced from the nickel powder specified above
(Above SCOMET 3A114 has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- 3A114 a. Nickel powder of purity 99.0% or greater by weight and having a mean particle size of less than 10 µm;

b. Porous nickel metal produced from the nickel powder specified above ]
3A115 Natural boron, boron carbide or metal borides having a boron purity of 85% or more.
3A116 Fibrous or filamentary materials, and prepregs, as follows:

a. Carbon or aramid fibrous or filamentary materials having ‘specific modulus’ of 12.7 x 106 m or greater; or ‘specific tensile strength’ of 23.5 x 104 m or greater;

b. Glass fibrous or filamentary materials having ‘specific modulus’ of 3.18 x 106 m or greater; and ‘specific tensile strength’ of 7.62 x 104 m or greater;

c. Thermoset resin impregnated continuous yarns, rovings, tows or tapes with a width of 15 mm or less (prepregs), made from carbon or glass fibrous or filamentary materials specified in (a) or (b) above.
3A117 Carbon - carbon composites.
3A118 Titanium alloys having both of the following characteristics:

a. Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20 degrees C); and

b. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

Technical note: The phrase ‘capable of’ encompasses titanium alloys before or after heat treatment
3A119 Rhenium, and alloys containing 90% by weight or more rhenium; and alloys of rhenium and tungsten containing 90% by weight or more of any combination of rhenium and tungsten, have both of the following characteristics:

a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and

b. A mass greater than 20kg
3A120 Technology and Software

Technology and software for the development, production or use of items specified in 3A1 or 3A4
(Above SCOMET 3A118 TO 3A120 has been inserted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
3A2 Structural Materials
3A201 Structural materials such as:

a. Composite structures, laminates, resin impregnated fibre prepregs and metal coated fibre preforms made either with an organic matrix or metal matrix utilizing fibrous or filamentary reinforcements, and manufactures thereof, specially designed for use in rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles and subsystems thereof;

b. Resaturated pyrolized (i.e. Carbon-Carbon) materials specially designed for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles;

c. Fine grain re-crystalised bulk graphites and pyrolytic or fibrous reinforced graphites usable for rocket nozzles and re-entry vehicles nose tips;

d. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes;

e. Materials and coatings for reduced radar reflectivity;

f. Bulk machinable silicon-carbide reinforced unfired ceramic usable in re-entry vehicles nose tips.

g. Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in complete rocket systems of 5A and complete unmanned aerial vehicles of 5B.
3A3 Rocket propellants and constituent chemicals:
3A301

Fuel substances as follows:

a. Hydrazine (CAS 302-01-2) with a concentration of more than 70%;
b. Hydrazine derivatives as follows:
1. Monomethylhydrazine (MMH) (CAS 60-34-4);
2. Unsymmetrical dimethylhydrazine (UDMH) (CAS 57-14-7);
3. Hydrazine mononitrate (CAS 13464-97-6);
4. Trimethylhydrazine (CAS 1741-01-1);
5. Tetramethylhydrazine (CAS 6415-12-9);
6. N, N diallylhydrazine (CAS 5164-11-4);
7. Allylhydrazine (CAS 7422-78-8);
8. Ethylene dihydrazine;
9. Monomethylhydrazine dinitrate;
10. Unsymmetrical dimethylhydrazine nitrate;
11. Hydrazinium azide (CAS 14546-44-2);
12. Dimethylhydrazinium azide;
13. Hydrazinium dinitrate (CAS 13464-98-7);
14. Diimido oxalic acid dihydrazine (CAS 3457-37-2);
15. 2-hydroxyethylhydrazine nitrate (HEHN);
16. Hydrazinium perchlorate (CAS 27978-54-7);
17. Hydrazinium diperchlorate (CAS 13812-39-0);
18. Methylhydrazine nitrate (MHN) (CAS 29674-96-2);
19. Diethylhydrazine nitrate (DEHN);
20. 3, 6-dihydrazino tetrazine nitrate (DHTN);

Technical note: 3, 6-dihydrazino tetrazine nitrate is also referred to as 1, 4-dihydrazine nitrate

c. Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of less than 200 x 10-6 m (200 µm) and an aluminium content of 97% by weight or more, if at least 10% of the total weight is made up of particles of less than 63 µm, according to ISO 2591-1:1988 or national equivalents;

Technical Note: A particle size of 63 µm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).

d. Hydrazine replacement fuels as follows:

1.2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8);
[OLD- 3A301 Propulsive substances – Hydrazine (CAS-302-01)and its derivatives usable as rocket fuel substances including Monomethylhydrazine (MMH)(CAS 60-34), Unsymmetrical di-methyl hydrazine (UDMH), (CAS 57-14-7)Hydrazine nitrate, (except aromatic hydrazines and their salts, adipic acid dihydrazide), ammonium perchlorate, spherical or spheroidal aluminium powder(CAS 7429-90-5); ]
3A302 Metal fuels containing any of the following: Zirconium(CAS 7440-67-7), beryllium(CAS 7440-41-7), magnesium, titanium, tungsten, boron and boron alloys, zinc, and alloys of magnesium(CAS 7439-95-4);
3A303

Polymeric substances, as follows:

a. Carboxy-terminated polybutadiene (including carboxyl – terminated polybutadiene) (CTPB);

b. Hydroxy-terminated polybutadiene (including hydroxyl – terminated polybutadiene) (HTPB);

c. Glycidyl azide polymer (GAP);

d. Polybutadiene - Acrylic Acid (PBAA);

e. Polybutadiene - Acrylic Acid - Acrylonitrile (PBAN);

f. Polytetrahydrofuran polyethylene glycol (TPEG).

g. Polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48- 8).

Technical Note:

Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1, 4-Butanediol (CAS 110-63-4) and polyethylene glycol (PEG) (CAS 25322-68-3).
[OLD- 3A303 Polymeric substances:
Carboxyl-terminated polybutadiene (CTPB)
Hydroxy-Terminated Polybutadiene (HTPB)
Glycidyl azide polymer (GAP)
Polybutadiene acrylic acid (PBAA)
Polybutadiene acrylonitrile (PBAN)
Polytetrahydrofuran polyethylene glycol (TPEG)

Technical Note:
Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1,4- Butanediol and polyethylene glycol (PEG)]
3A304 Composite propellants and composite modified double base propellants;
3A305 High energy density materials such as boron slurry;
3A306 Oxidizers/fuels - Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components; Dinitrogen trioxide, Nitrogen dioxide / Dinitrogen tetroxide, Mixed Oxides of Nitrogen (MON), Dinitrogen pentoxide, Inhibited red fuming nitric acid (IRFNA) (CAS 8007-58-7), Ammonium perchlorate (CAS 7790-98-9), Ammonium Dinitramide (ADN) (CAS 140456-78-6), Hydrazinium Nitroformate (HNF), 2,4,6,8,10,12-Hexanitrohexaazaisowurtzitane (CL-20) (CAS 135285-90-4), Compounds composed of fluorine and one more of other halogens, oxygen or nitrogen.
3A307 Bonding agents - Tris (1-2 (2-methyl)) aziridinyl phosphine oxide (MAPO)(CAS 57-39-6), Trimesoyl-1-(2-ethyl) aziridene (HX-868, BITA)(CAS 7722-73-8), Tepanol (HX-878)(CAS 68412-46-4), Tepan (HX-879) reaction product of tetraethlylenepentamine and acrylonitrile (CAS 68412-45-3), and Polyfunctional aziridine amides with isophthalic, trimesic, isocyanuric, or trimethyladipic backbone also having a 2-methyl or 2-ethyl aziridine group including 1,1'-Isophthaloyl-bis(2-methylaziridene (CAS 7652-64-4), (HX-752, HX-874, and HX-877);
3A308 Curing agents and reaction catalysts - Triphyenyl bismuth (TPB)(CAS 603-33-8);
3A309 Burning rate modifiers –
a. Carboranes, decaboranes, pentaboranes and derivatives thereof;
b. Ferrocene derivatives, as follows:
1. Catocene (CAS 37206-42-1);
2. Ethyl ferrocene;
3. Propyl ferrocene(CAS 1273-89-8)
4. n-Butyl ferrocene(CAS 31904-29-7);
5. Pentyl ferrocene (CAS 1274-00-6);
6. Dicyclopentyl ferrocene(CAS 20773-28-8);
7. Dicyclohexyl ferrocene;
8. Diethyl ferrocene;
9. Dipropyl ferrocene;
10. Dibutyl ferrocene(CAS 1274-08-4);
11. Dihexyl ferrocene (CAS 93894-59-8);
12. Acetyl ferrocenes;
13. Ferrocene Carboxylic acids;
14. Butacene;
c. Other ferrocene derivatives usable as rocket propellant burning rate modifiers.
3A310 Nitrate esters and nitrated plasticisers as follows:
a. Triethylene glycol dinitrate (TEGDN);
b. Trimethylolethane trinitrate (TMETN)(CAS 3032-55-1) ;
c. 1,2,4-butanetriol trinitrate (BTTN)(CAS 6659-60-5) ;
d. Diethylene glycol dinitrate (DEGDN);
e. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso-DAMTR);
f. Nitratoethylnitramine (NENA) based plasticisers, as follows:
1. Methyl-NENA (CAS 17096-47-8);
2. Ethyl-NENA (CAS 85068-73-1);
3. Butyl-NENA (CAS 82486-82-6);
g. Dinitropropyl based plasticisers, as follows:
1. Bis (2,2-dinitropropyl) acetal (BDNPA) (CAS 5108-69-0);
2. Bis (2,2-dinitropropyl) formal (BDNPF) (CAS 5917-61-3).
3A311 Stabilisers as follows:
a. 2-Nitrodiphenylamine (CAS 119-75-5);
b. N-methyl-p-nitroaniline (CAS 100-15-2).
3A4 High explosives
3A401

High explosive substances or mixtures, containing more than 2 % by weight of any of the following:

a. Cyclotetramethylenetetranitramine (HMX ) (CAS 2691-41-0);

b. Cyclotrimethylenetrinitramine (RDX) (CAS 121-82-4);

c. Triaminotrinitrobenzene (TATB) (CAS 3058-38-6);

d. Aminodinitrobenzo-furoxan or 7-amino-4,6 nitrobenzofurazane-1-oxide (ADNBF) (CAS 97096-78-1);

e. 1,1-diamino-2,2-dinitroethylene (DADE or FOX7) (CAS 145250-81-3);

f. 2,4-dinitroimidazole (DNI) (CAS 5213-49-0);

g. Diaminoazoxyfurazan (DAAOF or DAAF) (CAS 78644-89-0);

h. Diaminotrinitrobenzene (DATB) (CAS 1630-08-6);

i. Dinitroglycoluril (DNGU or DINGU) (CAS 55510-04-8);

j. 2,6-Bis (picrylamino)-3,5-dinitropyridine (PYX) (CAS 38082-89-2);

k. 3,3′-diamino-2,2′,4,4′,6,6′-hexanitrobiphenyl or dipicramide (DIPAM) (CAS 17215-44-0);

l. Diaminoazofurazan (DAAzF) (CAS 78644-90-3);

m. 1,4,5,8-tetranitro-pyridazino[4,5-d] pyridazine (TNP) (CAS 229176-04-9);

n. Hexanitrostilbene (HNS) (CAS 20062-22-0); or

o. Any explosive with a crystal density greater than 1.8 g/cm3 and having a detonation velocity greater than 8000 m/s.

Note: License applications for the export of items at 3A401a and 3A401b will normally be denied.
(Above SCOMET 3A401 has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- 3A401 High explosives, and propellants or mixtures containing any of the following;
a. Cycloteramethylenetetranitramine (HMX);
b. Cyclotrimethylenetrinitramine (RDX);
c. Triaminotrinitrobenzene (TATB);
d. Hexanitrostilbene (HNS);
e. Any explosive with a crystal density greater than 1.8 g/cm3 and having a detonation velocity greater than 8000 m/s.
License applications for the export of items at 3A401a and 3A401b will normally be denied.]
3A5 Stealth materials
3A501 a. Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures;
b. Devices, including made from non-stealth material, for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures;
3A502 Materials and coatings (including paints) specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet spectra other than coatings (including paints) when specially used for thermal control of satellites.
3A503 Technology related to the development, production or use of items in 3A.
3B Materials processing and “production equipment”, related “technology” and specially designed components and accessories therefor.
3B001 Remote manipulators that provide mechanical translation of human operator actions by electrical, hydraulic or mechanical means and operating arm and terminal fixture that can be used to provide remote actions;
3B002 Multidirectional, multidimensional weaving and interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to fabricate composite structures except textile machinery which has not been modified for rocket systems;
3B003 Equipment designed or modified for production of fibrous or filamentary materials as follows: converting polymeric substances; vapour deposition on heated filament substrates; wet spinning of refractory ceramics.
3B004 Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies;
3B005 Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites.
3B006 Pyrolytic deposition and densification equipment including:
a. Technology for producing pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases.
b. Specially designed nozzles for the above process.
c. Equipment and process controls and specially designated software thereof, specially designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips.
3B007 Production equipment usable for or specially designed or modified for production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of the solid or liquid rocket propellants or rocket propellant constituents and related technology.
3B008 Refrigeration units and equipment capable of cooling hydrogen or helium to -250 degrees Celsius (23K) or lower.
3B009 Continuous nitrators.
3B010 Dehydration presses.
3B011 Screw extruders usable for or specially designed or modified for high explosive extrusion.
3B012 Cutting machines for the sizing of extruded propellant.
3B013 Sweetie barrels (tumblers) 1.85 m or more in diameter and having over 227 kg product capacity;
3B014 Continuous mixers or batch mixers with provision for mixing under vacuum.
3B015 Fluid energy mills usable for grinding or milling any of the items in 3A3.
3B016

Metal powder production equipment usable for the production, in a controlled environment, of spherical, spheroidal or atomised materials specified in 3A301.c. or 3A302.

Note: This entry includes:

a. Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

b. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

c. Equipment usable for the production of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).
[OLD- 3B016 Equipment to achieve both sphericity and uniform particle size in metal powders.
a. Metal powder production equipment usable for production, in a controlled environment, of spherical or atomized materials including:
b. Plasma generators (high frequency arc-jets) usable for obtaining sputtered or spherical metallic powders with organisation of the process in an argon-water environment
c. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organisation of the process in an argon-water environment.]
3B017 Sputter ion pumps
3B018 Technical data (including processing conditions) and procedures for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves when used for the production of composites or partially processed composites.
3B019 Software specially designed or modified for the use of equipment for the production and handling of materials specified in 3A
3B020 Technology for the development, production or use of items in 3B
3C [Reserved]
3D Chemical and biomaterial manufacturing and handling equipment and facilities:
3D001 (1) Reaction Vessels , Reactors or Agitators

(i) Reaction vessels or reactors, with or without agitators, with total internal (geometric) volume greater than 0.1 m³ (100 l) and less than 20 m³ (20000 l), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys; or

h. niobium (columbium) or niobium alloys.

(ii) Agitators for use in the above-mentioned reaction vessels or reactors; and impellers, blades or shafts designed for such agitators where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys; or

h. niobium (columbium) or niobium alloys.

(2) Storage Tanks, Containers or Receivers

Storage tanks, containers or receivers with a total internal (geometric) volume greater than 0.1 m³ (100 l) where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys; or

h. niobium (columbium) or niobium alloys.

(3) Heat Exchangers or Condensers

Heat exchangers or condensers with a heat transfer surface area of greater than 0.15 m², and less than 20 m²; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. graphite or carbon-graphite;

f. tantalum or tantalum alloys;

g. titanium or titanium alloys;

h. zirconium or zirconium alloys;

i. silicon carbide;

j. titanium carbide; or

k. niobium (columbium) or niobium alloys.

Technical note: carbon-graphite is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight.

(4) Distillation or Absorption Columns

Distillation or absorption columns of internal diameter greater than 0.1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorption columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. graphite or carbon-graphite;

f. tantalum or tantalum alloys;

g. titanium or titanium alloys;

h. zirconium or zirconium alloys; or

i. niobium (columbium) or niobium alloys.

Technical note: carbon-graphite is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight.

(5) Filling Equipment

Remotely operated filling equipment in which all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight; or

b. alloys with more than 25% nickel and 20% chromium by weight.

(6) Valves

Valves with nominal sizes greater than 1.0 cm (3/8") and casings (valve bodies) or preformed casing liners designed for such valves, in which all surfaces that come in direct contact with the chemical(s) being produced, processed, or contained are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. tantalum or tantalum alloys;

f. titanium or titanium alloys;

g. zirconium or zirconium alloys;

h . niobium (columbium) or niobium alloys; or

i. ceramic materials as follows:

1. silicon carbide with a purity of 80% or more by weight;

2. aluminum oxide (alumina) with a purity of 99.9% or more by weight;

3. zirconium oxide (zirconia).

Technical note: The 'nominal size' is defined as the smaller of the inlet and outlet port diameters.

(7) Multi-Walled Piping

Multi-walled piping incorporating a leak detection port, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. graphite or carbon-graphite;

f. tantalum or tantalum alloys;

g. titanium or titanium alloys;

h. zirconium or zirconium alloys; or

i. niobium (columbium) or niobium alloys.

Technical note: carbon-graphite is a composition consisting of amorphous carbon and graphite, in which the graphite-content is eight percent or more by weight.

(8) Pumps

Multiple-seal and seal-less pumps with manufacturer's specified maximum flow-rate greater than 0.6 m3/h, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m³/h (under standard temperature (273 K (0o C)) and pressure (101.3 kPa) conditions), and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come into direct contact with the chemical(s) being processed are made from any of the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight;

c. fluoropolymers (polymeric or elastomeric materials with more than 35% fluorine by weight);

d. glass or glass-lined (including vitrified or enamelled coating);

e. graphite or carbon-graphite;

f. tantalum or tantalum alloys;

g. titanium or titanium alloys;

h. zirconium or zirconium alloys;

i. ceramics;

j. ferrosilicon (high silicon iron alloys); or

k. niobium (columbium) or niobium alloys.

Technical note: carbon-graphite is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight.

(9) Incinerators

Incinerators designed to destroy CW agents, AG-controlled precursors or chemical munitions, having specially designed waste supply systems, special handling facilities, and an average combustion chamber temperature greater than 1000o C, in which all surfaces in the waste supply system that come into direct contact with the waste products are made from or lined with the following materials:

a. nickel or alloys with more than 40% nickel by weight;

b. alloys with more than 25% nickel and 20% chromium by weight; or

c. ceramics.

Technical note: For the listed materials in the above entries, the term 'alloy' when not accompanied by a specific elemental concentration is understood as identifying those alloys where the identified metal is present in a higher percentage by weight than any other element.

Statement of Understanding

These controls do not apply to equipment which is specially designed for use in civil applications (for example food processing, pulp and paper processing, or water purification, etc) and is, by the nature of its design, inappropriate for use in storing, processing, producing or conducting and controlling the flow of chemical warfare agents or any controlled precursor chemical.

Note 1. The objective of these controls should not be defeated by the transfer of any non-controlled item containing one or more controlled components where the controlled component or components are the principal element of the item and can feasibly be removed or used for other purposes.

N.B. In judging whether the controlled component or components are to be considered the principal element, governments should weigh the factors of quantity, value, and technological know-how involved and other special circumstances which might establish the controlled component or components as the principal element of the item being procured.

Note 2. The objective of these controls should not be defeated by the transfer of a whole plant, on any scale, which has been designed to produce any CW agent or precursor chemical.
 
(Above entry in SCOMET Category 3D001 is substituted vide NOTIFICATION NO. 26/2013, DT. 03/07/2013)
[OLD - 3D001 Reaction vessels, reactors or agitators, storage tanks, containers or receivers, heat exchangers or condensers, distillation or absorption columns, valves, remotely operated filling equipment, multi-walled piping, bellows, diaphragm pumps, vacuum pumps, fans, compressors, blowers, gas (including air) handling or other substance-transfer equipment wholly or partly made from any of the following materials;
a. Nickel or alloys with more than 40% nickel by weight
b. Alloys with more than 25% nickel and 20% chromium by weight (e.g. ‘Hastelloy’, ‘Illium’. ‘Inconel’, ‘Incoloy’)
c. Fluoropolymers
d. Glass or glass lined (including vitrified or enamelled coating)
e. Graphite
f. Tantalum or tantalum alloys
g. Titanium or titanium alloys
h. Zirconium or zirconium alloys
i. Ceramics
j. Ferrosilicon
Note: 3D001 does not control the following items:
a. Open vessels fabricated from glass sheets (such as aquariums, water tanks etc.); or cookware, table-ware, decorative glass or ceramic items (such as vases, art objects, etc.)
b. Glass-ware (whether or not metal-jacketed) or glass-lined reaction vessels or reactors, whether or not equipped with agitators, provided that the total internal (geometric) volume of each vessel or reactor is greater than 20,000 litres (20 m3) or less than or equal to 100 litres (0.1 m3). Examples of the latter capacity glass or ceramic-ware include standard laboratory equipment such as test tubes, flasks, retorts etc. ]
3D002 Incinerators designed to destroy any chemicals specified in Category 1.
3D003 Combustors or pyrolysers capable of a heat-zone (‘burner’) temperature greater than 1,273 K (1000 Degree Centigrade), and in which any surfaces that come into direct contact with material coming into the containing chamber are made from, or lined with, any of the following materials:
a. Alloys with more than 25% nickel and 25% chromium by weight; (e.g., ‘Hatelloy’, ‘Illium’, ‘Inconel’, ‘Incoloy’)
b. Nickel, or alloys with more than 40% nickel by weight; or
c. Titanium;
d. Ceramics.
3D004 Equipment related to P3, P4 facilities such as protective suits and class III safety cabinets.
No licenses shall be granted for complete containment facilities at P3, P4, containment level as specified in the World Health Organization (WHO) bio-safety manual.
3D005 Technology related to the development, production or use of items in 3D.
Category 4 Nuclear-related other equipment, assemblies and components; test and production equipment; and related technology not controlled under Category 0
4A Equipment, assemblies, components including test and production equipment
4A001 Flow-forming machines, spin-forming machines capable of flow-forming functions, and mandrels, as follows:

a. For flow forming machines refer to 5A205

b. Spin forming machines having both of the following characteristics:

1. Three or more rollers (active or guiding); and

2. Which, according to the manufacturer’s technical specification, can be equipped with ‘numerical control’ units or a computer control.

c. Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 and 400 mm.

Note:

Item 4A001a and 4A001b include machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
 
4A002 Machine tools, as follows, and any combination thereof, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer’s technical specifications, can be equipped with electronic devices for simultaneous “contouring control” in two or more axes;

N.B.: For “numerical control” units controlled by their associated “software”, see Item 4C

a. Machine tools for turning, that have “positioning accuracies” with all compensations available better (less) than 6 µm according to ISO 230/2 (1988) along any linear axis (overall positioning) for machines capable of machining diameters greater than 35 mm;

Note: Item 4A002.a. does not control bar machines (Swissturn), limited to machining only bar feed thru, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.

b. Machine tools for milling, having any of the following characteristics:

1. “Positioning accuracies” with all compensations available better (less) than 6 µm according to ISO 230/2 (1988) along any linear axis (overall positioning);

2. Two or more contouring rotary axes; or

3. Five or more axes which can be coordinated simultaneously for “contouring control”.

Note: Item 4A002.b. does not control milling machines having both of the following characteristics:

1. X-axis travel greater than 2 m; and

2. Overall “positioning accuracy” on the x-axis worse (more) than 30 µm according to ISO 230/2 (1988).

c. Machine tools for grinding, having any of the following characteristics:

1. “Positioning accuracies” with all compensations available better (less) than 4 µm according to ISO 230/2 (1988) along any linear axis (overall positioning);

2. Two or more contouring rotary axes; or

3 Five or more axes which can be coordinated simultaneously for “contouring control”.

Note: Item 4A002

.c. does not control grinding machines as follows:

1. Cylindrical external, internal, and external-internal grinding machines having all the following characteristics:

a. Limited to a maximum workpiece capacity of 150 mm outside diameter or length; and

b. Axes limited to x, z and c.

2. Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 microns.

Positioning accuracy is according to ISO 230/2 (1988).

d. Non-wire type Electrical Discharge Machines (EDM) that have two or more contouring rotary axes and that can be coordinated simultaneously for “contouring control”.

Notes: 1. Stated “positioning accuracy” levels derived under the following procedures from measurements made according to ISO 230/2 (1988) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests.

Stated “positioning accuracy” are to be derived as follows:

a. Select five machines of a model to be evaluated;

b. Measure the linear axis accuracies according to ISO 230/2 (1988)

c. Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230/2 (1988) standard;

d. Determine the average accuracy value of each axis. This average value becomes the stated “positioning accuracy” of each axis for the model (Âx, Ây...);

e. Since Item 4A002 refers to each linear axis, there will be as many stated “positioning accuracy” values as there are linear axes;

f. If any axis of a machine tool not controlled by Items 4A002.a., 4A002.b., or 4A002.c. has a stated “positioning accuracy” of 6 µm or better (less) for grinding machines, and 8 µm or better (less) for milling and turning machines, both according to ISO 230/2 (1988), then the builder should be required to reaffirm the accuracy level once every eighteen months.

2. Item 4A002. does not control special purpose machine tools limited to the manufacture of any of the following parts:

a. Gears

b. Crankshafts or cam shafts

c. Tools or cutters

d. Extruder worms

Technical Notes:1. Axis nomenclature shall be in accordance with International Standard ISO 841, “Numerical Control Machines - Axis and Motion Nomenclature”.

2. Not counted in the total number of contouring axes are secondary parallel contouring axes (e.g., the w-axis on horizontal boring mills or a secondary rotary axis the centerline of which is parallel to the primary rotary axis).

3. Rotary axes do not necessarily have to rotate over 360 degrees. A rotary axis can be driven by a linear device, e.g., a screw or a rack-and-pinion.

4. For the purposes of 4A002. the number of axes which can be coordinated simultaneously for “contouring control” is the number of axes along or around which, during processing of the workpiece, simultaneous and interrelated motions are performed between the workpiece and a tool. This does not include any additional axes along or around which other relative motions within the machine are performed, such as:

a. Wheel-dressing systems in grinding machines;

b. Parallel rotary axes designed for mounting of separate workpieces;

c. Co-linear rotary axes designed for manipulating the same workpiece by holding it in a chuck from different ends.

5. A machine tool having at least 2 of the 3 turning, milling or grinding capabilities (e.g., a turning machine with milling capability) must be evaluated against each applicable entry, 4A002.a., 4A002.b. and 4A002.c.

6. Items 4A002.b.3 and 4A002.c.3 include machines based on a parallel linear kinematic design (e.g., hexapods) that have 5 or more axes none of which are rotary axes.
 
4A003 Dimensional inspection machines, instruments, or systems, as follows:

a. Computer controlled or numerically controlled coordinate measuring machines (CMM) having either of the following characteristics:

1. Having only two axes and having a maximum permissible error of length measurement along any axis (one dimensional), identified as any combination of E0x MPE, E0y MPE or E0z MPE, equal to or less(better) than (1.25 + L/1000) µm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009); or

2. Three or more axes and having a three dimensional (volumetric) maximum permissible error of length measurement (E0, MPE equal to or less (better) than (1.7 + L/800) µm (where L is the measured length in mm) at any point within the operating range of the machine (i.e., within the length of the axis), according to ISO 10360-2(2009).

Technical Note: The E0, MPE of the most accurate configuration of the CMM specified according to ISO 10360-2(2009) by the manufacturer (e.g., best of the following: probe stylus length, motion parameters, environment) and with all compensations available shall be compared to the 1.7 + L/ 800 µm threshold.

b. Linear displacement measuring instruments, as follows:

1. Non-contact type measuring systems with a “resolution” equal to or better (less) than 0.2 µm within a measuring range up to 0.2 mm;

2. Linear variable differential transformer (LVDT) systems having both of the following characteristics:

a. 1. “Linearity” equal to or less (better) than 0.1% measured from 0 to the full operating range, for LVDTs with an operating range up to 5 mm; or

2. “Linearity” equal to or less (better) than 0.1% measured from 0 to 5 mm for LVDTs with an operating range greater than 5 mm; and

b. Drift equal to or better (less) than 0.1% per day at a standard ambient test room temperature ± 1 K;

3. Measuring systems having both of the following characteristics:

a. Contain a laser; and

b. Maintain for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and a standard pressure:v1. A “resolution” over their full scale of 0.1 µm or better; and

2. With a “measurement uncertainty” equal to or better (less) than (0.2 + L/2000) µm (L is the measured length in millimeters);

Note: Item 1.B.3.b.3. does not control measuring interferometer systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimensional inspection machines, or similar equipment.

Technical Note: In Item 1.B.3.b. ‘linear displacement’ means the change of distance between the measuring probe and the measured object.

c. Angular displacement measuring instruments having an “angular position deviation” equal to or better (less) than 0.00025°;

Note: Item 1.B.3.c. does not control optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.

d. Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:

1. “Measurement uncertainty” along any linear axis equal to or better (less) than 3.5 µm per 5 mm; and

2. “Angular position deviation” equal to or less than 0.02°.

Notes: 1. Item 1.B.3. includes machine tools that can be used as measuring machines if they meet or exceed the criteria specified for the measuring machine function.

2. Machines described in Item 1.B.3. are controlled if they exceed the threshold specified anywhere within their operating range

Technical Note: All parameters of measurement values in this item represent plus/minus, i.e., not total band.
4A004 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:

a. Furnaces having all of the following characteristics:

1. Capable of operation at temperatures above 1123 K (850 °C);

2. Induction coils 600 mm or less in diameter; and

3. Designed for power inputs of 5 kW or more;

Note: Item 4A004.a. does not control furnaces designed for the processing of semiconductor wafers.

b. Power supplies, with a specified output power of 5 kW or more, specially designed for furnaces specified in Item 4A004.a.
4A005 Isostatic presses’, and related equipment, as follows:

a. ‘Isostatic presses’ as specified in 5A208;

b. Dies, moulds, and controls specially designed for the ‘isostatic presses’ specified in Item 4A005.a.

Technical Notes:

1. In Item 4A005 ´Isostatic presses’ means equipment capable of pressurizing a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a work piece or material.

2. In Item 4A005 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
4A006 Vibration test systems, equipment, and components as follows:

a. Electrodynamic vibration test systems, having all of the following characteristics:

1. Employing feedback or closed loop control techniques and incorporating a digital control unit;

2. Capable of vibrating at 10 g RMS or more between 20 and 2000 Hz; and

3. Capable of imparting forces of 50 kN or greater measured ‘bare table’;

b. Digital control units, combined with ‘software’ specially designed for vibration testing, with a real-time bandwidth greater than 5 kHz and being designed for a system specified in Item 4A006.a.;

c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force of 50 kN or greater measured ‘bare table’, which are usable for the systems specified in Item 4A006.a.;

d. Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force of 50 kN or greater, measured ‘bare table,’ which are usable for the systems specified in Item 4A006.a..

Technical Note: In Item 4A006 ‘bare table’ means a flat table, or surface, with no fixtures or fittings.
4A007 Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment, as follows:

a. Arc re-melt and casting furnaces having both of the following characteristics:

1. Consumable electrode capacities between 1000 and 20000 cm3; and

2. Capable of operating with melting temperatures above 1973 K (1700 °C);

b. Electron beam melting furnaces and plasma atomisation and melting furnaces, having both of the following characteristics:

1. A power of 50 kW or greater; and

2. Capable of operating with melting temperatures above 1473 K (1200 °C);

c. Computer control and monitoring systems specially configured for any of the furnaces specified in Item 4A007.a. or 4A007.b.
4A008 Crucibles made of materials resistant to liquid actinide metals, as follows:

a. Crucibles having both of the following characteristics:

1. A volume of between 150 cm3 (150 ml) and 8000 cm3 (8 litres); and

2. Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2% or less by weight:

a. Calcium fluoride (CaF2);

b. Calcium zirconate (metazirconate) (CaZrO3);

c. Cerium sulphide (Ce2S3);

d. Erbium oxide (erbia) (Er2O3);

e. Hafnium oxide (hafnia) (HfO2);

f. Magnesium oxide (MgO);

g. Nitrided niobium-titanium-tungsten alloy (approximately 50% Nb, 30% Ti, 20% W);

h. Yttrium oxide (yttria) (Y2O3); or

i. Zirconium oxide (zirconia) (ZrO2);

b. Crucibles having both of the following characteristics:

1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres); and

2. Made of or lined with tantalum, having a purity of 99.9% or greater by weight;

c. Crucibles having all of the following characteristics:

1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres);

2. Made of or lined with tantalum, having a purity of 98% or greater by weight; and

3. Coated with tantalum carbide, nitride, boride, or any combination thereof.
4A009 Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.
4A010 Composite structures in the form of tubes having both of the following characteristics:

a. An inside diameter of between 75 and 400 mm; and

b. Made with any of the materials specified in Item 3A116.
4A011 Frequency changers or generators, usable as a variable frequency or fixed frequency motor drive, having all of the following characteristics:

N.B.1: Frequency changers and generators specially designed or prepared for the gas centrifuge process are controlled under Prescribe Equipment (0B)

N.B.2: “Software” specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics below is controlled (see Item 4C).

a. Multiphase output providing a power of 40 VA or greater;

b. Operating at a frequency of 600 Hz or more; and

c. Frequency control better (less) than 0.2%.

Notes: 1. Item 4A011 only controls frequency changers intended for specific industrial machinery and/or consumer goods (machine tools, vehicles, etc.) if the frequency changers can meet the characteristics above when removed,

2. For the purpose of export control, the Government will determine whether or not a particular frequency changer meets the characteristics above, taking into account hardware and software constraints.

Technical Notes: 1. Frequency changers in Item 4A011. are also known as converters or inverters.

2. The characteristics specified in item 4A011 may be met by certain equipment marketed such as:

Generators, Electronic Test Equipment, AC Power Supplies, Variable Speed Motor Drives, Variable Speed Drives (VSDs), Variable Frequency Drives (VFDs), Adjustable Frequency Drives (AFDs), or Adjustable Speed Drives (ASDs).
4A012 Lasers, laser amplifiers and oscillators as follows:

a. Copper vapour lasers having both of the following characteristics:

1. Operating at wavelengths between 500 and 600 nm; and

2. An average output power equal to or greater than 40 W;

b. Argon ion lasers having both of the following characteristics:

1. Operating at wavelengths between 400 and 515 nm; and

2. An average output power greater than 40 W;

c. Neodymium-doped (other than glass) lasers with an output wavelength between 1000 and 1100 nm having either of the following:

1. Pulse-excited and Q-switched with a pulse duration equal to or greater than 1 ns, and having either of the following:

a. A single-transverse mode output with an average output power greater than 40 W; or

b. A multiple-transverse mode output with an average output power greater than 50 W;

or

2. Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of greater than 40 W;

d. Tuneable pulsed single-mode dye laser oscillators having all of the following characteristics:

1. Operating at wavelengths between 300 and 800 nm;

2. An average output power greater than 1 W;

3. A repetition rate greater than 1 kHz; and

4. Pulse width less than 100 ns;

e. Tuneable pulsed dye laser amplifiers and oscillators having all of the following characteristics:

1. Operating at wavelengths between 300 and 800 nm;

2. An average output power greater than 30 W;

3. A repetition rate greater than 1 kHz; and

4. Pulse width less than 100 ns;

Note: Item 4A012e does not control single mode oscillators.

f. Alexandrite lasers having all of the following characteristics:

1. Operating at wavelengths between 720 and 800 nm;

2. A bandwidth of 0.005 nm or less;

3. A repetition rate greater than 125 Hz; and

4. An average output power greater than 30 W;

g. Pulsed carbon dioxide lasers having all of the following characteristics:

1. Operating at wavelengths between 9000 and 11000 nm;

2. A repetition rate greater than 250 Hz;

3. An average output power greater than 500 W; and

4. Pulse width of less than 200 ns;

Note: Item 4A012g does not control the higher power (typically 1 to 5 1kW) industrial CO2 lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns.

h. Pulsed excimer lasers (XeF, XeCl, KrF) having all of the following characteristics:

1. Operating at wavelengths between 240 and 360 nm;

2. A repetition rate greater than 250 Hz; and

3. An average output power greater than 500 W;

i. Para-hydrogen Raman shifters designed to operate at 16 µm output wavelength and at a repetition rate greater than 250 Hz.

j. Pulsed carbon monoxide lasers having all of the following characteristics:

1. Operating at wavelengths between 5000 and 6000 nm;

2. A repetition rate greater than 250 Hz;

3. An average output power greater than 200 W; and

4. Pulse width of less than 200 ns.

Note: Item 4A012.j. does not control the higher power (typically 1 to 5 kW) industrial CO lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns.
4A013 Valves having all of the following characteristics:

a. A nominal size of 5 mm or greater;

b. Having a bellows seal; and

c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60% nickel by weight.

Technical Note: For valves with different inlet and outlet diameter, the nominal size parameter in Item 4A013a refers to the smallest diameter.
4A014 Superconducting solenoidal electromagnets having all of the following characteristics:

a. Capable of creating magnetic fields greater than 2 T;

b. A ratio of length to inner diameter greater than 2;

c. Inner diameter greater than 300 mm; and

d. Magnetic field uniform to better than 1% over the central 50% of the inner volume.

Note: Item 4A014 does not control magnets specially designed for and exported as part of medical nuclear magnetic resonance (NMR) imaging systems. (‘As part of’ does not necessarily mean physical part in the same shipment. Separate shipments from different sources are allowed, provided the related export documents clearly specify the ‘as part of” relationship.)
4A015 High-power direct current power supplies having both of the following characteristics:

a. Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and

b. Current or voltage stability better than 0.1% over a time period of 8 hours
4A016 High-voltage direct current power supplies having both of the following characteristics:

a. Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and

b. Current or voltage stability better than 0.1% over a time period of 8 hours.
 
4A017 All types of pressure transducers capable of measuring absolute pressures and having all of the following characteristics:

a. Pressure sensing elements made of or protected by aluminium, aluminium alloy, aluminium oxide (alumina or sapphire), nickel, nickel alloy with more than 60% nickel by weight, or fully fluorinated hydrocarbon polymers;

b. Seals, if any, essential for sealing the pressure sensing element, and in direct contact with the process medium, made of or protected by aluminium, aluminium alloy, aluminium oxide (alumina or sapphire), nickel, nickel alloy with more than 60% nickel by weight, or fully fluorinated hydrocarbon polymers; and

c. Having either of the following characteristics:

1. A full scale of less than 13 kPa and an “accuracy” of better than ± 1% of full scale; or

2. A full scale of 13 kPa or greater and an “accuracy” of better than ± 130 Pa when measuring at 13 kPa.

Technical Notes: 1. In Item 4A017. pressure transducers are devices that convert pressure measurements into a signal.

2. In Item 4A017. “accuracy” includes nonlinearity, hysteresis and repeatability at ambient temperature.
 
4A018 Vacuum pumps having all of the following characteristics:

a. Input throat size equal to or greater than 380 mm;

b. Pumping speed equal to or greater than 15 m3/s; and

c. Capable of producing an ultimate vacuum better than 13.3 mPa.

Technical Notes: 1. The pumping speed is determined at the measurement point with nitrogen gas or air.

2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.
4A019 Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.
4A020 Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:

a. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps; Note: Item 4A020a includes precision mandrels, clamps, and shrink fit machines.

b. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;

Technical Note: In Item 4A020b such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.

c. Bellows-forming mandrels and dies for producing single -convolution bellows.

Technical Note: The bellows referred to in Item 4A020c have all of the following characteristics:

1. Inside diameter between 75 and 400 mm;

2. Length equal to or greater than 12.7 mm;

3. Single convolution depth greater than 2 mm; and

4. Made of high-strength aluminium alloys, maraging steel, or high strength fibrous or filamentary materials.
4A021 Centrifugal multi-plane balancing machines, fixed or portable, horizontal or vertical, as follows:

a. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:

1. Swing or journal diameter greater than 75 mm;

2. Mass capability of from 0.9 to 23 kg; and

3. Capable of balancing speed of revolution greater than 5000 rpm;

b. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:

1. Journal diameter greater than 75 mm;

2. Mass capability of from 0.9 to 23 kg;

3. A minimum achievable residual specific unbalance equal to or less than 10 g-mm/kg per plane; and

4. Belt drive type.
4A022 Filament winding machines and related equipment, as follows:

a. Filament winding machines as specified in 5A206; and having all of the following characteristics:

1. Having motions for positioning, wrapping, and winding fibers coordinated and programmed in two or more axes;

2. Specially designed to fabricate composite structures or laminates from “fibrous or filamentary materials”; and

3. Capable of winding cylindrical tubes with an internal diameter between 75 and 650 mm and lengths of 300 mm or greater;

b. Coordinating and programming controls for the filament winding machines specified in Item 4A022a;

c. Precision mandrels for the filament winding machines specified in Item 4A022a.
4A023 Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

Notes: 1. Item 4A023 includes separators capable of enriching stable isotopes as well as those for uranium. (A separator capable of separating the isotopes of lead with a one-mass unit difference is inherently capable of enriching the isotopes of uranium with a three-unit mass difference.)

2. Item 4A023 includes separators with the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.

Technical Note: A single 50 mA ion source cannot produce more than 3 g of separated highly enriched uranium (HEU) per year from natural abundance feed.
 
4A024 Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:

N.B.: Mass spectrometers specially designed or prepared for analyzing on-line samples of uranium hexafluoride are controlled under Prescribed Equipment (0B Category).

a. Inductively coupled plasma mass spectrometers (ICP/MS);

b. Glow discharge mass spectrometers (GDMS);

c. Thermal ionization mass spectrometers (TIMS);

d. Electron bombardment mass spectrometers having both of the following features:

1. A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and

2. One or more cold traps that can be cooled to a temperature of 193 K (-80 °C) or less in order to trap analyte molecules that are not ionized by the electron beam;

e. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.

Technical Notes:

1. Item 4A024.d. describes mass spectrometers that are typically used for isotopic analysis of UF6 gas samples.

2. Electron bombardment mass spectrometers in Item 4A024.d. are also known as electron impact mass spectrometers or electron ionization mass spectrometers.

3. In Item 4A024.d.2, a ‘cold trap’ is a device that traps gas molecules by condensing or freezing them on cold surfaces. For the purposes of this entry, a closed-loop gaseous helium cryogenic vacuum pump is not a cold trap.
4A025 Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:

a. Made of phosphor bronze mesh chemically treated to improve wettability; and

b. Designed to be used in vacuum distillation towers.
 
4A026 Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:

a. Airtight (i.e., hermetically sealed);

b. A capacity greater than 8.5 m3/h; and

c. Either of the following characteristics:

1. For concentrated potassium amide solutions (1% or greater), an operating pressure of 1.5 to 60 MPa; or

2. For dilute potassium amide solutions (less than 1%), an operating pressure of 20 to 60 MPa.
4A027 Turboexpanders or turboexpander-compressor sets having both of the following characteristics:

a. Designed for operation with an outlet temperature of 35 K (- 238 ºC) or less; and

b. Designed for a throughput of hydrogen gas of 1000 kg/h or greater.
4A028 Water-hydrogen sulphide exchange tray columns and internal contactors, as follows:

N.B.: For columns which are specially designed or prepared for the production of heavy water, see Prescribed Equipment (0B002).

a. Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:

1. Can operate at pressures of 2 MPa or greater;

2. Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and

3. With a diameter of 1.8 m or greater;

b. Internal contactors for the water-hydrogen sulphide exchange tray columns specified in Item 4A028a.

Technical Note: Internal contactors of the columns are segmented trays which have an effective assembled diameter of 1.8 m or greater; are designed to facilitate counter current contacting and are constructed of stainless steels with a carbon content of 0.03% or less. These may be sieve trays, valve trays, bubble cap trays or turbo grid trays.
4A029 Hydrogen-cryogenic distillation columns having all of the following characteristics:

a. Designed for operation at internal temperatures of 35 K (-238 ºC) or less;

b. Designed for operation at internal pressures of 0.5 to 5 MPa;

c. Constructed of either:

1. Stainless steel of the 300 series with low sulfur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or

2. Equivalent materials which are both cryogenic and H2-compatible; and

d. With internal diameters of 30 cm or greater and ‘effective lengths’ of 4 m or greater.

Technical Note: The term ‘effective length’ means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column.
 
4A030 Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following characteristics:

a. Capable of an inlet volume flow rate of 50 m3/h or greater;

b. Capable of a pressure ratio of 2:1 or greater; and

c. Having all surfaces that come in contact with the process gas made from any of the following materials:

1. Aluminium or aluminium alloy;

2. Aluminium oxide;

3. Stainless steel;

4. Nickel or nickel alloy;

5. Phosphor bronze; or

6. Fluoropolymers.

Technical Notes: 1. In a scroll compressor or vacuum pump, crescentshaped pockets of gas are trapped between one or more pairs of intermeshed spiral vanes, or scrolls, one of which moves while the other remains stationary. The moving scroll orbits the stationary scroll; it does not rotate. As the moving scroll orbits the stationary scroll, the gas pockets diminish in size (i.e., they are compressed) as they move toward the outlet port of the machine.

2. In a bellows-sealed scroll compressor or vacuum pump, the process gas is totally isolated from the lubricated parts of the pump and from the external atmosphere by a metal bellows. One end of the bellows is attached to the moving scroll and the other end is attached to the stationary housing of the pump.

3. Fluoropolymers include, but are not limited to, the following materials:

a. Polytetrafluoroethylene (PTFE),

b. Fluorinated Ethylene Propylene (FEP),

c. Perfluoroalkoxy (PFA),

d. Polychlorotrifluoroethylene (PCTFE); and

e. Vinylidene fluoride-hexafluoropropylene copolymer.
 
4A031 Industrial equipment including assemblies and components (other than those specified under Prescribed Equipment in 0B003.e) as follows:

a. High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:

1. A ‘cold area’ greater than 0.09 m2;

2. A density greater than 3 g/cm3; and

3. A thickness of 100 mm or greater.

Technical Note: In Item 4A031.a.1. the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application.

b. Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 5 x 104 Gy (silicon) without operational degradation.

Technical Note: The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionizing radiation.

c. ‘Robots’, ‘end-effectors’ and control units as follows:

1. ‘Robots’ or ‘end-effectors’ having either of the following characteristics:

(a) Specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives); or

(b) Specially designed or rated as radiation hardened to withstand a total radiation dose greater than 5 x 104 Gy (silicon) without operational degradation;

2. Control units specially designed for any of the ‘robots’ or ‘endeffectors’ specified in Item 4A031.c.1.

Note: Item 1.A.3. does not control ‘robots’ specially designed for non-nuclear industrial applications such as automobile paint-spraying booths.

Technical Notes:

1. ‘Robots’

In Item 4A031.c. ‘robot’ means a manipulation mechanism, which may be of the continuous path or of the point-to-point variety, may use “sensors”, and has all of the following characteristics:

(a) is multifunctional;

(b) is capable of positioning or orienting material, parts, tools, or special devices through variable movements in three-dimensional space;

(c) incorporates three or more closed or open loop servo-devices which may include stepping motors; and

(d) has “user-accessible programmability” by means of teach/playback method or by means of an electronic computer which may be a programmable logic controller, i.e., without mechanical intervention.

N.B.1:

In the above definition “sensors” means detectors of a physical phenomenon, the output of which (after conversion into a signal that can be interpreted by a control unit) is able to generate “programs” or modify programmed instructions or numerical “program” data.

This includes “sensors” with machine vision, infrared imaging, acoustical imaging, tactile feel, inertial position measuring, optical or acoustic ranging or force or torque measuring capabilities.

N.B.2:

In the above definition “user-accessible programmability” means the facility allowing a user to insert, modify or replace “programs” by means other than:

(a) a physical change in wiring or interconnections; or

(b) the setting of function controls including entry of parameters.

N.B.3:

The above definition does not include the following devices:

(a) Manipulation mechanisms which are only manually/teleoperator controllable;

(b) Fixed sequence manipulation mechanisms which are automated moving devices operating according to mechanically fixed programmed motions. The “program” is mechanically limited by fixed stops, such as pins or cams. The sequence of motions and the selection of paths or angles are not variable or changeable by mechanical, electronic, or electrical means;

(c) Mechanically controlled variable sequence manipulation mechanisms which are automated moving devices operating according to mechanically fixed programmed motions. The “program” is mechanically limited by fixed, but adjustable, stops such as pins or cams. The sequence of motions and the selection of paths or angles are variable within the fixed “program” pattern. Variations or modifications of the “program” pattern (e.g., changes of pins or exchanges of cams) in one or more motion axes are accomplished only through mechanical operations;

(d) Non-servo-controlled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions. The “program” is variable but the sequence proceeds only by the binary signal from mechanically fixed electrical binary devices or adjustable stops;

(e) Stacker cranes defined as Cartesian coordinate manipulator systems manufactured as an integral part of a vertical array of storage bins and designed to access the contents of those bins for storage or retrieval.

2. ‘End-effectors’

In Item 4A031.c. ‘end-effectors’ are grippers, ‘active tooling units’, and any other tooling that is attached to the baseplate on the end of a ‘robot’ manipulator arm.

N.B.:

In the above definition ‘active tooling units’ is a device for applying motive power, process energy or sensing to the workpiece.

d. Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:

1. A capability of penetrating 0.6 m or more of hot cell wall (through-thewall operation); or

2. A capability of bridging over the top of a hot cell wall with a thickness of 0.6 m or more (over-the-wall operation).

Technical Note: Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of a master/slave type or operated by joystick or keypad.
 
4B Equipment, assemblies and components, including test and measurement equipment usable in development of nuclear explosive devices
 
4B001 Photomultiplier tubes having both of the following characteristics:

a. Photocathode area of greater than 20 cm2; and

b. Anode pulse rise time of less than 1 ns.
4B002 Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:

a. 1. An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and

2. With a figure of merit (K) of 0.25 or greater; or

b. 1. An accelerator peak electron energy of 25 MeV or greater; and

2. A peak power greater than 50 MW.

Note: Item 4B002 does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes.

Technical Notes: 1. The figure of merit K is defined as: K=1.7 x 103 V2.65Q. V is the peak electron energy in million electron volts. If the accelerator beam pulse duration is less than or equal to 1µs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 µs, then Q is the maximum accelerated charge in 1 µs. Q equals the integral of i with respect to t, over the lesser of 1 µs or the time duration of the beam pulse ( Q= ?idt ) where i is beam current in amperes and t is the time in seconds.

2. Peak power = (peak potential in volts) x (peak beam current in amperes).

3. In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 µs or the duration of the bunched beam packet resulting from one microwave modulator pulse.

4. In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.
 
4B003 High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1.5 km/s or greater.

Note: This item does not control guns specially designed for high velocity weapon systems.
 
4B004 High-speed cameras and imaging devices and components therefor, as follows:

N.B.: “Software” specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics below is controlled (See Item 4C).

a. Streak cameras, and specially designed components therefor, as follows:

1. Streak cameras with writing speeds greater than 0.5 mm/µs;

2. Electronic streak cameras capable of 50 ns or less time resolution;

3. Streak tubes for cameras specified in 4B004.a.2.;

4. Plug-ins specially designed for use with streak cameras which have modular structures and that enable the performance specifications in 4B004.a.1 or 4B004.a.2.;

5. Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 4B004.a.1.

b. Framing cameras and specially designed components therefor as follows:

1. Framing cameras with recording rates greater than 225,000 frames per second;

2. Framing cameras capable of 50 ns or less frame exposure time;

3. Framing tubes and solid-state imaging devices having a fast image gating (shutter) time of 50ns or less specially designed for cameras specified in 4B004.b.1 or 4B004.b.2.;

4. Plug-ins specially designed for use with framing cameras which have modular structures and that enable the performance specifications in 4B004.b.1 or 4B004.b.2.;

5. Synchronizing electronics units, rotor assemblies consisting of turbines, mirrors and bearings specially designed for cameras specified in 4B004.b.1 or 4B004.b.2.

c. Solid state or electron tube cameras and specially designed components therefor as follows:

1. Solid-state cameras or electron tube cameras with a fast image gating (shutter) time of 50 ns or less;

2. Solid-state imaging devices and image intensifiers tubes having a fast image gating (shutter) time of 50 ns or less specially designed for cameras specified in 4B004.c.1.;

3. Electro-optical shuttering devices (Kerr or Pockels cells) with a fast image gating (shutter) time of 50 ns or less;

4. Plug-ins specially designed for use with cameras which have modular structures and that enable the performance specifications in 4B004.c.1.

Technical Note: High speed single frame cameras can be used alone to produce a single image of a dynamic event, or several such cameras can be combined in a sequentially-triggered system to produce multiple images of an event.
4B005 High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:

a. Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; and

b. Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information.
4B006 Specialized instrumentation for hydrodynamic experiments, as follows:

a. Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 µs;

b. Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2);

c. Quartz pressure transducers for pressures greater than 10 GPa.

Note: Item 4B006.a. includes velocity interferometers such as VISARs (Velocity Interferometer Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters).
4B007 High-speed pulse generators, and pulse heads therefor, having both of the following characteristics:

a. Output voltage greater than 6 V into a resistive load of less than 55 ohms; and

b. ‘Pulse transition time’ less than 500 ps.

Technical Notes:

1. In Item 4B007.b. ‘pulse transition time’ is defined as the time interval between 10% and 90% voltage amplitude.

2. Pulse heads are impulse forming networks designed to accept a voltage step function and shape it into a variety of pulse forms that can include rectangular, triangular, step, impulse, exponential, or monocycle types. Pulse heads can be an integral part of the pulse generator, they can be a plug-in module to the device or they can be an externally connected device.
4B008 Detonators and multipoint initiation systems, as follows:

a. Electrically driven explosive detonators, as follows:

1. Exploding bridge (EB);

2. Exploding bridge wire (EBW);

3. Slapper;

4. Exploding foil initiators (EFI);

b. Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over an area greater than 5000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2.5 µs.

Note: Item 4B008. does not control detonators using only primary explosives, such as lead azide.

Technical Note:

In Item 4B008. the detonators of concern all utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper types,the exploding conductor starts a chemical detonation in a contacting high-explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator.
4B009 Firing sets and equivalent high-current pulse generators, as follows:

a. Detonator firing sets (initiation systems, firesets), including electronically-charged, explosively-driven and optically-driven firing sets designed to drive multiple controlled detonators specified by Item 4B008 above;

b. Modular electrical pulse generators (pulsers) having all of the following characteristics:

1. Designed for portable, mobile, or ruggedized-use;

2. Capable of delivering their energy in less than 15 µs into loads of less than 40 ohms;

3. Having an output greater than 100 A;

4. No dimension greater than 30 cm;

5. Weight less than 30 kg ; and

6. Specified to operate over an extended temperature range of 223 to 373 K (-50 ºC to 100 ºC) or specified as suitable for aerospace applications.

c. Micro-firing units having all of the following characteristics:

1. No dimension greater than 35 mm;

2. Voltage rating of equal to or greater than 1 kV; and

3. Capacitance of equal to or greater than 100 nF.

Note: Optically driven firing sets include both those employing laser initiation and laser charging. Explosively-driven firing sets include both explosive ferroelectric and explosive ferromagnetic firing set types. Item 4B009.b. includes xenon flashlamp drivers.
 
4B010 Switching devices as follows:

a. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:

1. Containing three or more electrodes;

2. Anode peak voltage rating of 2.5 kV or more;

3. Anode peak current rating of 100 A or more; and

4. Anode delay time of 10 µs or less;

Note: Item 4B010.a. includes gas krytron tubes and vacuum sprytron tubes.

b. Triggered spark-gaps having both of the following characteristics:

1. Anode delay time of 15 µs or less; and

2. Rated for a peak current of 500 A or more;

c. Modules or assemblies with a fast switching function having all of the following characteristics:

1. Anode peak voltage rating greater than 2 kV;

2. Anode peak current rating of 500 A or more; and

3. Turn-on time of 1 µs or less.
4B011 Pulse discharge capacitors having either of the following sets of characteristics:

a. 1. Voltage rating greater than 1.4 kV;

2. Energy storage greater than 10 J;

3. Capacitance greater than 0.5 µF; and

4. Series inductance less than 50 nH; or

b. 1. Voltage rating greater than 750 V;

2. Capacitance greater than 0.25 µF; and

3. Series inductance less than 10 nH.
4B012 Neutron generator systems, including tubes, having both of the following characteristics:

a. Designed for operation without an external vacuum system; and

b. 1. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction; or

2. Utilizing electrostatic acceleration to induce a deuteriumdeuterium nuclear reaction and capable of an Output of 3 x 109 neutrons/s or greater.
4B013 Striplines to provide low inductance path to detonators with the following characteristics:

a. Voltage rating greater than 2 kV; and

b. Inductance of less than 20 nH 4C Technology and Software Technology and software for the development, production or use of items specified in 4A or 4B. ’
 
(Above SCOMET Category 4A, 4B & 4C has been substituted vide NOTIFICATION NO. 05/2016, DT. 29/04/2016 )
[OLD- 4A Equipment, assemblies, components including test and production equipment
4A001 Flow-forming machines, spin-forming machines capable of flow-forming functions, and mandrels, as follows:
a. For flow forming machines refer to 5A205.
b. Spin forming machines having both of the following characteristics:
1. Three or more rollers (active or guiding); and
2. which can be equipped with ‘numerical control’ units or a computer control.
c. Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 and 400 mm.
Note: Item 4A001a and 4A001b include machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
4A002 Machine tools, as follows, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer’s technical specifications, can be equipped with electronic devices for simultaneous contouring control in two or more axes:
a. Machine tools for turning, that have positioning accuracies with all compensations available better (less) than 6 µm along any linear axis (overall positioning) for machines capable of machining diameters greater than 35mm;
Note: Item 4A002a does not control bar machines, limited to machining only bar feed through, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.
b. Machine tools for milling, having any of the following characteristics:
1. Positioning accuracies with all compensations available better (less) than 6 µm along any linear axis (overall positioning); or
2. Two or more contouring rotary axes;
Note: Item 4A002b does not control milling machines having both of the following characteristics:
1. X-axis travel greater than 2 m; and
2. Overall positioning accuracy on the x-axis worse (more) than 30 µm.
c. Machine tools for grinding, having any of the following characteristics:
1. Positioning accuracies with all compensations available better (less) than 4 µm along any linear axis (overall positioning); or
2. Two or more contouring rotary axes;
Note: Item 4A002c does not control grinding machines as follows:
1. Cylindrical external, internal, and external-internal grinding machines having all the following characteristics:
a. Limited to cylindrical grinding;
b. A maximum work-piece outside diameter or length of 150 mm;
c. Not more than two axes that can be coordinated simultaneously for contouring control; and
d. No contouring c-axis;
2. Jig grinders with axes limited to x, y, c, and a, where c-axis is used to maintain the grinding wheel normal to the work surface, and the a-axis is configured to grind barrel cams;
3. Tool or cutter grinding machines with software specially designed for the manufacturing of tools or cutters;
4. Crankshaft or camshaft grinding machines.
d. Non-wire type Electrical Discharge Machines (EDM) that have two or more contouring rotary axes and that can be coordinated simultaneously for contouring control.
Note: Stated positioning accuracy levels derived under the following procedures from measurements made according to ISO 230/2 (1988) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests.
Stated positioning accuracy are to be derived as follows:
1. Select five machines of a model to be evaluated;
2. Measure the linear axis accuracies according to ISO 230/2 (1988);
3. Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230/2 (1988) standard;
4. Determine the average accuracy value of each axis. This average value becomes the stated positioning accuracy of each axis for the model (Âx, Ây...);
5. Since Item 4A002 refers to each linear axis, there will be as many stated positioning accuracy values as there are linear axes;
6. If any axis of a machine tool not controlled by Items 4A002a, 4A002b, or 4A002c has a stated positioning accuracy of 6 µm or better (less) for grinding machines, and 8 µm or better (less) for milling and turning machines, both according to ISO 230/2 (1988), then the builder should be required to reaffirm the accuracy level once every eighteen months.
Technical Notes
1. Axis nomenclature shall be in accordance with International Standard ISO 841, Numerical Control Machines Axis and Motion Nomenclature.
2. Not counted in the total number of contouring rotary axes are secondary parallel contouring rotary axes the centre line of which is parallel to the primary rotary axis.
3. Rotary axes do not necessarily have to rotate over 360 degrees. A rotary axis can be driven by a linear device, e.g., a screw or a rack and-pinion.
4A003 Dimensional inspection machines, instruments, or systems, as follows:
a. Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics:
1. Two or more axes; and
2. A one-dimensional length measurement uncertainty equal to or better (less) than (1.25 + L/1000) µm tested with a probe of an accuracy of better (less) than 0.2 µm (L is the measured length in millimetres);
b. ‘Linear displacement’ measuring instruments, as follows:
1. Non-contact type measuring systems with a resolution equal to or better (less) than 0.2 µm within a measuring range up to 0.2 mm;
2. Linear variable differential transformer (LVDT) systems having both of the following characteristics:
a. Linearity equal to or better (less) than 0.1% within a measuring range up to 5 mm; and
b. Drift equal to or better (less) than 0.1% per day at a standard ambient test room temperature ± 1 K;
3. Measuring systems having both of the following characteristics:
a. Contain a laser; and
b. Maintain for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and a standard pressure:
1. A resolution over their full scale of 0.1 µm or better; and
2. With a measurement uncertainty equal to or better (less) than (0.2 + L/2000) µm (L is the measured length in millimetres);
Note: Item 4A003b3 does not control measuring interferometer systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimensional inspection machines, or similar equipment.
Technical Note: In Item 4A003b ‘linear displacement’ means the change of distance between the measuring probe and the measured object.
c. Angular displacement measuring instruments having an angular position deviation equal to or better (less) than 0.00025°;
Note: Item 4A003c does not control optical instruments, such as autocollimators, using collimated light to detect angular displacement of a mirror.
d. Systems for simultaneous linear-angular inspection of hemi-shells, having both of the following characteristics:
1. Measurement uncertainty along any linear axis equal to or better (less) than 3.5 µm per 5 mm; and
2. Angular position deviation equal to or less than 0.02°.
Notes: 1. Item 4A003 includes machine tools that can be used as measuring machines if they meet or exceed the criteria specified for the measuring machine function.
2. Machines described in Item 4A003 are controlled if they exceed the threshold specified anywhere within their operating range.
Technical Note: All parameters of measurement values in this item represent plus/minus, i.e., not total band.
4A004 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:
a. Furnaces having all of the following characteristics:
1. Capable of operation at temperatures above 1123 K (850 °C);
2. Induction coils 600 mm or less in diameter; and
3. Designed for power inputs of 5 kW or more;
Note: Item 4A004a does not control furnaces designed for the processing of semiconductor wafers.
b. Power supplies, with a specified output power of 5 kW or more, specially designed for furnaces specified in Item 4A004a.
4A005 ‘Isostatic presses’, and related equipment, as follows:
a. ‘Isostatic presses’ as specified in 5A208;
b. Dies, moulds, and controls specially designed for the ‘isostatic presses’ specified in Item 4A005a.
Technical Notes:
1. In Item 4A005 ´Isostatic presses’ means equipment capable of pressurizing a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a work piece or material.
2. In Item 4A005 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
4A006 Vibration test systems, equipment, and components as follows:
a. Electrodynamic vibration test systems, having all of the following characteristics:
1. Employing feedback or closed loop control techniques and incorporating a digital control unit;
2. Capable of vibrating at 10 g RMS or more between 20 and 2000 Hz; and
3. Capable of imparting forces of 50 kN or greater measured ‘bare table’;
b. Digital control units, combined with software specially designed for vibration testing, with a real-time bandwidth greater than 5 kHz and being designed for a system specified in Item 4A006a;
c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force of 50 kN or greater measured ‘bare table’, which are usable for the systems specified in Item 4A006a;
d. Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force of 50 kN or greater, measured ‘bare table,’ which are usable for the systems specified in Item 4A006a.

Technical Note : In Item 4A006 ‘bare table’ means a flat table, or surface, with no fixtures or fittings.
4A007 Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment, as follows:
a. Arc re-melt and casting furnaces having both of the following characteristics:
1. Consumable electrode capacities between 1000 and 20000 cm3; and
2. Capable of operating with melting temperatures above 1973 K (1700 °C);
b. Electron beam melting furnaces and plasma atomisation and melting furnaces, having both of the following characteristics:
1. A power of 50 kW or greater; and
2. Capable of operating with melting temperatures above 1473 K (1200 °C);
c. Computer control and monitoring systems specially configured for any of the furnaces specified in Item 4A007a or 4A007b.
4A008 Crucibles made of materials resistant to liquid actinide metals, as follows:
a. Crucibles having both of the following characteristics:
1. A volume of between 150 cm3 (150 ml) and 8000 cm3 (8 litres); and
2. Made of or coated with any of the following materials, having a purity of 98% or greater by weight:
a. Calcium fluoride (CaF2);
b. Calcium zirconate (metazirconate) (CaZrO3);
c. Cerium sulphide (Ce2S3);
d. Erbium oxide (erbia) (Er2O3);
e. Hafnium oxide (hafnia) (HfO2);
f. Magnesium oxide (MgO);
g. Nitrided niobium-titanium-tungsten alloy (approximately 50% Nb, 30% Ti, 20% W);
h. Yttrium oxide (yttria) (Y2O3); or
i. Zirconium oxide (zirconia) (ZrO2);
b. Crucibles having both of the following characteristics:
1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres); and
2. Made of or lined with tantalum, having a purity of 99.9% or greater by weight;
c. Crucibles having all of the following characteristics:
1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres);
2. Made of or lined with tantalum, having a purity of 98% or greater by weight; and
3. Coated with tantalum carbide, nitride, boride, or any combination thereof.
4A009 Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.
4A010 Composite structures in the form of tubes having both of the following characteristics:
a. An inside diameter of between 75 and 400 mm; and
b. Made with any of the materials specified in Item 3A116.
4A011 Frequency changers or generators having all of the following characteristics:
a. Multiphase output capable of providing a power of 40 W or greater;
b. Capable of operating in the frequency range between 600 and 2000 Hz;
c. Total harmonic distortion better (less) than 10%; and
d. Frequency control better (less) than 0.1%.
Note: Frequency changers and generators especially designed or prepared for the gas centrifuge process are controlled under Prescribed Equipment (0B Category).
Technical Note: Frequency changers in Item 4A011 are also known as converters or inverters.
4A012 Lasers, laser amplifiers and oscillators as follows:
a. Copper vapour lasers having both of the following characteristics:
1. Operating at wavelengths between 500 and 600 nm; and
2. An average output power equal to or greater than 40 W;
b. Argon ion lasers having both of the following characteristics:
1. Operating at wavelengths between 400 and 515 nm; and
2. An average output power greater than 40 W;
c. Neodymium-doped (other than glass) lasers with an output wavelength between 1000 and 1100 nm having either of the following:
1. Pulse-excited and Q-switched with a pulse duration equal to or greater than 1 ns, and having either of the following:
a. A single-transverse mode output with an average output power greater than 40 W; or
b. A multiple-transverse mode output with an average output power greater than 50 W;
or
2. Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of greater than 40 W;
d. Tuneable pulsed single-mode dye laser oscillators having all of the following characteristics:
1. Operating at wavelengths between 300 and 800 nm;
2. An average output power greater than 1 W;
3. A repetition rate greater than 1 kHz; and
4. Pulse width less than 100 ns;
e. Tuneable pulsed dye laser amplifiers and oscillators having all of the following characteristics:
1. Operating at wavelengths between 300 and 800 nm;
2. An average output power greater than 30 W;
3. A repetition rate greater than 1 kHz; and
4. Pulse width less than 100 ns;
Note: Item 4A012e does not control single mode oscillators.
f. Alexandrite lasers having all of the following characteristics:
1. Operating at wavelengths between 720 and 800 nm;
2. A bandwidth of 0.005 nm or less;
3. A repetition rate greater than 125 Hz; and
4. An average output power greater than 30 W;
g. Pulsed carbon dioxide lasers having all of the following characteristics:
1. Operating at wavelengths between 9000 and 11000 nm;
2. A repetition rate greater than 250 Hz;
3. An average output power greater than 500 W; and
4. Pulse width of less than 200 ns;
Note: Item 4A012g does not control the higher power (typically 1 to 5 1kW) industrial CO2 lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns.
h. Pulsed excimer lasers (XeF, XeCl, KrF) having all of the following characteristics:
1. Operating at wavelengths between 240 and 360 nm;
2. A repetition rate greater than 250 Hz; and
3. An average output power greater than 500 W;
i. Para-hydrogen Raman shifters designed to operate at 16 µm output wavelength and at a repetition rate greater than 250 Hz.
4A013 Valves having all of the following characteristics:
a. A nominal size of 5 mm or greater;
b. Having a bellows seal; and
c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60% nickel by weight.
Technical Note: For valves with different inlet and outlet diameter, the nominal size parameter in Item 4A013a refers to the smallest diameter.
4A014 Superconducting solenoidal electromagnets having all of the following characteristics:
a. Capable of creating magnetic fields greater than 2 T;
b. A ratio of length to inner diameter greater than 2;
c. Inner diameter greater than 300 mm; and
d. Magnetic field uniform to better than 1% over the central 50% of the inner volume.
Note: Item 4A014 does not control magnets specially designed for and exported as part of medical nuclear magnetic resonance (NMR) imaging systems. (‘As part of’ does not necessarily mean physical part in the same shipment. Separate shipments from different sources are allowed, provided the related export documents clearly specify the ‘as part of” relationship.)
4A015 High-power direct current power supplies having both of the following characteristics:
a. Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and
b. Current or voltage stability better than 0.1% over a time period of 8 hours.
4A016 High-voltage direct current power supplies having both of the following characteristics:
a. Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and
b. Current or voltage stability better than 0.1% over a time period of 8 hours.
4A017 Pressure transducers capable of measuring absolute pressures at any point in the range 0 to 13 kPa and having both of the following characteristics:
a. Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel, or nickel alloy with more than 60% nickel by weight; and
b. Having either of the following characteristics:
1. A full scale of less than 13 kPa and an accuracy of better than ± 1% of full scale; or
2. A full scale of 13 kPa or greater and an accuracy of better than ± 130 Pa.
Technical Notes:
1. In Item 4A017 pressure transducers are devices that convert pressure measurements into an electrical signal.
2. In Item 4A017 accuracy includes non-linearity, hysteresis and repeatability at ambient temperature.
4A018 Vacuum pumps having all of the following characteristics:
a. Input throat size equal to or greater than 380 mm;
b. Pumping speed equal to or greater than 15 m3/s; and
c. Capable of producing an ultimate vacuum better than 13.3 mPa.
Technical Notes:
1. The pumping speed is determined at the measurement point with nitrogen gas or air.
2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.
4A019 Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.
4A020 Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:
a. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;
Note: Item 4A020a includes precision mandrels, clamps, and shrink fit machines.
b. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;
Technical Note: In Item 4A020b such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.
c. Bellows-forming mandrels and dies for producing single -convolution bellows.
Technical Note: The bellows referred to in Item 4A020c have all of the following characteristics:
1. Inside diameter between 75 and 400 mm;
2. Length equal to or greater than 12.7 mm;
3. Single convolution depth greater than 2 mm; and
4. Made of high-strength aluminium alloys, maraging steel, or high strength fibrous or filamentary materials.
4A021 Centrifugal multi-plane balancing machines, fixed or portable, horizontal or vertical, as follows:
a. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:
1. Swing or journal diameter greater than 75 mm;
2. Mass capability of from 0.9 to 23 kg; and
3. Capable of balancing speed of revolution greater than 5000 rpm;
b. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:
1. Journal diameter greater than 75 mm;
2. Mass capability of from 0.9 to 23 kg;
3. Capable of balancing to a residual imbalance equal to or less than 0.010 kg x mm/kg per plane; and
4. Belt drive type.
4A022 Filament winding machines and related equipment, as follows:
a. Filament winding machines as specified in 5A206.
b. Coordinating and programming controls for the filament winding machines specified in Item 4A022a;
c. Precision mandrels for the filament winding machines specified in Item 4A022a.
4A023 Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.
Notes:
1. Item 4A023 includes separators capable of enriching stable isotopes as well as those for uranium.
2. A separator capable of separating the isotopes of lead with a one-mass unit difference is inherently capable of enriching the isotopes of uranium with a three-unit mass difference.
3. Item 4A023 includes separators with the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.
Technical Note: A single 50 mA ion source cannot produce more than 3 g of separated highly enriched uranium (HEU) per year from natural abundance feed.
4A024 Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:
a. Inductively coupled plasma mass spectrometers (ICP/MS);
b. Glow discharge mass spectrometers (GDMS);
c. Thermal ionisation mass spectrometers (TIMS);
d. Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to UF6;
e. Molecular beam mass spectrometers having either of the following characteristics:
1. A source chamber constructed from, lined with or plated with stainless steel or molybdenum, and equipped with a cold trap capable of cooling to 193 K (-80 °C) or less; or
2. A source chamber constructed from, lined with or plated with materials resistant to UF6;
f. Mass spectrometers equipped with a micro-fluorination ion source designed for actinides or actinide fluorides.
Note: Mass spectrometers especially designed or prepared for analyzing on-line samples of uranium hexafluoride are controlled under Prescribed Equipment (0B Category).
4A025 Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:
a. Made of phosphor bronze mesh chemically treated to improve wettability; and
b. Designed to be used in vacuum distillation towers.
4A026 Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:
a. Airtight (i.e., hermetically sealed);
b. A capacity greater than 8.5 m3/h; and
c. Either of the following characteristics:
1. For concentrated potassium amide solutions (1% or greater), an operating pressure of 1.5 to 60 MPa; or
2. For dilute potassium amide solutions (less than 1%), an operating pressure of 20 to 60 MPa.
4A027 Turbo-expanders or turbo-expander-compressor sets having both of the following characteristics:
a. Designed for operation with an outlet temperature of 35 K (- 238 ºC) or less; and
b. Designed for a throughput of hydrogen gas of 1000 kg/h or greater.
4A028 Water-hydrogen sulphide exchange tray columns and internal contactors, as follows:
a. Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:
1. Can operate at pressures of 2 MPa or greater;
2. Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and
3. With a diameter of 1.8 m or greater;
b. Internal contactors for the water-hydrogen sulphide exchange tray columns specified in Item 4A028a.
Note: For columns which are especially designed or prepared for the production of heavy water, see Prescribed Equipment (0B002).
Technical Note: Internal contactors of the columns are segmented trays which have an effective assembled diameter of 1.8 m or greater; are designed to facilitate counter current contacting and are constructed of stainless steels with a carbon content of 0.03% or less. These may be sieve trays, valve trays, bubble cap trays or turbo grid trays.
4A029 Hydrogen-cryogenic distillation columns having all of the following characteristics:
a. Designed for operation at internal temperatures of 35 K (-238 ºC) or less;
b. Designed for operation at internal pressures of 0.5 to 5 MPa;
c. Constructed of either:
1. Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or
2. Equivalent materials which are both cryogenic and H2-compatible; and
d. With internal diameters of 1 m or greater and effective lengths of 5 m or greater.
4A030 Ammonia synthesis converters or synthesis units, in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen high-pressure exchange column and the synthesized ammonia is returned to said column.
4B Equipment, assemblies and components, including test and measurement equipment usable in development of nuclear explosive devices
4B001 Photomultiplier tubes having both of the following characteristics:
a. Photocathode area of greater than 20 cm2; and
b. Anode pulse rise time of less than 1 ns.
4B002 Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:
a. An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and
b. With a figure of merit (K) of 0.25 or greater;
or
a. An accelerator peak electron energy of 25 MeV or greater; and
b. A peak power greater than 50 MW.
Note: Item 4B002 does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes.
Technical Notes:
1. The figure of merit K is defined as: K=1.7 x 103 V2.65Q. V is the peak electron energy in million electron volts. If the accelerator beam pulse duration is less than or equal to 1 µs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 µs, then Q is the maximum accelerated charge in 1 µs. Q equals the integral of i with respect to t, over the lesser of 1 µs or the time duration of the beam pulse ( Q=?idt ) where i is beam current in amperes and t is the time in seconds.
2. Peak power = (peak potential in volts) x (peak beam current in amperes).
3. In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 µs or the duration of the bunched beam packet resulting from one microwave modulator pulse.
4. In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.
4B003 Multistage light gas guns or other high-velocity gun systems (coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 2 km/s or greater.
4B004 Mechanical rotating mirror cameras, as follows, and specially designed components therefor:
a. Framing cameras with recording rates greater than 225000 frames per second;
b. Streak cameras with writing speeds greater than 0.5 mm/µs.
Note: In Item 4B004 components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors, and bearings.
4B005 Electronic streak cameras, electronic framing cameras, tubes and devices, as follows:
a. Electronic streak cameras capable of 50 ns or less time resolution;
b. Streak tubes for cameras specified in Item 4B005a;
c. Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time;
d. Framing tubes and solid-state imaging devices for use with cameras specified in Item 4B005c, as follows:
1. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance;
2. Gate silicon intensifier target (SIT) vidicon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate;
3. Kerr or Pockels cell electro-optical shuttering;
4. Other framing tubes and solid-state imaging devices having a fast image gating time of less than 50 ns specially designed for cameras specified in Item 4B005c.
4B006 Specialized instrumentation for hydrodynamic experiments, as follows:
a. Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 µs;
b. Manganin gauges for pressures greater than 10 GPa;
c. Quartz pressure transducers for pressures greater than 10 GPa.
Note: Item 4B006a includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).
4B007 High-speed pulse generators having both of the following characteristics:
a. Output voltage greater than 6 V into a resistive load of less than 55 ohms; and
b. ‘Pulse transition time’ less than 500 ps.
Technical Note: In Item 4B007b ‘pulse transition time’ is defined as the time interval between 10% and 90% voltage amplitude.
4B008 Detonators and multipoint initiation systems, as follows:
a. Electrically driven explosive detonators, as follows:
1. Exploding bridge (EB);
2. Exploding bridge wire (EBW);
3. Slapper;
4. Exploding foil initiators (EFI);
b. Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over an area greater than 5000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2.5 µs.
Note: Item 4B008 does not control detonators using only primary explosives, such as lead azide.
Technical Note: In Item 4B008 the detonators of concern all utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper types, the exploding conductor starts a chemical detonation in a contacting high-explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator.
4B009 Firing sets and equivalent high-current pulse generators, as follows:
a. Explosive detonator firing sets designed to drive multiple controlled detonators specified by Item 4B008 above;
b. Modular electrical pulse generators (pulsers) having all of the following characteristics:
1. Designed for portable, mobile, or ruggedized-use;
2. Enclosed in a dust-tight enclosure;
3. Capable of delivering their energy in less than 15 µs;
4. Having an output greater than 100 A;
5. Having a ‘rise time’ of less than 10 µs into loads of less than 40 ohms;
6. No dimension greater than 25.4 cm;
7. Weight less than 25 kg ; and
8. Specified to operate over an extended temperature range of 223º to 373º K (-50 ºC to 100 ºC) or specified as suitable for aerospace applications.
Note: Item 4B009b includes xenon flashlamp drivers.
Technical Note: In Item 4B009b5 ‘rise time’ is defined as the time interval from 10% to 90% current amplitude when driving a resistive load.
4B010 Switching devices as follows:
a. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:
1. Containing three or more electrodes;
2. Anode peak voltage rating of 2.5 kV or more;
3. Anode peak current rating of 100 A or more; and
4. Anode delay time of 10 µs or less;
Note: Item 4B010a includes gas krytron tubes and vacuum sprytron tubes.
b. Triggered spark-gaps having both of the following characteristics:
1. Anode delay time of 15 µs or less; and
2. Rated for a peak current of 500 A or more;
c. Modules or assemblies with a fast switching function having all of the following characteristics:
1. Anode peak voltage rating greater than 2 kV;
2. Anode peak current rating of 500 A or more; and
3. Turn-on time of 1 µs or less.
4B011 Pulse discharge capacitors having either of the following sets of characteristics:
a. 1. Voltage rating greater than 1.4 kV;
2. Energy storage greater than 10 J;
3. Capacitance greater than 0.5 µF; and
4. Series inductance less than 50 nH;
or
b. 1. Voltage rating greater than 750 V;
2. Capacitance greater than 0.25 µF; and
3. Series inductance less than 10 nH.
4B012 Neutron generator systems, including tubes, having both of the following characteristics:
a. Designed for operation without an external vacuum system; and
b. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction.
4C Technology
Technology for the development, production or use of items in 4A and 4B.]
5 Aerospace systems, equipment including production and test equipment, related technology, and specially designed components and accessories therefor
5A Rocket Systems (including ballistic missiles, space launch vehicles and sounding rockets)
5A1 Systems
5A101 Systems for missiles and rockets, including:
a. complete rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets);
b. complete rocket stages with engines;
c. solid or liquid fuel rocket engines and their control systems including liquid propellant apogee engines designed or modified for satellites.
Note: 5A101 does not control JATO units, propulsion units for flares, ejection seats, emergency escape equipment and rockets for display fireworks.
5A102

Subsystems and components usable in missiles and rockets including:
a. rocket motor cases, interior lining, insulation and nozzles;
b. rocket staging mechanisms, separation mechanisms and inter-stages;

c. Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in missiles and rockets, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.

Notes:

1. The only servo valves, pumps and gas turbines specified in 3.A.5. are the following:

1.1. Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms.

1.2. Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 rpm at the maximum operating mode or with discharge pressures equal to or greater than 7 MPa

1.3. Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to or greater than 8,000 rpm at the maximum operating mode.

2. Systems and components specified in this clause may be exported as part of a satellite;

(Above clause c. has been substituted vide NOTIFICATION NO. 116/2013, DT. 13/03/2015)

[OLD-

c. liquid and slurry propellant (including oxidizers), control systems, and components thereof, specially designed or modified for resistance to vibration;]
d. re-entry vehicles and equipment including
1. Heat-shields and components thereof, fabricated of ceramic or ablative materials;
2. Heat sinks and components thereof, fabricated of light weight, high heat capacity materials;
3. Electronic equipment specially designed for re-entry vehicles.
e. guidance systems and their components such as gyros and inertial reference units;
f. thrust-vector control subsystems including methods of achieving thrust vector control such as flexible nozzle, fluid or secondary gas injection, movable engine or nozzle, deflection of exhaust gas stream (jet vanes or probes) and use of thrust tabs;
g. hybrid rocket motors and components thereof;
h. safing, arming, fusing and firing mechanisms for weapons or warhead;
i. software specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.

j. Combustion chambers and nozzles for liquid propellant rocket engines;

(Above clause j. has been added vide NOTIFICATION NO. 116/2013, DT. 13/03/2015)
5A2 Production and Test Equipment
5A201 Transonic, supersonic, hypersonic wind tunnels; shock tunnels; gun tunnels; aeroballistic ranges.
5A202 Test and production equipment and facilities designed to handle systems in 5A1.
5A203 Test benches/stands, usable for complete rocket systems and subsystems (including ballistic missile systems, space launch vehicles and sounding rockets) which have the capacity to handle solid or liquid propellant rockets, motors or engines, or which are capable of simultaneously measuring the three axial thrust components.
5A204 Vibration test equipment (vibration test systems and vibration thrusters) and components using digital control techniques and feedback or closed loop test equipment and software thereof (Refer 4A006).
5A205 Flow-forming machines and specially designed components thereof which, according to the manufacturers technical specification,
1. can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and
2. have more than two axes which can be coordinated simultaneously for contouring control.
Note: Item 5A205 includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
5A206 Filament winding machines or fibre placement machines for which the motion for positioning wrapping and winding fibres can be coordinated and programmed in two or more axes; precision mandrels thereof, and coordinating and programming controls.
5A207 Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes;
5A208 Isostatic presses having all of the characteristics of maximum working pressure equal to or greater than 69 MPa or greater; designed to achieve and maintain a controlled thermal environment of 600oC or greater; and possessing a chamber cavity with an inside diameter of 152 mm or greater.
5A209 Environmental chambers simulating vibration environments, with altitudes equal to or greater than 15 km, or temperature ranging between minus 50 and plus 125 degrees centigrade.
5A210 Environmental chambers simulating acoustic pressure level of 140 dB or greater or rated acoustic power output of 4 KW or greater, with altitudes equal to or greater than 15 km, or temperature ranging between minus 50 and plus 125 degrees centigrade.
5A211 Accelerators delivering electro-magnetic radiation produced by Bremsstrahlung from accelerated electrons.
5A212 Pulsed electron accelerators
5A213 Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 or better and having all the following characteristics:
a. An inner ring bore diameter between 12 and 50 mm;
b. An outer ring outside diameter between 25 and 100 mm; and
c. A width between 10 and 20 mm.
5A214 Liquid propellant tanks specially designed for the propellants controlled in Item 3A3 or other liquid propellants used in the systems specified in 5A and 5B.
5A215 Production facilities and production equipment specially designed for equipment or materials for 5A101 and 5A102.
5A216 Production equipment and specially designed components thereof, for the production, handling or acceptance testing of liquid propellants or propellant constituents as referred in 3A3;
5A217 Launch and ground support equipment and facilities usable for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned airborne system and cruise missiles as follows:-
a. apparatus, devices and vehicles, designed or modified for the transport, handling, control, activation and launching of the systems.
b. gravity meters (gravimeters), gravity gradiometers, and specially designed components thereof, designed or modified for airborne or marine use usable for complete rocket systems and for complete unmanned aerial vehicle systems (including cruise missile systems target drones and reconnaissance drones)
c. telemetry and tele-command equipment, including ground equipment, designed or modified for complete rocket systems and complete unmanned aerial vehicle systems and cruise missiles, excluding equipment designed or modified for manned aircraft or satellites, ground based equipment designed or modified for terrestrial or marine application, and equipment designed for commercial, civil or ‘safety of life’ (e.g. data integrity, flight safety) GNSS services.
d. radomes designed to withstand a combined thermal and pressure shock usable in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (eg. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
e. Software which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path.
f. Thermal batteries designed or modified for complete rocket systems of 5A or complete unmanned aerial vehicles of 5B
Note: ‘Thermal batteries’ are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.
5A218 Systems, specially designed for radar cross section measurement, usable for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned airborne system and cruise missiles and their subsystems.
5A3 Technology
5A301 Technology related to the development, production, testing and use of items in 5A1 and 5A2.
5A302 Software for the development, production, and testing and use of items in 5A1 and 5A2.
5A303 Software which coordinates the function of more than one subsystem, specially designed or modified for use in the systems specified in 5A1 and 5A2.
5B Unmanned aerial vehicles including cruise missiles, target drones and reconnaissance drones and related equipment, and specially designed components therefor:
a. Unmanned aerial vehicles including Remotely Piloted air Vehicles (RPVs) and autonomous programmable vehicles;
b. Associated launchers and ground support equipment;
c. Related equipment for command and control;
d. Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones);
e. Light weight Turbojet and turbofan engines (including turbo compound engines);.
f. Ramjet / Scramjet / pulse jet/ combined cycle engines, including devices to regulate combustion, and specially designed components;
g. Complete unmanned aerial vehicle systems having an autonomous flight control and navigation capability or capability of controlled flight out of the direct vision range involving a human operator, designed or modified to incorporate an aerosol dispensation mechanism, or capable of carrying elements of a payload in the form of a particulate or liquid other than fuel components of such vehicles;
Note: This category does not control unpowered airborne vehicles such as gliders, hot air balloons etc.;
h. Safing, arming, fusing and firing mechanisms for weapons or warhead;
i Production facilities and Production equipment specially designed for equipment or materials for 5;.
j. Technology, for the development, production or use of equipment, materials or software specified for 5B;
k. Software, for the development, production or use of equipment or materials specified for 5B;
l. Software which coordinates the function of more than one subsystem, specially designed or modified for use in the systems specified in 5B;
m. ‘Turboprop engine systems’ specially designed for the systems in 5B.d, and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level standard conditions), excluding civil certified engines.
Note: For the purposes of this entry, a ‘turboprop engine system’ incorporates all of the following:
i. Turboshaft engine; and
ii. Power transmission system to transfer the power to a propeller.
5C Avionics and navigation systems designed or modified for use in, or usable in rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles
5C001 Guidance systems and their components such as gyros and inertial reference units, and specially designed components therefor;
5C002 Integrated flight instrument systems which include gyrostabilizers or automatic pilots, and specially designed components therefor;
5C003 Compasses (including gyro-astro compasses), gyroscopes, accelerometers and inertial equipment and specially designed software thereof and specially designed components therefor.
5C004 Inertial or other equipment using accelerometers or systems incorporating such equipment, and specially designed integration software therefor;
5C005 Encrypted telemetry systems, equipment and software thereof.
5C006 Flight control system (including servo valves) designed or modified for the systems as follows:
a. Hydraulic, mechanical, electro-optical or electro-mechanical flight control systems (including fly-by-wire systems);
b. Attitude control equipment;
c. Design technology for integration of flight control, guidance, and propulsion data into a flight management system for optimisation of rocket system trajectory;
d. Specially designed test, calibration, and alignment thereof.
5C007 1. Integrated navigation system incorporating an inertial measurement device (example: an attitude and heading reference system, inertial reference unit, or inertial navigation system); one or more external sensor used to update the position and/or velocity, either periodically or continuously throughout the flight (example: satellite navigation receiver, radar altimeter and/or Doppler radar); integration hardware and software.
2. Three axis magnetic heading sensors having all of the following characteristics, and specially designed components therefor:
a. Internal tilt compensation in pitch (+/- 90 degrees) and having roll (+/- 180 degrees) axes.
b. Capable of providing azimuthal accuracy better (less) than 0.5 degrees rms at latitudes of +/- 80 degrees, referenced to local magnetic field; and
c. Designed or modified to be integrated with flight control and navigation systems.
Note: Flight control and navigation systems in this item include gyrostabilizers, automatic pilots and inertial navigation systems.
5C008 Production equipment and other test, calibration and alignment equipment, designed or modified to be used with equipment specified in 5C001 – 5C004 and 5C007.
5C009 Equipment used to characterize mirrors for laser gyros such as scatterometer, reflectometer and profilometer and for other inertial equipments such as Inertial measurement unit (IMU Module) tester, IMU Platform tester, IMU stable element handling fixture, Gyro tuning test station, Gyro dynamic balance station, Gyro run-in/motor test station, Gyro evacuation and filling station, Centrifuge fixture for gyro bearings, Accelerometer axis align station, Accelerometer test station and Fiber Optic Gyro Coil Winding Machines. [OLD- and Accelerometer test station.]

(In above 5C009 the figure and words ", Accelerometer test station and Fiber Optic Gyro Coil Winding Machines" has been substituted vide NOTIFICATION NO. 116/2013, DT. 13/03/2015)
5C010 Avionics equipment and embedded or specially designed software and components thereof, including but not limited to:
a. Radar and laser radar system including altimeter;
b. Electronic assemblies and components including umbilical and interstage electrical connectors
Technical Note: Interstage connectors also include electrical connectors installed between systems and their payload.
c. Design technology for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards from external sources.
d. Passive sensors for determining bearings to electromagnetic sources (direction finding devices) or terrain characteristics
e. Receiving equipment for Global Navigation Satellite Systems (GNSS: e.g. GPS, GLONASS, GALILEO), capable of operating at aircraft speeds and altitudes or above.
f. Terrain contour mapping equipment, Scene mapping and correlation (both digital and analogue) equipment, Doppler navigation radar equipment, Passive interferometer equipment and Imaging sensor equipment (both active and passive)
g. Design technology for electromagnetic shielding systems, the configuration of hardened electrical circuits and subsystems and for the determination of hardening criteria.
5C011 On-board electronic equipment, devices and their design and manufacturing know-how (except warhead fuses, timers and sequencers), and embedded or specially designed software thereof.
5C012 Detectors designed or modified, in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (eg. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
5C013 Radiation Hardened microcircuits usable in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (e.g. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
5C014 Precision tracking systems using a code translator installed on the rocket or unmanned aerial vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurement of inflight position and velocity; Range instrumentation radars including associated optical/infrared trackers and related software.
5C015 Balancing machines capable of balancing rotors/assemblies and correcting unbalance in two planes or more.
5C016 Indicator heads or balancing instrumentation designed or modified for use with balancing machines.
5C017 Motion simulators or rate tables having all of the following characteristics:
a. Two axes or more;
b. Designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both; and
c. Having any of the following characteristics:
1. For any single axis having all of the following:
a. Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and
b. A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0.6 degrees/s;
2. Having a worst-case rate stability equal to or better (less) than plus or minus 0.05 % averaged over 10 degrees or more; or
3. A positioning ‘accuracy’ equal to or less (better) than 5 arc second.
Note 1: 5C017 does not control rotary tables designed or modified for machine tools or for medical equipment.
Note 2: Motion simulators or rate tables specified in 5C017 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export.
5C018 Position tables (equipment capable of precise rotary positioning in any axes) having two axes or more and a position accuracy equal to or better than 5 arc second.
5C019 Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both.
Note: Centrifuges specified in 5C019 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export.
5C020 Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces designed or modified for the unmanned aerial vehicle systems to optimize aerodynamic performance throughout the flight regime of an unmanned aerial vehicle system.
5C021 Design technology for integration of the flight control, guidance, and propulsion data into a flight management system, designed or modified for the complete rocket systems, unmanned aerial vehicles and cruise missiles for optimization of the trajectory.
5C022 Technology for the development, production, or use of items in 5C.
5C023 Software for the development, production and use of items in 5C.
5C024 Software specially designed or modified for use in the systems specified in 5C.
5D Manned-aircraft, aero-engines, related equipment and components:
Note: This category does not control foreign military aircraft or an Indian aircraft carrying a military registration number.
5D001 Combat aircraft and specially designed components thereof;
a. Other aircraft specially designed or modified for military use, including military reconnaissance, assault, military training, transporting and air-dropping troops or military equipment, logistics support, and specially designed components thereof;
b. Aero-engines specially designed or modified for military use, and specially designed components thereof;
c. Airborne equipment, including airborne refuelling equipment, specially designed for use with the aircraft controlled by 5D001a or 5D001b or the aero-engines controlled by 5D001c, and specially designed components thereof;
d. Pressure refuellers, pressure refuelling equipment, equipment specially designed to facilitate operations in confined areas and ground equipment, developed specially for aircraft controlled by 5D001a or 5D001b or for aero-engines controlled by 5D001c;
e. Pressurized breathing equipment and partial pressure suits for use in aircraft anti-g suits, military crash helmets and protective masks, liquid oxygen converters used for aircraft or missiles, and catapults and cartridge actuated devices for emergency escape of personnel from aircraft;
f. Parachutes:
1. Paragliders, drag parachutes, drogue parachutes for stabilization and attitude control of dropping bodies, (e.g. recovery capsules, ejection seats, bombs);
2. Drogue parachutes for use with ejection seat systems for deployment and inflation sequence regulation of emergency parachutes;
3. Recovery parachutes for guided missiles, drones or space vehicles;
4. Approach parachutes and landing deceleration parachutes.
g. Automatic piloting systems for parachuted loads, equipment specially designed or modified for military use for controlled opening jumps at any height, including oxygen equipment.
Note 1: 5D001b does not control aircraft or variants of those aircraft specially designed for military use which:
1. Have been certified for civil use by the civil aviation authority of India, and
2. Are not configured for military use and are not fitted with equipment or attachments specially designed or modified for military use;
Note 2: The control in 5D001b and 5D001c on specially designed components and related equipment for non-military aircraft or aero-engines modified for military use applies only to those military components and to military related equipment required for the modification to military use.
5E Microlight aircraft and powered ‘hang-gliders’
Category 6 [Reserved]
Category 7: Electronics, computers, and information technology including information security
7A Electronics
7A001 High-power microwave devices including tubes, travelling wave tubes (TWT) and phase shifters, and continuous wave and pulsed high power microwave travelling wave tube amplifiers (TWTA) operating at frequencies higher than 31 GHz, and their power supplies.
7A002 Microwave monolithic integrated circuits (MMIC) operating at frequencies above 3 GHz and surface acoustic wave (SAW) devices operating at frequencies above 2.5 GHz.
7A003 Phased array antennas and their elements.
7A004 Radiation-hardened microprocessors, field programmable gate arrays and solid state memory devices.
7A005 Microprocessor microcircuits, microcomputer microcircuits, microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converter, and digital-to-analogue converter, printed circuit boards or modules, electro-optical or optical integrated circuits designed for signal processing, field programmable logic devices, neural network integrated circuits, custom integrated circuits for which either the function is unknown or the control status of the equipment in which the integrated circuit will be used is unknown, Fast Fourier Transform (FFT) processors, electrical erasable programmable read-only memories (EEPROMs), flash memories or static random-access memories (SRAMs), having any of the following:
a. Rated for operation at an ambient temperature above 398 K (+125°C);
b. Rated for operation at an ambient temperature below 218 K (-55°C); or
c. Rated for operation over the entire ambient temperature range from 218 K (-55°C) to 398 K (+125°C).
7A006 Radiation-hardened analogue-to-digital and digital-to-analogue converter integrated circuits, as follows:
a. Analogue-to-digital converters having any of the following:
1. A resolution of 8 bit or more, but less than 12 bit, with a total conversion time of less than 5 ns;
2. A resolution of 12 bit with a total conversion time of less than 200 ns; or
3. A resolution of more than 12 bit with a total conversion time of less than 2 µs;
b. Digital-to-analogue converters with a resolution of 12 bit or more, and a settling time of less than 10 ns.
7A007 Detector units operating in the thermal infrared, ultraviolet, x-ray and gamma ray spectrum.
7A008 Focal plane assemblies for imaging cameras operating in the visible, near and thermal infrared spectrum.
7A009 Technology for the development, production or use of items specified in 7A005 and 7A006.
7A010

Analogue-to-digital converters, usable in the systems specified in 5A, having any of the following characteristics:

a. Designed to meet military specifications for ruggedised equipment; or

b. Designed or modified for military use and being any of the following types:

1. Analogue-to-digital converter microcircuits, which are radiation-hardened or have all of the following characteristics:

1.1. Rated for operation in the temperature range from below -54oC to above +125oC; and

1.2. Hermetically sealed;
 

or
2. Electrical input type analogue-to-digital converter printed circuit boards or modules, having all of the following characteristics:

2.1. Rated for operation in the temperature range from below -45oC to above +80oC; and

2.2. Incorporating microcircuits specified in 7A010.b.1.
7B Electronic test equipment
7B001 Frequency synthesized signal generators with maximum frequency greater than 31 GHz.
7B002 Network analysers operating at frequencies above 40 GHz.
7C Computers
7C001 Digital computers and software as follows:
a. Digital computers having a composite theoretical performance (CTP) exceeding 75000 (seventy-five thousand) million theoretical operations per second (Mtops)
b. Software, and/or computer inter-connection schemes, whether or not co-supplied with (a) designed to ‘parallelise’ digital computers (individually of any CTP rating) enabling a CTP of more than 75000 Mtops to be achieved by the ‘parallelised’ configuration.
Technical notes:
1. The Composite Theoretical Performance (CTP) rating is to be calculated in accordance with the calculation scheme separately notified in this regard.
2. Individual digital computers each with a CTP rating of 75000 Mtops or less do not require an export license to any destination or end-user, unless supplied with (b) above.
3. Digital Computers’ includes (1) hybrid computers incorporating ‘digital computers’ or specified in (a) above, systolic array computers, neural computers, optical computers, vector processors, digital signal processors, logical processors (2) digital electronic equipment designed for ‘image enhancement’ or signal processing other than when supplied as integral adjuncts to medical imaging (eg CAT-scanning) equipment.
7C002 Analogue, digital or hybrid computers, digital differential analysers, and specially designed software therefor, for use in, or for modelling, simulation, or design integration of rocket systems, unmanned aerial vehicles and cruise missiles.
7C003 Technology for the development, production or use of items in 7C002.
7D Information technology including information security
7D001 Data processing security equipment, data security equipment and transmission and signalling line security equipment, using ciphering processes.
7D002 Identification, authentication and keyloader equipment and key management, manufacturing and distribution equipment.
7E [Reserved]

(Amendments/additions to Categories 2, 3, 5 & 7 of SCOMET list [Appendix 3 to Schedule 2 of ITC(HS) Classification of Export & Import Items]

2A029 TO 2A031, 2B006, 2D054 TO 2D069, 2F018 TO 2F026, 2G025 TO 2G028, 7A010  - ADDED AND 3A301, 3A303, 3B016 - SUBSTITUTED, 5A102, 5C009 - AMENDED  vide NOTIFICATION NO. 116/2013, DT. 13/03/2015)

(Above Appendix 3 vide Annexure to Notification No. 37(RE-2012)/2009-2014 Dated 14.03.2013)

 [ OLD - Annexure to the
Notification No. 111/RE(2010)/2009-2014 dated 18.4.2012
 

 

ITC (HS), 2012 CONTENTS


 

Export of Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) listed below shall be permitted only against an export licence issued in this behalf unless export is prohibited or is permitted without licence subject to fulfillment of conditions, if any, as indicated under/against any specific category or item.

Provisions of Chapter IV A of the FT(D&R) Act,1992 as amended in 2010 shall apply to the goods, services and technologies as specified in the list below.

Supply of SCOMET Items from DTA to SEZ

No export permission is required for supply of SCOMET items from DTA to SEZ. However, all supplies of SCOMET items from DTA to SEZ will be reported to the Development Commissioner of the respective SEZ by the supplier in the prescribed proforma (Annexure 1) within one (1) week of the supplies getting effected. An annual report of such supplies from DTA to SEZ shall be sent to SCOMET Cell, DGFT (Hqrs), Department of Commerce, Udyog Bhawan, Maulana Azad Road, New Delhi-110011, by the Development Commissioner (DC), SEZ in the prescribed proforma (Annexure 2) . Report by the DC, SEZ to be filed by 15th May of every financial year for the supplies effected during the preceding financial year.

Export of SCOMET Items from SEZ to outside the country

Export permission is required if the SCOMET items are to be physically exported outside the country from SEZ i.e. to another country (Refer Rule 26 of the SEZ Rules, 2006).

(Inserted vide Notification No.93(RE-2010)/2009-14 dated 6.1.2012)

It is mandatory for all companies and their subsidiaries registered in India and all other business entities operating in India and involved in the manufacture, processing and use of Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) listed below to obtain permission of the Central Government before entering into any arrangement or understanding that involves an obligation to facilitate or undertake site visits, on-site verification or access to records/ documentation, by foreign Governments or foreign third parties, either acting directly or through an Indian party or parties. Requests for such permissions shall be considered in the manner in which requests for export/import licence are considered.

Provided that where obligations involving site visits, on-site verification or access to records/ documentation by foreign governments or foreign third parties are to be undertaken pursuant to a bilateral agreement or a multilateral treaty to which India is a party, the provisions of the relevant agreement or treaty shall apply.

Exporters are advised to refer to the relevant guidelines relating to the export of SCOMET items in the Handbook of Procedures (Vol.I), as issued from time to time.

Glossary: Expressions used in the SCOMET List have the following meanings:

“Accuracy” usually measured in terms of inaccuracy, means the maximum deviation, positive or negative, of an indicated value from an accepted standard or true value.

“Active flight control systems” are systems that function to prevent undesirable “aircraft” and missile motions or structural loads by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control.

“Aircraft”: A fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tilt-wing airborne vehicle.

“Angular position deviation” means the maximum difference between angular position and the actual, very accurately measured angular position after the work piece mount of the table has been turned out of its initial position.

“Composite” means a “matrix” and an additional phase or additional phases consisting of particles, whiskers, fibres or any combination thereof, present for a specific purpose or purposes.

“Composite theoretical performance” (“CTP”) is a measure of computational performance given in millions of theoretical operations per second (Mtops), calculated using the aggregation of computing elements (CE).

“Contouring control” means two or more “numerically controlled” motions operating in accordance with instructions that specify the next required position and the required feed rates to that position. These feed rates are varied in relation to each other so that a desired contour is generated.

“CTP” is equivalent to “composite theoretical performance. “Designed or modified” describes equipment, parts or components which, as a result of “development,” or modification, have become endowed with specified properties that make them fit for a particular application.

“Development”: Activity related to all phases prior to “production” such as design, design research, design analysis, design concepts, assembly and testing of prototypes, pilot production schemes, design data, process of transforming design data into a product, configuration design, integration design, layouts.

“Digital computer” means equipment which can, in the form of one or more discrete variables, perform all of the following:

a. Accept data;

b. Store data or instructions in fixed or alterable (writable) storage devices;

c. Process data by means of a stored sequence of instructions which is modifiable; and

d. Provide output of data.

N.B.: Modifications of a stored sequence of instructions include replacement of fixed storage devices, but not a physical change in wiring or interconnections.

“Explosives”: Solid, liquid or gaseous substances or mixtures of substances which, in their application as primary, booster, or main charges in warheads, demolition and other applications, are required to detonate.

“Fibrous or filamentary materials” include:

a. Continuous “monofilaments”;

b. Continuous “yarns” and “rovings”;

c. “Tapes”, fabrics, random mats and braids;

d.Chopped fibres, staple fibres and coherent fibre blankets;

e. Whiskers, either monocrystalline or polycrystalline, of any length;

f. Aromatic polyamide pulp.

“Hybrid computer” means equipment which can perform all of the following:

a. Accept data;

b. Process data, in both analogue and digital representations; and

c. Provide output of data.

“Image enhancement” means the processing of externally derived information-bearing images by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform). This does not include algorithms using only linear or rotational transformation of a single image, such as translation, feature extraction, registration or false coloration.

“Information security” is all the means and functions ensuring the accessibility, confidentiality or integrity of information or communications, excluding the means and functions intended to safeguard against malfunctions. This includes cryptography, ‘cryptanalysis’, protection against compromising emanations and computer security.

N.B.: ‘Cryptanalysis’: analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text.

“Insulation” is applied to the components of a rocket motor, i.e. the case, nozzle, inlets, case closures, and includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.

“Interior lining” is suited for the bond interface between the solid propellant and the case or insulating liner. Usually a liquid polymer based dispersion of refractory or insulating materials, e.g. carbon filled hydroxyl terminated polybutadiene (HTPB) or other polymer with added curing agents sprayed or screeded over a case interior.

“Isolated live cultures” includes live cultures in dormant form and in dried preparations.

“Isostatic presses” mean equipment capable of pressurising a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a workpiece or material.

“Laser”: An assembly of components which produce both spatially and temporally coherent light that is amplified by stimulated emission of radiation.

“Linearity” (usually measured in terms of non-linearity) means the maximum deviation of the actual characteristic (average of upscale and downscale readings), positive or negative, from a straight line so positioned as to equalise and minimise the maximum deviations.

“Matrix” means a substantially continuous phase that fills the space between particles, whiskers or fibres.

"Measurement uncertainty” is the characteristic parameter which specifies in what range around the output value the correct value of the measurable variable lies with a confidence level of 95 %. It includes the uncorrected systematic deviations, the uncorrected backlash and the random deviations.

“Microcircuit”: A device in which a number of passive and/or active elements are considered as indivisibly associated on or within a continuous structure to perform the function of a circuit.

“Microprogrammes”: A sequence of elementary instructions maintained in a special storage, the execution of which is initiated by the introduction of its reference instruction register.

“Missiles” means complete rocket systems and unmanned aerial vehicle systems.

“Modified” in the context of “software” describes “software” which has been intentionally changed such that it has properties that make it fit for specified purposes or applications. Its properties may also make it suitable for purposes or applications other than those for which it was “modified.”

“Monofilament” or filament is the smallest increment of fibre, usually several micrometres in diameter.

“Monolithic integrated circuit” means a combination of passive or active ‘circuit elements’ or both which:

a. Are formed by means of diffusion processes, implantation processes or deposition processes in or on a single semiconducting piece of material, a so-called ‘chip’;

b. Can be considered as indivisibly associated; and

c. Perform the function(s) of a circuit.

N.B.: ‘Circuit element’ is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

“Neural computer” means a computational device designed or modified to mimic the behaviour of a neuron or a collection of neurons, i.e., a computational device which is distinguished by its hardware capability to modulate the weights and numbers of the interconnections of a multiplicity of computational components based on previous data.

“Numerical control” means the automatic control of a process performed by a device that makes use of numeric data usually introduced as the operation is in progress.

“Optical integrated circuit” means a “monolithic integrated circuit” or a hybrid integrated circuit, containing one or more parts designed to function as a photo sensor or photo emitter or to perform (an) optical or (an) electro-optical function(s).

“Precursors”: Speciality chemicals used in the manufacture of explosives.

“Pressure transducers” are devices that convert pressure measurements into an electrical signal.

“Production” means all production stages (e.g., product engineering, manufacture, integration, assembly (mounting), inspection, testing, quality assurance);

“Production equipment”: Tooling, templates, jigs, mandrels, moulds, dies, fixtures, alignment mechanisms, test equipment, other machinery and components therefor, limited to those specially designed or modified for “development” or for one or more phases of “production”.

“Production facilities”: Equipment and specially designed “software” therefor integrated into installations for “development” or for one or more phases of “production”.

“Programmes”: A sequence of instructions to carry out a process in, or convertible into, a form executable by an electronic computer.

“Propellants”: Substances or mixtures that react chemically to produce large volumes of hot gases at controlled rates to perform mechanical work.

“Public domain” means a domain that has no restrictions upon dissemination of information within or from it; the existence of any legal rights to the intellectual property in that information does not remove the information from being in “public domain”.

“Radiation hardened”: Means that the component or equipment is designed or rated to withstand radiation levels which meet or exceed a total radiation dose of 5 x 103 Gy or 5 x 105 rads (Si).

“Required”: As applied to “technology”, refers to only that portion of “technology” which is peculiarly responsible for achieving or exceeding the controlled performance levels, characteristics or functions. Such “required” “technology” may be shared by different products.

“Resolution” means the least increment of a measuring device; or on digital instruments, the least significant bit.

“Roving” is a bundle (typically 12-120) of approximately parallel ‘strands’.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

“Settling time” means the time required for the output to come within one-half bit of the final value when switching between any two levels of the converter.

“Signal processing” means the processing of externally derived information-bearing signals by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform).

“Software”: A collection of one or more “programmes”, or “micro-programmes”, fixed in any tangible medium of expression. However, unless otherwise provided for against any item on the SCOMET List, the List does not control “software” which is either in the public domain or is generally available to the public by being :

a. Sold from stock at retail selling points without restriction, by means of:

1. Over-the-counter transactions;

2. Mail order transactions; or

3. Telephone call transactions; and

b. Designed for installation by the user without further substantial support by the supplier.

“Space qualified”: Products designed, manufactured and tested to meet the special electrical, mechanical or environmental requirements for use in the launch and deployment of satellites or high altitude flight systems operating at altitudes of 100 km or higher.

“Stability” means the standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable temperature conditions. This can be expressed as a function of time.

“Specially designed” qualifies the description of equipment, parts, components or “software” which, as a result of “development”, have unique properties that distinguish them for certain predetermined purposes.

For example, a piece of equipment that is “specially designed” will only be considered so if it has no other function or use. Thus a piece of manufacturing equipment that is “specially designed” to produce a certain type of component will only be considered such if it is not capable of producing other types of components.

“Tape” is a material constructed of interlaced or unidirectional “monofilaments”, ‘strands’, “rovings”, “tows”, or “yarns”, etc., usually preimpregnated with resin.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

“Technology” means, except as otherwise provided for against any item in the SCOMET List, information (including information embodied in “software”) other than information in the “public domain”, that is capable of being used in:

a. the development, production or use of any goods or software;

b. the development of, or the carrying out of, an industrial or commercial activity or the provision of a service of any kind.

Explanation: When technology is described wholly or partly by reference to the uses to which it (or the goods to which it relates) may be put, it shall include services which are provided or used, or which are capable of being used, in the development, production or use of such technology or goods.

“Tow” is a bundle of “monofilaments”, usually approximately parallel.

“Toxins” means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of “microorganisms”.

“Unmanned Aerial Vehicle” (“UAV”) means any aircraft capable of initiating flight and sustaining controlled flight and navigation without any human presence on board.

“Usable in,” “usable for,” “usable as” or “capable of” qualifies the description of equipment, parts, components, materials, technology or “software” which are suitable for a particular purpose. There is no requirement that the equipment, parts, components, technology or “software” should have been configured, modified or specified for that particular purpose. (Contrast with “specially designed” – see above).

“Use” includes operation; installation (including on site installation); maintenance; repair; overhaul; refurbishing.

“Vaccine” is a medicinal product in a pharmaceutical formulation licensed by, or having marketing or clinical trial authorisation from, the regulatory authorities of either the country of manufacture or of use, which is intended to stimulate a protective immunological response in humans or animals in order to prevent disease in those to whom or to which it is administered. “

"Yarn” is a bundle of twisted ‘strands’.

N.B.: ‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

Items on the SCOMET List are organized in the following categories.
 

Category 0 Nuclear materials, nuclear-related other materials, equipment and technology
0A Prescribed Substances 0A1 Source Material
0A2 Special Fissionable Material
0A3 Other Materials
0B Prescribed Equipment
0C Technology
Category 1 Toxic chemical agents and other chemicals
1A Prohibited chemicals
1B Chemicals permitted only to States party to the Chemical Weapons Convention
1C Chemicals permitted also to States not party to the Chemical Weapons Convention
Category 2 Micro-organisms, toxins
2A Bacteria
2B Fungi
2C Parasites
2D Viruses
2E Rickettsials
2F Toxins
2G Plant pathogens
2H Genetically Modified Organisms
Category 3 Materials, Materials Processing Equipment and related technologies
3A Materials
3A1 Special materials
3A2 Structural materials
3A3 Rocket propellants and constituent chemicals
3A4 High explosives
3A5 Stealth materials
3B Materials processing and production equipment, related technology and specially designed components and accessories therefor.
3C [Reserved]
3D Chemical and biomaterial manufacturing and handling equipment and facilities
Category 4 Nuclear-related other equipment and technology, not controlled under Category 0
4A Equipment, assemblies, components including test and production equipment
4B Equipment, assemblies, components including test and measurement equipment usable in development of nuclear explosive devices
4C Technology
Category 5 Aerospace systems, equipment, including production and test equipment, related technology and specially designed components and accessories therefor.
5A Rocket systems
5A1 Systems
5A2 Production and test equipment
5A3 Technology
5B Unmanned aerial vehicles
5C Avionics and navigation systems
5D Manned-aircraft, aero-engines, related equipment and components
5E Micro-light aircraft and powered ‘hang-gliders’
Category 6 [Reserved]
Category 7 Electronics, computers, and information technology including information security
7A Electronics
7B Electronic test equipment
7C Computers
7D Information technology including information security
7E [Reserved]
Category 0 Nuclear materials, nuclear-related other materials, equipment and technology

Note: Export of these items is regulated under the Atomic Energy Act, 1962 and rules framed, and notifications/orders issued thereunder from time-to-time by the Department of Atomic Energy. The licensing authority for items in this category is the Department of Atomic Energy. An application for licences to export prescribed equipment or/an prescribed substances shall be made in writing to the Joint Secretary, Department of Atomic Energy, Anushakti Bhavan, CSM Marg, Mumbai 400 001.
0A Prescribed Substances

Note: Any radioactive material in Category 0A shall additionally attract the provisions of Radiation Protection Rules, 2004 made under the Atomic Energy Act, 1962 and the provisions of Section-16 of the Atomic Energy Act, 1962.
0A1 Source Material
0A101 Uranium containing the mixture of isotopes occurring in nature.
0A102 Uranium depleted in the isotope 235.
0A103 Thorium.
0A104 Any of the foregoing in the form of metal, alloy, chemical compound, or concentrate or any substance.
0A105 Any other material containing one or more of the foregoing.

Prescribed quantitative limits: as given below and in any period of 12 months:

a. Uranium (containing the mixture of isotopes in nature) exceeding 100 kilograms.

b. Depleted uranium (uranium depleted in the isotope 235 below that occurring in nature) exceeding 1000 kilograms.

c. Thorium exceeding 1000 kilograms.
0A2 Special Fissionable Material
0A201 Plutonium-239.
0A202 Uranium-233.
0A203 Uranium enriched in the isotopes 235 or 233.
0A204 Neptunium.
0A205 Any material containing one or more of the foregoing.
0A206 Such other fissionable material determined by the Central Government from time to time, but the term “special fissionable material” does not include source material.

Note: Any quantity of special fissionable material is prescribed substance.
0A3 Other Materials

‘Other Materials’ means non-nuclear materials for reactors, nuclear related dual-use materials indicated below and such materials as determined by the Central Government from time to time.
0A301 Deuterium, heavy water (deuterium oxide) and any other deuterium compound, in which the ratio of deuterium to hydrogen atoms exceeds 1:5000, in quantities exceeding 5 kilograms of deuterium in one consignment or 25 kilograms of deuterium in any period of 12 months.
0A302 Nuclear grade graphite / carbon, having a purity level better than 5 parts per million (ppm) boron equivalent and with a density greater than 1.5 gram/cc in quantities exceeding 30 metric tons in any period of 12 months.
0A303 Zirconium with hafnium content of less than 1 part to 500 parts of zirconium by weight (i.e. less than 2000 ppm) in the form of metal, its alloys, compounds, manufactures thereof, waste or scrap of any of the foregoing.
0A304 Beryllium, its compounds, alloys and its minerals / concentrates including Beryl but excluding:

a. beryllium windows used for x-ray machines and gamma ray detectors and

b. beryl in the form of emeralds or aquamarines.
0A305 Lithium enriched in the Lithium-6 (6Li) isotope to greater than its natural isotopic abundance (i.e. more than 7.5%) and the products or devices containing enriched lithium such as elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.
0A306 Niobium and Tantalum, their metals, alloys and minerals including columbite and tantalite.
0A307 Titanium alloys having both of the following characteristics:

a. ‘Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20 degrees C); and

b. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

Technical note: The phrase ‘capable of’ encompasses titanium alloys before or after heat treatment.
0A308 Tritium, tritium compounds or mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, except when utilized in such quantities and for such purposes as for organic labelled compounds, Gas Filled Light Sources and as Tritiated Water for radiotracer studies.
0A309 Hafnium: (CAS 7440-58-6)

Hafnium metal, alloys containing more than 60% hafnium by weight, hafnium compounds containing more than 60% hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.
0A310 Radium-226:

Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing, except medical applicators and a product or device containing less than 0.37 GBq (10mCi) of Ra-226 in any form.
0A311 Boron (CAS 7740-42-8)

Boron enriched in the Boron-10 (10B) isotope to greater than its natural isotopic abundance as follows:

Elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
0A312 Helium-3

Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.

Note: A product or device containing less than 1gm of Helium-3 is excluded.
 
0A313 Alpha–emitting radionuclides:

Alpha–emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, in the following forms:

a. Elemental;

b. Compounds having a total alpha activity of 37 GBq per kg or greater;

c. Mixtures having a total alpha activity of 37 GBq per kg or greater;

d. Products or devices containing any of the foregoing.

Alpha emitters controlled by this item include:
Actinium-225 Actinium-227 Americium-242m
Californium-248 Californium-250 Californium-252
Californium-253 Californium-254 Curium-240
Curium-241 Curium-242 Curium-243
Curium244 Einsteinium-252 Einsteinium-253
Einsteinium254 Einsteinium-255 Fermium-257
Gadolinium-148 Mendelevium-258 Neptunium-235
Plutonium-236 Plutonium-237 Plutonium-238
Plutonium-241 Polonium-209 Polonium-210
Polonium-208 Radium-223 Thorium-228
Thorium-227 Uranium-230 Uranium-232

 
0B Prescribed Equipment
0B001 Nuclear Reactors; associated equipment, components, and systems specially designed, prepared, or adapted or used or intended to be used in such reactors:-

a. Complete nuclear reactors

b. Nuclear reactor vessels

c. Nuclear reactor fuel charging and discharging machines

d. Nuclear reactor control rods and equipment

e. Nuclear reactor pressure tubes

f. Zirconium tubes and assemblies of tubes in which hafnium to zirconium ratio is 1:500 or less

g. Primary coolant pumps

h. Nuclear reactor internals

i. Heat exchangers (steam generators) for use in the primary coolant circuit of a nuclear reactor

j. Neutron detection and measuring instruments for determining neutron flux levels within the core of a nuclear reactor.
0B002 Plants for processing, production, concentration, conversion or recovery of Prescribed Substances (such as uranium, plutonium, thorium, deuterium, heavy water, tritium, lithium); associated equipment, components and systems specially designed, prepared or adapted or used or intended to be used in such plants including but not limited to:

a. Plants for production or concentration of deuterium, heavy water-

1. Water - Hydrogen Sulphide Exchange Towers

2. Blowers and Compressors for hydrogen-sulphide gas circulation

3. Ammonia-Hydrogen Exchange Towers greater than or equal to 35 m in height with diameters of 1.5 m to 2.5 m

4. Tower Internals and Stage Pumps

5. Ammonia Crackers with operating pressures greater than or equal to 3 MPa

6. Infrared Absorption Analyzers capable of ‘on-line’ hydrogen/ deuterium ratio analysis

7. Catalytic Burners for conversion of enriched deuterium gas into heavy water

8. Complete heavy water upgrade systems or columns therefor

b. Plants for the conversion of uranium

c. Plants for the conversion of plutonium

d. Tritium facilities or plants, and equipment therefor

e. Lithium isotope separation facilities or plants, and equipment therefor
 
0B003 Plants for reprocessing of irradiated nuclear fuel and equipment, components and systems specially designed, prepared or adapted or used or intended to be used in such plants, including but not limited to:

a. Irradiated fuel element chopping machines designed for remote operation

b. Dissolvers capable of withstanding hot and highly corrosive liquid for dissolution of irradiated nuclear fuel and which can be remotely loaded and maintained

c. Solvent extractors and solvent extraction equipment resistant to the corrosive effect of nitric acid

d. Chemical holding or storage vessels resistant to the corrosive effect of nitric acid

e. Industrial equipment including assemblies and components as follows:

1. High density (lead glass or other) radiation shielding windows

2. Radiation hardened TV cameras, or lenses therefor

3. ‘Robots’ or ‘end effectors’ specially designed for handling high explosives; and control units therefor

4. Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells
0B004 Plants for treatment, handling, storage and transportation of radioactive wastes from nuclear reactors or from plants for processing Source Materials or Special Fissionable Materials or from nuclear reprocessing plants; irradiated nuclear fuel; Special Fissionable Materials, and equipment specially designed, prepared, adapted, or intended to be used therefor.
0B005 All systems, associated equipment, components for separation or enrichment of isotopes of uranium, plutonium, lithium or boron, other than analytical instruments, specially designed, prepared, adapted, used or intended to be used therefor as follows:

a. Gas centrifuges and assemblies and components specially designed or prepared for use in gas Centrifuges

b. Specially designed or prepared auxiliary systems, equipment and components for gas centrifuge enrichment plants

c. Specially designed or prepared assemblies and components for use in gaseous diffusion enrichment

d. Specially designed or prepared auxiliary systems, equipment and components for use in gaseous diffusion enrichment

e. Specially designed or prepared systems, equipment and components for use in aerodynamic enrichment plants

f. Specially designed or prepared systems, equipment and components for use in chemical exchange or ion exchange enrichment plants.

g. Specially designed or prepared systems, equipment and components for use in laser-based enrichment plants.

h. Specially designed or prepared systems, equipment and components for use in plasma separation enrichment plants.

i. Specially designed or prepared systems, equipment and components for use in electromagnetic enrichment plants.
0B006 Plants for the fabrication of nuclear reactor fuel elements, and equipment specially designed or prepared therefor including but not limited to:

a. fully automatic pellet inspection stations specially designed or prepared for checking final dimensions and surface defects of the fuel pellets;

b. automatic welding machines specially designed or prepared for welding end caps onto the fuel pins (or rods);

c. automatic test and inspection stations specially designed or prepared for checking the integrity of completed fuel pins (or rods).

Item ‘c’ typically includes equipment for: 1) x-ray examination of pin (or rod) end cap welds, 2) helium leak detection from pressurized pins (or rods), and 3) gamma-ray scanning of the pins (or rods) to check for correct loading of the fuel pellets inside.
0B007 Plants or systems for production, handling, storage and transportation of Radioisotopes in quantities exceeding 100 Curies (3.7 X 10 12 Becquerel).
0B008 Neutron generators including neutron chain reacting assemblies and fusion assemblies of all kinds for producing fissile materials
0C Technology

Technology and software for the development, production or use of prescribed substances or prescribed equipment specified in 0A or 0B.
Category 1 Toxic chemical agents and other chemicals
1A Export of the following chemicals is prohibited:

(This corresponds to Schedule 1 to the Chemical Weapons Convention (CWC))

Note: Where reference is made below to groups of di-alkylated chemicals, followed by a list of alkyl groups in parentheses, all chemicals possible by all possible combinations and alkyl groups listed in parentheses are considered prohibited unless explicitly exempted.
(1). O-Alky (
(2). O-Alkyl, (
(3). O-Alkyl (H or < C10, incl. cycloalkyl) S-2-Dialkyl (Me, Et, n-Pr or i-Pr)-aminoethyl alkyl (Me, Et, n-Pr or i-Pr) phosphonothiolates and corresponding alkylated or protonated salts
e.g. VX: O-Ethyl S-2 diisopropylaminoethyl methyl phosphonothiolate
(4). Sulphur mustards:
2-Chloroethylchloromethylsulphide
Mustard gas: Bis (2-chloroethyl) sulphide
Bis (2-chloroethylthio) methane
Sesquimustard:1,2-Bis (2-chloroethylthio) ethane
1,3-Bis (2-chloroethylthio)-n-propane
1,4-Bis (2-chloroethylthio)-n-butane
1,5-Bis (2-chloroethylthio)-n-Pentane
Bis (2-Chloroethylthiomethyl) ether
O-Mustard: Bis (2-Chloroethylthiomethyl) ether
(5). Lewisites:
Lewisite 1: 2-Chlorovinyldichloroarsine
Lewisite 2: Bis (2-Chlorovinyl) chloroarsine
Lewisite 3: Tris (2-Chlorovinyl) arsine
(6). Nitrogen mustards:
HN1: Bis (2-chloroethyl) ethylamine
HN2: Bis (2-chloroethyl) Chloroarsine
HN3: Tris (2-chloroethyl) amine
(7). Saxitoxin
(8). Ricin
(9). Alkyl (Me, Et, n-Pr or I-Pr) phosphonyldifluorides
e.g. DF: Methyl phosphonyldifluoride
(10). O-Alkyl (H or < C10, incl. cycloalkyl) O-2 dialkyl (Me, Et, n-Pr or i-Pr)-aminoethylalkyl (Me, Et N-Pr or i-Pr) phosphonites and corresponding alkylated or protonated salts
e.g.QL: O-Ethyl O-2-diisopropylaminoethyl methyl phosphonite
(11). Chlorosarin: O-Isopropyl methylphosphonochloridate
(12). Chlorosoman: O-Pinacolyl methylphosphonochloridate
1B Export of chemicals listed in 1B below is permitted only to States party to the Chemical Weapons Convention
(This corresponds to Schedule 2 to the Chemicals Weapons Convention) Note to exporter:
(a) A list of States Parties can be obtained from the Disarmament & International Security Affairs Division of the Ministry of External Affairs (Room No. 40G, South Block, New Delhi) or at the official website of the Organization for the Prohibition of Chemical Weapons at www.opcw.org.
(b) A general permission valid for a period of two years may be applied for export of chemicals in this category. This permission shall be subject to the condition that for each export consignment, exporters shall, within 30 days of exports, notify the details to the National Authority, Chemical Weapons Convention, Cabinet Secretariat ; Ministry of External Affairs (D&ISA); Department of Chemicals and Petrochemicals and the Directorate General of Foreign Trade and submit to DGFT, a copy of Bill of Entry into the destination State Party within 30 days of delivery.
Note: Where reference is made below to groups of dialkylated chemicals, followed by a list of alkyl groups in parentheses, all chemicals possible by all possible combinations and alkyl groups listed in parentheses are included unless explicitly exempted.
1. Amiton 0,0-Diethyl S-[2-(diethylamino) ethyl)] phosphorothiolate and corresponding alkylated or protonated salts
2. PFIB: 1,1,3,3,3,-Pentafluoro-2-(trifluoromethyl)1-propene
3. BZ: 3-Quinuclidinyl benzilate
4. Chemicals, except for those listed in Schedule 1, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms,
e.g.Methylphosphonyl dichloride
Dimethyl methylphosphonate
Exemption:- Fonofos: O-Ethyl S-phenyl ethylphosphonothiolothionate
5. N, N-Dialkyl (ME, Et, n-Pr or i-Pr) phosphoramidic dihalides
6. Dialkyl (Me, Et, n-Pr or i-Pr) N, N-dialkyl (Me, Et, n-Pr or i-Pr)-phosphoramidates
7. Arsenic trichloride
8. 2,2-Diphenyl-2 hydroxyacetic acid
9. Quinuclidine-3-ol
10. N,H-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethyl-2 -chlorides and corresponding protonated salts
11. N, N-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethane-2-ols and corresponding protonated salts
Exemptions: N,N-Dimethylaminoethanol and corresponding protonated salts
N,N-Diethylaminoethanol and corresponding protonated salts
12. N, N-Dialkyl (Me, Et, n-Pr or i-Pr) aminoethane-2-thiols and corresponding protonated salts
13. Thiodiglycol: Bis(2-hydroxyethyl) sulphide
14. Pinacolyl alcohol: 3,3-Dimethylbutane-2-ol
A List of commercially important Schedule-2 Chemicals of CWC is given below :

Sl. No. Name of Chemical Entry into Schedule CAS (Chemical Abstract Service) Numbers ITC(HS) codes
1. 2-Chloro N, N-Di-isopropyl ethylamine 2B10 4261-68-1 29211911
2. Diethyl amino Ethanethiol 2B12 100-38-9 29221910
3. O, O, Dimethyl Methyl Phosphonate 2B04 756-79-6 29209045
4. 2-Hydroxy N, N-Diisopropyl Ethylamine 2B11 96-80-0 29221111
5. N, N-Diethyl Amino ethyl Chloride Hydrochloride 2B10 869-24-9 29221112
6. Di-ethyl Amino ethanethiol Hydrochloride 2B12 1942-52-5 29221113
7. Di-Methyl Amino ethyl chloride Hydrochloride 2B10 4584-46-7 29221114
8. Di-Methyl Amino ethanethiol 2B12 108-02-1 29221115
9. Di-Methyl Amino ethanethiol Hydrochloride 2B12 13242-44-9 29221116
10. Phosphorothioic acid, S [2-(diethylamino) ethyl] O, O – diethyl ester 2A01 78-53-5 29201910
11. 1-Propene, 1,1, 3, 3, 3, - Pentafluoro – 2-(trifluoromethyl) (PFIB) 2A02 382-21-8 29033911
12. Benzeneacetic acid, alphahydroxy – alpha-phenyl, 1 – azabicyclo [2.2.2.] oct-3-yl ester 2A03 6581-06-2 29392050
13. Phosphonic Acid, Methyl-compound with (aminoimino methyl) urea (1: 1) 2B04 84402-58-4 29209047
14. 1-Propanaminium N, N, N-trimethyl – 3- [1-oxo-9 octadecenyl) amino]-. (Z)- methyl methylphosphonate 2B04 70055-71-9 29209048
15. Phosphonic acid, [methyl bis (5-ethyl-2-methyl-2-oxido-1, 3, 2- dioxaphosphorinan-5-yl) methyl] ester 2B04 42595-45-9 29209051
16. Phosphonic acid, [methyl-(5-ethyl-2-methyl 2-oxido-1,3,2-dioxaphosphorinan-5-yl) methyl] ester 2B04 41203-81-0 29209052
17. Phosphonic acid, propyl-dimethyl ester 2B04 18755-43-6 29209053
18. Phosphonous acid, methyl-diethyl ester 2B04 15715-41-0 29209054
19. Phosphonic acid, ethyl- 2B04 6779-09-5 29209055
20. Phosphonic acid, propyl- 2B04 4672-38-2 29209056
21. Phosphinic acid, methyl- 2B04 4206-94-4 29209057
22. Phosphonochloridic acid, methyl-, methyl ester 2B04 1066-52-0 29209058
23. Phosphonothioic dichloride, ethyl- 2B04 993-43-1 29209061
24. Phosphonic acid methyl- 2B04 993-13-5 29209062
25. Phosphonic acid, methyl-, dimethyl ester 2B04 756-79-6 29209063
26. Phosphonic dichloride, methyl- 2B04 676-97-1 29209064
27. Phosphonous dichloride, methyl- 2B04 676-83-5 29209065
28. Phosphonic acid, ethyl-, diethyl ester 2B04 78-38-6 29209066
29. Arsenous trichloride 2B07 7784-34-1 28121060
30. Benzeneacetic acid, alpha-hydroxy-alpha-phenyl 2B08 76-93-7 29181910
31. 1-Azabicyclo (2.2.2.) octan-3-ol 2B09 1619-34-7 29333930
32. Ethanamine, 2-Chloro-N, N-dimethyl- 2B10 107-99-3 29211914
33. Ethanol, 2-[bis(1-methylethyl ) amino ]- 2B11 96-80-0 29221920
34. Ethanethiol, 2-(diethylamino)- 2B12 100-38-9 29221930
35. Ethanol, 2, 2’-thiobis- 2B13 111-48-8 29309091
36. 2-Butanol, 3, 3-dimethyl- 2B14 464-07-3 29051910

 
1C Export of Chemicals as specified below is allowed to State Parties to the CWC without an export licence subject to the condition that the exporter shall notify within 30 days of export to the National Authority, Chemicals Weapons Convention, Cabinet Secretariat; the Ministry of External Affairs (D&ISA); the Department of Chemicals & Petro-chemicals, and the DGFT of such exports in the prescribed format (Aayat Niryat Form ) along with the End-Use Certificate and submit to the DGFT a copy of the bill of entry into the destination State Party within 30 days of delivery. Export of chemicals as specified below to states not party to the Chemical Weapons Convention shall continue to be restricted and will be allowed only against an export licence, and in that case also exporters shall submit to the DGFT a copy of the bill of entry into the destination country within 30 days of export.

Sl.No. Name of Chemical Entry into Schedule CAS Numbers ITC (HS) codes
1. Phosgene : ( Carbonyl dichloride) 3A01 75-44-5 28121010
2. Cyanogen chloride [(CN) C1] 3A02 506-77-4 28530091
3. Hydrocyanic acid 3A03 74-90-8 28111910
4. Chloropicrin: Trichloronitro-Methane 3A04 76-06-2 29049080
5. Phosphorus Oxychloride 3B05 10025-87-3 28121030
6. Phosphorus trichloride 3B06 7719-12-2 28121021
7. Phosphorous Pentachloride 3B07 10026-13-8 28121022
8. Trimethyl Phosphite 3B08 121-45-9 29209041
9. Triethyl Phosphite 3B09 122-52-1 29209042
10. Dimethyl Phosphite 3B10 868-85-9 29209043
11. Diethyl Phosphite 3B11 762-04-9 29209044
12. Sulphur monochloride 3B12 10025-67-9 28121042
13. Sulphur dichloride 3B13 10545-99-0 28121043
14. Thionyl Chloride 3B14 7719-09-7 28121047
15. Ethyldiethanolamine 3B15 139-87-7 29221211
16. Methyldiethanolamine 3B16 105-59-9 29221212
17. Triethanolamine 3B17 102-71-6 29221300

 
Category 2 Micro-organisms, toxins 2A Bacteria, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2A001 Bacillus anthracis
2A002 Bordetella bronchoseptica
2A003 Brucella abortus,
2A004 Brucella melitensis
2A005 Brucella suis
2A006 Chlamydia psittaci
2A007 Clostridium botulinum
2A008 Clostridium perfringes
2A009 Corynebacterium diphtheriae
2A010 Francisella tularensis
2A011 Klebsiella pneumoniae
2A012 Legionlla pneumophila
2A013 Leptospira interrogans - all serotypes reported in India
2A014 Mycobacterium bovis
2A015 Mycobacterium tuberculosis
2A016 Mycoplasma mycoides - var mycoides
2A017 Mycoplasma mycoides - var Capri
2A018 Neisseria meningitidis
2A019 Paseturella multicoda type B
2A020 Pseudomonas mallei
2A021 Pseudomonas pseudomallei
2A022 Salmonella paratyphi
2A023 Shigella dysenteriae
2A024 Staphylococcus aureus
2A025 Streptococcus pneumoniae
2A026 Vibrio cholerae elter
2A027 Vibrio Cholerae 0139
2A028 Yersinia pestis
2B Fungi, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2B001 Blastomyces dermatitidis
2B002 Coccidiodes immitis
2B003 Histoplasma capulatum
2B004 Nocardia asteroides
2B005 Paracoccidioides braziliensis
2C Parasites, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2C001 Entamoeba histolytica
2C002 Babesia microti
2C003 Babesia divergens
2C004 Blostidium coli
2C005 Cryptosporidium spp.
2C006 Leishmania species
2C007 Naegleria australiensis
2C008 Naegleria fowleri
2C009 Plasmodium falciparum
2C010 Pneumocystis carinii
2C011 Schistosoma mansoni
2C012 Schistosoma japonicum
2C013 Schistosoma hemotobium
2C014 Toxoplasma gondii
2C015 Trichinella spiralis
2C016 Trypanosoma bruiei
2D Viruses, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2D001 African Horse Sickness virus
2D002 African Swine Fever virus
2D003 Avian influenza virus
2D004 Blue tongue virus
2D005 Camel pox virus
2D006 Chikungunya virus
2D007 Crimean-Congo hemorrhagic fever virus
2D008 Dengue virus
2D009 Eastern equine encephalitis virus
2D010 Ebola fever virus
2D011 Encephalomyocarditis virus (EMC)
2D012 Foot and Mouth Disease virus (all serotypes and subtypes)
2D013 Guanirito virus
2D014 Goatpox virus
2D015 Hantaan virus
2D016 Herpes virus simiae (monkey B virus)
2D017 Herpes ateles, Herpes saimiri
2D018 HIV- 1 & HIV-2 and other strains of SIV
2D019 Hog cholera virus
2D020 Human T-cell Leukemia virus
2D021 Junin virus
2D022 Japanese encephalitis virus
2D023 Kyasanur Forest Disease virus and Central European encephalitis viruses.
2D024 Korean hemorrhagic fever virus
2D025 Lymphocytic choriomeningitis virus (LCM)
2D026 Lassa virus
2D027 Marburg virus
2D028 Murrey valley encephalitis virus
2D029 Marchupo virus
2D030 Mason-pfizer monkey virus
2D031 Monkey pox virus
2D032 Newcastle disease virus
2D033 Omsk hemorrhagic fever virus
2D034 Peste des petits ruminant virus
2D035 Porcine enterovirus type I
2D036 Powassan virus
2D037 Rabies virus -all strains
2D038 Respiratory syncitial virus
2D039 Rift Valley Fever virus
2D040 Rinderpest virus
2D041 Sabia virus
2D042 Sheep pox (field strain)
2D043 Sin Nombre virus
2D044 Smallpox virus
2D045 St.Louis encephalitis virus
2D046 Swine Fever virus
2D047 Tick-borne encephalitis virus (Russian Spring Summer Encephalitis virus)
2D048 Teschen disease virus (Porcine entero virus type 1)
2D049 Variola virus
2D050 Venezuelan encephalitis virus
2D051 Vesicular stomatitis virus
2D052 Western encephalitis virus
2D053 Yellow fever virus, 17 D vaccine strain
2E Rickettsials, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following:
2E001 Coxiella burnetti
2E002 Rickettsiae rickettsii
2E003 Rickettsia quintana
2E004 Rickettsia prowazebi
2F Toxins
2F001 Abrins
2F002 Aflatoxins
2F003 Anatoxins
2F004 Botulinum toxin (s) (clostradium botulinum)
2F005 Bungarotoxins
2F006 Clostridium perfringens toxins
2F007 Corynebacterium diphtheriae toxins
2F008 Cyanginosins (Microcystins) (Microcystic aeuginosa)
2F009 Enterotoxin (Staphylococcus aureus)
2F010 Neurotoxin (Shigella dysenteriae)
2F011 Ricins
2F012 Shigatoxins
2F013 Saxitoxins
2F014 Trichothecene mycotoxins
2F015 Tetanus toxin (clostridium tetani)
2F016 Tetrodotoxin (Spheroides rufripes)
2F017 Verrucologen (M. verrucadia)
2G Plant pathogens
2G001 Bemisia tabaci
2G002 Colletotrichum coffeanum var. virulans
2G003 Clavicep purpurea
2G004 Dothistroma pini (Scirrhia pini)
2G005 Erwinia amylovora
2G006 Frankliniella occidentalis
2G007 Microcyclus ulei
2G008 Peronospora hyoscyami de Bary f.sp. tabacina (Adam) skalicky
2G009 Phytophthora infestans
2G010 Puccinia graminis
2G011 Puccinia erianthi
2G012 Puccinia striiformiis (Puccinia glumarum)
2G013 Pyricularia oryzae
2G014 Pseudomonas solanacearum
2G015 Peronospora hyscyami de Bary
2G016 Ralstonia solanacearum
2G017 Sugar cane Fiji disease virus
2G018 Sclerotinia sclerotiorum
2G019 Tilletia indica
2G020 Thrips palmi
2G021 Ustilago Maydis
2G022 Xanthomonas albilineans
2G023 Xanthomonas campestris pv citri
2G024 Xanthomonas campestris pv oryzae
2H Genetically Modified Organisms
2H001 Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity and are derived from organisms specified above in 2A, 2B, 2C, 2D, 2E and 2H.

Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences coding for any of the toxins specified above in 2F.
Category 3 Materials, Materials Processing Equipment and related technologies
3A Materials
3A1 Special Materials
3A101 Zirconium, beryllium, magnesium, and alloys of these in particle size less than 60 µm
3A102 Maraging steel in any form in which any linear dimension exceeds 75 mm, or in the form of sheet, plate or tubing with a wall or plate thickness equal or less than 5 mm.
3A103 Tungsten (CAS 12070-12-1), molybdenum(CAS 1317-33-5), and alloys of those metals in the form of uniform spherical or atomized particles of size less than 500 µm
3A104 Germanium
3A105 Gallium
3A106 Indium
3A107 Titanium alloys including Titanium-stabilised Duplex Stainless Steel (Ti-DSS) (other than as specified at 0A307)
3A108 Aluminium alloys in any form ‘capable of acquiring’ an ultimate tensile strength of 460 MPa or more at 293 K (20 degrees C)

Note: The phrase ‘capable of acquiring’ encompasses alloys before or after heat treatment
3A109 Bismuth having a purity of 99.99% or greater by weight and containing less than 10 parts per million by weight of silver
3A110 Calcium containing less than 1000 parts per million by weight of metallic impurities other than magnesium and containing less than 10 parts per million by weight of Boron
3A111 Chlorine trifluoride (ClF3)
3A112 Magnesium containing less than 200 parts per million by weight of metallic impurities other than calcium and containing less than 10 parts per million by weight of boron
3A113 Tungsten, tungsten carbide, and alloys containing more than 90% tungsten by weight in forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm and a mass greater than 20 kg.
3A114 a. Nickel powder of purity 99.0% or greater by weight and having a mean particle size of less than 10 µm;

b. Porous nickel metal produced from the nickel powder specified above
3A115 Natural boron, boron carbide or metal borides having a boron purity of 85% or more.
3A116 Fibrous or filamentary materials, and prepregs, as follows:

a. Carbon or aramid fibrous or filamentary materials having ‘specific modulus’ of 12.7 x 106 m or greater; or ‘specific tensile strength’ of 23.5 x 104 m or greater;
b. Glass fibrous or filamentary materials having ‘specific modulus’ of 3.18 x 106 m or greater; and ‘specific tensile strength’ of 7.62 x 104 m or greater;
c. Thermoset resin impregnated continuous yarns, rovings, tows or tapes with a width of 15 mm or less (prepregs), made from carbon or glass fibrous or filamentary materials specified in (a) or (b) above.
3A117 Carbon - carbon composites.
3A2 Structural Materials
3A201 Structural materials such as:
a. Composite structures, laminates, resin impregnated fibre prepregs and metal coated fibre preforms made either with an organic matrix or metal matrix utilizing fibrous or filamentary reinforcements, and manufactures thereof, specially designed for use in rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles and subsystems thereof;
b. Resaturated pyrolized (i.e. Carbon-Carbon) materials specially designed for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles;
c. Fine grain re-crystalised bulk graphites and pyrolytic or fibrous reinforced graphites usable for rocket nozzles and re-entry vehicles nose tips;
d. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes;
e. Materials and coatings for reduced radar reflectivity;
f. Bulk machinable silicon-carbide reinforced unfired ceramic usable in re-entry vehicles nose tips.
3A3 Rocket propellants and constituent chemicals:
3A301 Propulsive substances – Hydrazine (CAS-302-01)and its derivatives usable as rocket fuel substances including Monomethylhydrazine (MMH)(CAS 60-34), Unsymmetrical di-methyl hydrazine (UDMH), (CAS 57-14-7)Hydrazine nitrate, (except aromatic hydrazines and their salts, adipic acid dihydrazide), ammonium perchlorate, spherical aluminium powder(CAS 7429-90-5);
3A302 Metal fuels containing any of the following: Zirconium(CAS 7440-67-7), beryllium(CAS 7440-41-7), magnesium, titanium, tungsten, boron and boron alloys, zinc, and alloys of magnesium(CAS 7439-95-4);
3A303 Polymeric substances: Carboxyl-terminated polybutadiene (CTPB) Hydroxy-Terminated Polybutadiene (HTPB) Glycidyl azide polymer (GAP) Polybutadiene acrylic acid (PBAA) Polybutadiene acrylonitrile (PBAN)
3A304 Composite propellants and composite modified double base propellants;
3A305 High energy density materials such as boron slurry;
3A306 Oxidizers/fuels - Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components; Dinitrogen trioxide, Nitrogen dioxide / Dinitrogen tetroxide, Mixed Oxides of Nitrogen (MON), Dinitrogen pentoxide, Inhibited red fuming nitric acid (IRFNA) (CAS 8007-58-7), Ammonium perchlorate (CAS 7790-98-9), Ammonium Dinitramide (ADN) (CAS 140456-78-6), Hydrazinium Nitroformate (HNF), Compounds composed of fluorine and one more of other halogens, oxygen or nitrogen.
3A307 Bonding agents - Tris (1-2 (2-methyl)) aziridinyl phosphine oxide (MAPO)(CAS 57-39-6), Trimesoyl-1-(2-ethyl) aziridene (HX-868, BITA)(CAS 7722-73-8), Tepanol (HX-878)(CAS 68412-46-4), Tepan (HX-879) reaction product of tetraethlylenepentamine and acrylonitrile (CAS 68412-45-3), and Polyfunctional aziridine amides with isophthalic, trimesic, isocyanuric, or trimethyladipic backbone also having a 2-methyl or 2-ethyl aziridine group including 1,1'-Isophthaloyl-bis(2-methylaziridene (CAS 7652-64-4), (HX-752, HX-874, and HX-877);
3A308 Curing agents and reaction catalysts - Triphyenyl bismuth (TPB)(CAS 603-33-8);
3A309 Burning rate modifiers –
a. Carboranes, decaboranes, pentaboranes and derivatives thereof;
b. Ferrocene derivatives, as follows:
1. Catocene (CAS 37206-42-1);
2. Ethyl ferrocene;
3. Propyl ferrocene(CAS 1273-89-8)
4. n-Butyl ferrocene(CAS 31904-29-7);
5. Pentyl ferrocene (CAS 1274-00-6);
6. Dicyclopentyl ferrocene(CAS 20773-28-8);
7. Dicyclohexyl ferrocene;
8. Diethyl ferrocene;
9. Dipropyl ferrocene;
10. Dibutyl ferrocene(CAS 1274-08-4);
11. Dihexyl ferrocene (CAS 93894-59-8);
12. Acetyl ferrocenes;
13. Ferrocene Carboxylic acids;
14. Butacene;
c. Other ferrocene derivatives usable as rocket propellant burning rate modifiers.
3A310 Nitrate esters and nitrated plasticisers as follows:
a. Triethylene glycol dinitrate (TEGDN);
b. Trimethylolethane trinitrate (TMETN)(CAS 3032-55-1) ;
c. 1,2,4-butanetriol trinitrate (BTTN)(CAS 6659-60-5) ;
d. Diethylene glycol dinitrate (DEGDN).
3A311 Stabilisers as follows:
a. 2-Nitrodiphenylamine (CAS 119-75-5);
b. N-methyl-p-nitroaniline (CAS 100-15-2).
3A4 High explosives
3A401 High explosives, and propellants or mixtures containing any of the following;
a. Cycloteramethylenetetranitramine (HMX);
b. Cyclotrimethylenetrinitramine (RDX);
c. Triaminotrinitrobenzene (TATB);
d. Hexanitrostilbene (HNS). License applications for the export of items at 3A401a and 3A401b will normally be denied.
3A5 Stealth materials
3A501 a. Materials for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures;
b. Devices, including made from non-stealth material, for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures; ]
3A502 Materials and coatings (including paints) specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet spectra other than coatings (including paints) when specially used for thermal control of satellites.
3A503 Technology related to the development, production or use of items in 3A.
3B Materials processing and “production equipment”, related “technology” and specially designed components and accessories therefor.
3B001 Remote manipulators that provide mechanical translation of human operator actions by electrical, hydraulic or mechanical means and operating arm and terminal fixture that can be used to provide remote actions;
3B002 Multidirectional, multidimensional weaving and interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to fabricate composite structures except textile machinery which has not been modified for rocket systems;
3B003 Equipment designed or modified for production of fibrous or filamentary materials as follows: converting polymeric substances; vapour deposition on heated filament substrates; wet spinning of refractory ceramics.
3B004 Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies;
3B005 Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites.
3B006 Pyrolytic deposition and densification equipment including:
a. Technology for producing pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases.
b. Specially designed nozzles for the above process.
c. Equipment and process controls and specially designated software thereof, specially designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips.
3B007 Production equipment usable for or specially designed or modified for production, handling, mixing, curing, casting, pressing, machining or acceptance testing of the solid or liquid rocket propellants or rocket propellant constituents and related technology.
3B008 Refrigeration units and equipment capable of cooling hydrogen or helium to -250 degrees Celsius (23K) or lower.
3B009 Continuous nitrators.
3B010 Dehydration presses.
3B011 Screw extruders usable for or specially designed or modified for high explosive extrusion.
3B012 Cutting machines for the sizing of extruded propellant.
3B013 Sweetie barrels (tumblers) 1.85 m or more in diameter and having over 227 kg product capacity;
3B014 Continuous mixers or batch mixers with provision for mixing under vacuum.
3B015 Fluid energy mills usable for grinding or milling any of the items in 3A3.
3B016 Equipment to achieve both sphericity and uniform particle size in metal powders.
a. Metal powder production equipment usable for production, in a controlled environment, of spherical or atomized materials including:
b. Plasma generators (high frequency arc-jets) usable for obtaining sputtered or spherical metallic powders with organisation of the process in an argon-water environment
c. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organisation of the process in an argon-water environment.
3B017 Sputter ion pumps
3B018 Technical data (including processing conditions) and procedures for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves when used for the production of composites or partially processed composites.
3B019 Software specially designed or modified for the use of equipment for the production and handling of materials specified in 3A
3B020 Technology for the development, production or use of items in 3B
3C [Reserved]
3D Chemical and biomaterial manufacturing and handling equipment and facilities:
3D001 Reaction vessels, reactors or agitators, storage tanks, containers or receivers, heat exchangers or condensers, distillation or absorption columns, valves, remotely operated filling equipment, multi-walled piping, bellows, diaphragm pumps, vacuum pumps, fans, compressors, blowers, gas (including air) handling or other substance-transfer equipment wholly or partly made from any of the following materials;
a. Nickel or alloys with more than 40% nickel by weight
b. Alloys with more than 25% nickel and 20% chromium by weight (e.g. ‘Hastelloy’, ‘Illium’. ‘Inconel’, ‘Incoloy’)
c. Fluoropolymers
d. Glass or glass lined (including vitrified or enamelled coating)
e. Graphite
f. Tantalum or tantalum alloys
g. Titanium or titanium alloys
h. Zirconium or zirconium alloys
i. Ceramics
j. Ferrosilicon
Note: 3D001 does not control the following items:
a. Open vessels fabricated from glass sheets (such as aquariums, water tanks etc.); or cookware, table-ware, decorative glass or ceramic items (such as vases, art objects, etc.)
b. Glass-ware (whether or not metal-jacketed) or glass-lined reaction vessels or reactors, whether or not equipped with agitators, provided that the total internal (geometric) volume of each vessel or reactor is greater than 20,000 litres (20 m3) or less than or equal to 100 litres (0.1 m3). Examples of the latter capacity glass or ceramic-ware include standard laboratory equipment such as test tubes, flasks, retorts etc.
3D002 Incinerators designed to destroy any chemicals specified in Category 1.
3D003 Combustors or pyrolysers capable of a heat-zone (‘burner’) temperature greater than 1,273 K (1000 Degree Centigrade), and in which any surfaces that come into direct contact with material coming into the containing chamber are made from, or lined with, any of the following materials:

a. Alloys with more than 25% nickel and 25% chromium by weight; (e.g., ‘Hatelloy’, ‘Illium’, ‘Inconel’, ‘Incoloy’)

b. Nickel, or alloys with more than 40% nickel by weight; or

c. Titanium;

d. Ceramics.
 
3D004 Equipment related to P3, P4 facilities such as protective suits and class III safety cabinets.

No licenses shall be granted for complete containment facilities at P3, P4, containment level as specified in the World Health Organization (WHO) bio-safety manual.
3D005 Technology related to the development, production or use of items in 3D
Category 4 Nuclear-related other equipment, assemblies and components; test and production equipment; and related technology not controlled under Category 0
4A Equipment, assemblies, components including test and production equipment
4A001 Flow-forming machines, spin-forming machines capable of flow-forming functions, and mandrels, as follows:

a. For flow forming machines refer to 5A205.

b. Spin forming machines having both of the following characteristics:

1. Three or more rollers (active or guiding); and

2. which can be equipped with ‘numerical control’ units or a computer control.

c. Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 and 400 mm.

Note: Item 4A001a and 4A001b include machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
4A002 Machine tools, as follows, for removing or cutting metals, ceramics, or composites, which, according to the manufacturer’s technical specifications, can be equipped with electronic devices for simultaneous contouring control in two or more axes:

a. Machine tools for turning, that have positioning accuracies with all compensations available better (less) than 6 µm along any linear axis (overall positioning) for machines capable of machining diameters greater than 35mm;

Note: Item 4A002a does not control bar machines, limited to machining only bar feed through, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.

b. Machine tools for milling, having any of the following characteristics:

1. Positioning accuracies with all compensations available better (less) than 6 µm along any linear axis (overall positioning); or

2. Two or more contouring rotary axes;

Note: Item 4A002b does not control milling machines having both of the following characteristics:

1. X-axis travel greater than 2 m; and

2. Overall positioning accuracy on the x-axis worse (more) than 30 µm.

c. Machine tools for grinding, having any of the following characteristics:

1. Positioning accuracies with all compensations available better (less) than 4 µm along any linear axis (overall positioning); or

2. Two or more contouring rotary axes;

Note: Item 4A002c does not control grinding machines as follows:

1. Cylindrical external, internal, and external-internal grinding machines having all the following characteristics:

a. Limited to cylindrical grinding;

b. A maximum work-piece outside diameter or length of 150 mm;

c. Not more than two axes that can be coordinated simultaneously for contouring control; and

d. No contouring c-axis;

2. Jig grinders with axes limited to x, y, c, and a, where c-axis is used to maintain the grinding wheel normal to the work surface, and the a-axis is configured to grind barrel cams;

3. Tool or cutter grinding machines with software specially designed for the manufacturing of tools or cutters;

4. Crankshaft or camshaft grinding machines.

d. Non-wire type Electrical Discharge Machines (EDM) that have two or more contouring rotary axes and that can be coordinated simultaneously for contouring control.

Note: Stated positioning accuracy levels derived under the following procedures from measurements made according to ISO 230/2 (1988) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests. Stated positioning accuracy are to be derived as follows:

1. Select five machines of a model to be evaluated;

2. Measure the linear axis accuracies according to ISO 230/2 (1988);

3. Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230/2 (1988) standard;

4. Determine the average accuracy value of each axis. This average value becomes the stated positioning accuracy of each axis for the model (Âx, Ây...);

5. Since Item 4A002 refers to each linear axis, there will be as many stated positioning accuracy values as there are linear axes;

6. If any axis of a machine tool not controlled by Items 4A002a, 4A002b, or 4A002c has a stated positioning accuracy of 6 µm or better (less) for grinding machines, and 8 µm or better (less) for milling and turning machines, both according to ISO 230/2 (1988), then the builder should be required to reaffirm the accuracy level once every eighteen months.

Technical Notes

1. Axis nomenclature shall be in accordance with International Standard ISO 841, Numerical Control Machines Axis and Motion Nomenclature.

2. Not counted in the total number of contouring rotary axes are secondary parallel contouring rotary axes the centre line of which is parallel to the primary rotary axis.

3. Rotary axes do not necessarily have to rotate over 360 degrees. A rotary axis can be driven by a linear device, e.g., a screw or a rack and-pinion.
4A003 Dimensional inspection machines, instruments, or systems, as follows:

a. Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics:

1. Two or more axes; and

2. A one-dimensional length measurement uncertainty equal to or better (less) than (1.25 + L/1000) µm tested with a probe of an accuracy of better (less) than 0.2 µm (L is the measured length in millimetres);

b. ‘Linear displacement’ measuring instruments, as follows:

1. Non-contact type measuring systems with a resolution equal to or better (less) than 0.2 µm within a measuring range up to 0.2 mm;

2. Linear variable differential transformer (LVDT) systems having both of the following characteristics:

a. Linearity equal to or better (less) than 0.1% within a measuring range up to 5 mm; and

b. Drift equal to or better (less) than 0.1% per day at a standard ambient test room temperature ± 1 K;

3. Measuring systems having both of the following characteristics:

a. Contain a laser; and

b. Maintain for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and a standard pressure:

1. A resolution over their full scale of 0.1 µm or better; and

2. With a measurement uncertainty equal to or better (less) than (0.2 + L/2000) µm (L is the measured length in millimetres);

Note: Item 4A003b3 does not control measuring interferometer systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimensional inspection machines, or similar equipment.

Technical Note: In Item 4A003b ‘linear displacement’ means the change of distance between the measuring probe and the measured object.

c. Angular displacement measuring instruments having an angular position deviation equal to or better (less) than 0.00025°;

Note: Item 4A003c does not control optical instruments, such as autocollimators, using collimated light to detect angular displacement of a mirror.

d. Systems for simultaneous linear-angular inspection of hemi-shells, having both of the following characteristics:

1. Measurement uncertainty along any linear axis equal to or better (less) than 3.5 µm per 5 mm; and

2. Angular position deviation equal to or less than 0.02°.

Notes: 1. Item 4A003 includes machine tools that can be used as measuring machines if they meet or exceed the criteria specified for the measuring machine function.

2. Machines described in Item 4A003 are controlled if they exceed the threshold specified anywhere within their operating range.

Technical Note: All parameters of measurement values in this item represent plus/minus, i.e., not total band.
 
4A004 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:
a. Furnaces having all of the following characteristics:
1. Capable of operation at temperatures above 1123 K (850 °C);
2. Induction coils 600 mm or less in diameter; and
3. Designed for power inputs of 5 kW or more;
Note: Item 4A004a does not control furnaces designed for the processing of semiconductor wafers.
b. Power supplies, with a specified output power of 5 kW or more, specially designed for furnaces specified in Item 4A004a.
4A005 ‘Isostatic presses’, and related equipment, as follows:
a. ‘Isostatic presses’ as specified in 5A208;
b. Dies, moulds, and controls specially designed for the ‘isostatic presses’ specified in Item 4A005a.
Technical Notes:
1. In Item 4A005 ´Isostatic presses’ means equipment capable of pressurizing a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a work piece or material.
2. In Item 4A005 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
4A006 Vibration test systems, equipment, and components as follows:
a. Electrodynamic vibration test systems, having all of the following characteristics:
1. Employing feedback or closed loop control techniques and incorporating a digital control unit;
2. Capable of vibrating at 10 g RMS or more between 20 and 2000 Hz; and
3. Capable of imparting forces of 50 kN or greater measured ‘bare table’;
b. Digital control units, combined with software specially designed for vibration testing, with a real-time bandwidth greater than 5 kHz and being designed for a system specified in Item 4A006a;
c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force of 50 kN or greater measured ‘bare table’, which are usable for the systems specified in Item 4A006a;
d. Test piece support structures and electronic units designed to combine multiple shaker units into a complete shaker system capable of providing an effective combined force of 50 kN or greater, measured ‘bare table,’ which are usable for the systems specified in Item 4A006a.
Technical Note : In Item 4A006 ‘bare table’ means a flat table, or surface, with no fixtures or fittings.
4A007 Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment, as follows:
a. Arc re-melt and casting furnaces having both of the following characteristics:
1. Consumable electrode capacities between 1000 and 20000 cm3; and
2. Capable of operating with melting temperatures above 1973 K (1700 °C);
b. Electron beam melting furnaces and plasma atomisation and melting furnaces, having both of the following characteristics:
1. A power of 50 kW or greater; and
2. Capable of operating with melting temperatures above 1473 K (1200 °C);
c. Computer control and monitoring systems specially configured for any of the furnaces specified in Item 4A007a or 4A007b.
4A008 Crucibles made of materials resistant to liquid actinide metals, as follows:
a. Crucibles having both of the following characteristics:
1. A volume of between 150 cm3 (150 ml) and 8000 cm3 (8 litres); and
2. Made of or coated with any of the following materials, having a purity of 98% or greater by weight:
a. Calcium fluoride (CaF2);
b. Calcium zirconate (metazirconate) (CaZrO3);
c. Cerium sulphide (Ce2S3);
d. Erbium oxide (erbia) (Er2O3);
e. Hafnium oxide (hafnia) (HfO2);
f. Magnesium oxide (MgO);
g. Nitrided niobium-titanium-tungsten alloy (approximately 50% Nb, 30% Ti, 20% W);
h. Yttrium oxide (yttria) (Y2O3); or
i. Zirconium oxide (zirconia) (ZrO2);
b. Crucibles having both of the following characteristics:
1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres); and
2. Made of or lined with tantalum, having a purity of 99.9% or greater by weight;
c. Crucibles having all of the following characteristics:
1. A volume of between 50 cm3 (50 ml) and 2000 cm3 (2 litres);
2. Made of or lined with tantalum, having a purity of 98% or greater by weight; and
3. Coated with tantalum carbide, nitride, boride, or any combination thereof.
4A009 Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.
4A010 Composite structures in the form of tubes having both of the following characteristics:
a. An inside diameter of between 75 and 400 mm; and
b. Made with any of the materials specified in Item 3A116.
4A011 Frequency changers or generators having all of the following characteristics:
a. Multiphase output capable of providing a power of 40 W or greater;
b. Capable of operating in the frequency range between 600 and 2000 Hz;
c. Total harmonic distortion better (less) than 10%; and
d. Frequency control better (less) than 0.1%.
Note: Frequency changers and generators especially designed or prepared for the gas centrifuge process are controlled under Prescribed Equipment (0B Category).
Technical Note: Frequency changers in Item 4A011 are also known as converters or inverters.
4A012 Lasers, laser amplifiers and oscillators as follows:
a. Copper vapour lasers having both of the following characteristics:
1. Operating at wavelengths between 500 and 600 nm; and
2. An average output power equal to or greater than 40 W;
b. Argon ion lasers having both of the following characteristics:
1. Operating at wavelengths between 400 and 515 nm; and
2. An average output power greater than 40 W;
c. Neodymium-doped (other than glass) lasers with an output wavelength between 1000 and 1100 nm having either of the following:
1. Pulse-excited and Q-switched with a pulse duration equal to or greater than 1 ns, and having either of the following:
a. A single-transverse mode output with an average output power greater than 40 W; or
b. A multiple-transverse mode output with an average output power greater than 50 W; or
2. Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of greater than 40 W;
d. Tuneable pulsed single-mode dye laser oscillators having all of the following characteristics:
1. Operating at wavelengths between 300 and 800 nm;
2. An average output power greater than 1 W;
3. A repetition rate greater than 1 kHz; and
4. Pulse width less than 100 ns;
e. Tuneable pulsed dye laser amplifiers and oscillators having all of the following characteristics:
1. Operating at wavelengths between 300 and 800 nm;
2. An average output power greater than 30 W;
3. A repetition rate greater than 1 kHz; and
4. Pulse width less than 100 ns;
Note: Item 4A012e does not control single mode oscillators.
f. Alexandrite lasers having all of the following characteristics:
1. Operating at wavelengths between 720 and 800 nm;
2. A bandwidth of 0.005 nm or less;
3. A repetition rate greater than 125 Hz; and
4. An average output power greater than 30 W;
g. Pulsed carbon dioxide lasers having all of the following characteristics:
1. Operating at wavelengths between 9000 and 11000 nm;
2. A repetition rate greater than 250 Hz;
3. An average output power greater than 500 W; and
4. Pulse width of less than 200 ns;
Note: Item 4A012g does not control the higher power (typically 1 to 5 kW) industrial CO2 lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns. h. Pulsed excimer lasers (XeF, XeCl, KrF) having all of the following characteristics:
1. Operating at wavelengths between 240 and 360 nm;
2. A repetition rate greater than 250 Hz; and
3. An average output power greater than 500 W;
i. Para-hydrogen Raman shifters designed to operate at 16 µm output wavelength and at a repetition rate greater than 250 Hz.
4A013 Valves having all of the following characteristics:
a. A nominal size of 5 mm or greater;
b. Having a bellows seal; and
c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60% nickel by weight.
Technical Note: For valves with different inlet and outlet diameter, the nominal size parameter in Item 4A013a refers to the smallest diameter.
4A014 Superconducting solenoidal electromagnets having all of the following characteristics:
a. Capable of creating magnetic fields greater than 2 T;
b. A ratio of length to inner diameter greater than 2;
c. Inner diameter greater than 300 mm; and
d. Magnetic field uniform to better than 1% over the central 50% of the inner volume.
Note: Item 4A014 does not control magnets specially designed for and exported as part of medical nuclear magnetic resonance (NMR) imaging systems. (‘As part of’ does not necessarily mean physical part in the same shipment. Separate shipments from different sources are allowed, provided the related export documents clearly specify the ‘as part of” relationship.)
4A015 High-power direct current power supplies having both of the following characteristics:
a. Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and
b. Current or voltage stability better than 0.1% over a time period of 8 hours.
4A016 High-voltage direct current power supplies having both of the following characteristics:
a. Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and
b. Current or voltage stability better than 0.1% over a time period of 8 hours.
4A017 Pressure transducers capable of measuring absolute pressures at any point in the range 0 to 13 kPa and having both of the following characteristics:
a. Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel, or nickel alloy with more than 60% nickel by weight; and
b. Having either of the following characteristics:
1. A full scale of less than 13 kPa and an accuracy of better than ± 1% of full scale; or
2. A full scale of 13 kPa or greater and an accuracy of better than ± 130 Pa.
Technical Notes:
1. In Item 4A017 pressure transducers are devices that convert pressure measurements into an electrical signal.
2. In Item 4A017 accuracy includes non-linearity, hysteresis and repeatability at ambient temperature.
4A018 Vacuum pumps having all of the following characteristics:
a. Input throat size equal to or greater than 380 mm;
b. Pumping speed equal to or greater than 15 m3/s; and
c. Capable of producing an ultimate vacuum better than 13.3 mPa.
Technical Notes:
1. The pumping speed is determined at the measurement point with nitrogen gas or air.
2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.
4A019 Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.
4A020 Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:
a. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;
Note: Item 4A020a includes precision mandrels, clamps, and shrink fit machines.
b. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;
Technical Note: In Item 4A020b such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.
c. Bellows-forming mandrels and dies for producing single -convolution bellows.
Technical Note: The bellows referred to in Item 4A020c have all of the following characteristics:
1. Inside diameter between 75 and 400 mm;
2. Length equal to or greater than 12.7 mm;
3. Single convolution depth greater than 2 mm; and
4. Made of high-strength aluminium alloys, maraging steel, or high strength fibrous or filamentary materials.
4A021 Centrifugal multi-plane balancing machines, fixed or portable, horizontal or vertical, as follows:
a. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:
1. Swing or journal diameter greater than 75 mm;
2. Mass capability of from 0.9 to 23 kg; and
3. Capable of balancing speed of revolution greater than 5000 rpm;
b. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:
1. Journal diameter greater than 75 mm;
2. Mass capability of from 0.9 to 23 kg;
3. Capable of balancing to a residual imbalance equal to or less than 0.010 kg x mm/kg per plane; and
4. Belt drive type. 4A022 Filament winding machines and related equipment, as follows:
a. Filament winding machines as specified in 5A206.
b. Coordinating and programming controls for the filament winding machines specified in Item 4A022a;
c. Precision mandrels for the filament winding machines specified in Item 4A022a.
4A023 Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater. Notes:
1. Item 4A023 includes separators capable of enriching stable isotopes as well asthose for uranium.
2. A separator capable of separating the isotopes of lead with a one-mass unit difference is inherently capable of enriching the isotopes of uranium with a three-unit mass difference.
3. Item 4A023 includes separators with the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.
Technical Note: A single 50 mA ion source cannot produce more than 3 g of separated highly enriched uranium (HEU) per year from natural abundance feed.
4A024 Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:
a. Inductively coupled plasma mass spectrometers (ICP/MS);
b. Glow discharge mass spectrometers (GDMS);
c. Thermal ionisation mass spectrometers (TIMS);
d. Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to UF6;
e. Molecular beam mass spectrometers having either of the following characteristics:
1. A source chamber constructed from, lined with or plated with stainless steel or molybdenum, and equipped with a cold trap capable of cooling to 193 K (-80 °C) or less; or
2. A source chamber constructed from, lined with or plated with materials resistant to UF6;
f. Mass spectrometers equipped with a micro-fluorination ion source designed for actinides or actinide fluorides.
Note: Mass spectrometers especially designed or prepared for analyzing on-line samples of uranium hexafluoride are controlled under Prescribed Equipment (0B Category).
4A025 Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:
a. Made of phosphor bronze mesh chemically treated to improve wettability; and
b. Designed to be used in vacuum distillation towers.
4A026 Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:
a. Airtight (i.e., hermetically sealed);
b. A capacity greater than 8.5 m3/h; and
c. Either of the following characteristics:
1. For concentrated potassium amide solutions (1% or greater), an operating pressure of 1.5 to 60 MPa; or
2. For dilute potassium amide solutions (less than 1%), an operating pressure of 20 to 60 MPa.
4A027 Turbo-expanders or turbo-expander-compressor sets having both of the following characteristics:
a. Designed for operation with an outlet temperature of 35 K (- 238 ºC) or less; and
b. Designed for a throughput of hydrogen gas of 1000 kg/h or greater.
4A028 Water-hydrogen sulphide exchange tray columns and internal contactors, as follows:
a. Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:
1. Can operate at pressures of 2 MPa or greater;
2. Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and
3. With a diameter of 1.8 m or greater; b. Internal contactors for the water-hydrogen sulphide exchange tray columns specified in Item 4A028a.
Note: For columns which are especially designed or prepared for the production of heavy water, see Prescribed Equipment (0B002).
Technical Note: Internal contactors of the columns are segmented trays which have an effective assembled diameter of 1.8 m or greater; are designed to facilitate counter current contacting and are constructed of stainless steels with a carbon content of 0.03% or less. These may be sieve trays, valve trays, bubble cap trays or turbo grid trays.
4A029 Hydrogen-cryogenic distillation columns having all of the following characteristics:
a. Designed for operation at internal temperatures of 35 K (-238 ºC) or less;
b. Designed for operation at internal pressures of 0.5 to 5 MPa; c. Constructed of either:
1. Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or
2. Equivalent materials which are both cryogenic and H2-compatible; and d. With internal diameters of 1 m or greater and effective lengths of 5 m or greater.
4A030 Ammonia synthesis converters or synthesis units, in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen high-pressure exchange column and the synthesized ammonia is returned to said column.
4B Equipment, assemblies and components, including test and measurement equipment usable in development of nuclear explosive devices
4B001 Photomultiplier tubes having both of the following characteristics:
a. Photocathode area of greater than 20 cm2; and
b. Anode pulse rise time of less than 1 ns.
4B002 Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:
a. An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and
b. With a figure of merit (K) of 0.25 or greater;
or
a. An accelerator peak electron energy of 25 MeV or greater; and
b. A peak power greater than 50 MW.
Note: Item 4B002 does not control accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes.
Technical Notes:
1. The figure of merit K is defined as: K=1.7 x 103 V2.65Q. V is the peak electron energy in million electron volts. If the accelerator beam pulse duration is less than or equal to 1 µs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 µs, then Q is the maximum accelerated charge in 1 µs. Q equals the integral of i with respect to t, over the lesser of 1 µs or the time duration of the beam pulse ( Q=?idt ) where i is beam current in amperes and t is the time in seconds.
2. Peak power = (peak potential in volts) x (peak beam current in amperes).
3. In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 µs or the duration of the bunched beam packet resulting from one microwave modulator pulse.
4. In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.
4B003 Multistage light gas guns or other high-velocity gun systems (coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 2 km/s or greater.
4B004 Mechanical rotating mirror cameras, as follows, and specially designed components therefor:
a. Framing cameras with recording rates greater than 225000 frames per second;
b. Streak cameras with writing speeds greater than 0.5 mm/µs.
Note: In Item 4B004 components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors, and bearings.
4B005 Electronic streak cameras, electronic framing cameras, tubes and devices, as follows:
a. Electronic streak cameras capable of 50 ns or less time resolution;
b. Streak tubes for cameras specified in Item 4B005a;
c. Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time;
d. Framing tubes and solid-state imaging devices for use with cameras specified in Item 4B005c, as follows:
1. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance;
2. Gate silicon intensifier target (SIT) vidicon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate;
3. Kerr or Pockels cell electro-optical shuttering; 4. Other framing tubes and solid-state imaging devices having a fast image gating time of less than 50 ns specially designed for cameras specified in Item 4B005c.
4B006 Specialized instrumentation for hydrodynamic experiments, as follows:
a. Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 µs;
b. Manganin gauges for pressures greater than 10 GPa; c. Quartz pressure transducers for pressures greater than 10 GPa.
Note: Item 4B006a includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).
4B007 High-speed pulse generators having both of the following characteristics:
a. Output voltage greater than 6 V into a resistive load of less than 55 ohms; and
b. ‘Pulse transition time’ less than 500 ps.
Technical Note: In Item 4B007b ‘pulse transition time’ is defined as the time interval between 10% and 90% voltage amplitude
4B008 Detonators and multipoint initiation systems, as follows:
a. Electrically driven explosive detonators, as follows:
1. Exploding bridge (EB);
2. Exploding bridge wire (EBW);
3. Slapper;
4. Exploding foil initiators (EFI);
b. Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over an area greater than 5000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2.5 µs.
Note: Item 4B008 does not control detonators using only primary explosives, such as lead azide.
Technical Note: In Item 4B008 the detonators of concern all utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. In nonslapper types, the exploding conductor starts a chemical detonation in a contacting high-explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator.
4B009 Firing sets and equivalent high-current pulse generators, as follows:
a. Explosive detonator firing sets designed to drive multiple controlled detonators specified by Item 4B008 above;
b. Modular electrical pulse generators (pulsers) having all of the following characteristics:
1. Designed for portable, mobile, or ruggedized-use;
2. Enclosed in a dust-tight enclosure;
3. Capable of delivering their energy in less than 15 µs;
4. Having an output greater than 100 A;
5. Having a ‘rise time’ of less than 10 µs into loads of less than 40 ohms;
6. No dimension greater than 25.4 cm;
7. Weight less than 25 kg ; and
8. Specified to operate over an extended temperature range of 223º to 373º K (-50 ºC to 100 ºC) or specified as suitable for aerospace applications.
Note: Item 4B009b includes xenon flashlamp drivers.
Technical Note: In Item 4B009b5 ‘rise time’ is defined as the time interval from 10% to 90% current amplitude when driving a resistive load.
4B010 Switching devices as follows:
a. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:
1. Containing three or more electrodes;
2. Anode peak voltage rating of 2.5 kV or more;
3. Anode peak current rating of 100 A or more; and
4. Anode delay time of 10 µs or less;
Note: Item 4B010a includes gas krytron tubes and vacuum sprytron tubes.
b. Triggered spark-gaps having both of the following characteristics:
1. Anode delay time of 15 µs or less; and 2. Rated for a peak current of 500 A or more;
c. Modules or assemblies with a fast switching function having all of the following characteristics:
1. Anode peak voltage rating greater than 2 kV; 2. Anode peak current rating of 500 A or more; and
3. Turn-on time of 1 µs or less.
4B011 Pulse discharge capacitors having either of the following sets of characteristics:
a. 1. Voltage rating greater than 1.4 kV;
2. Energy storage greater than 10 J;
3. Capacitance greater than 0.5 µF; and
4. Series inductance less than 50 nH; or
b. 1. Voltage rating greater than 750 V;
2. Capacitance greater than 0.25 µF; and
3. Series inductance less than 10 nH.
4B012 Neutron generator systems, including tubes, having both of the following characteristics:
a. Designed for operation without an external vacuum system; and
b. Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction.
4C Technology Technology for the development, production or use of items in 4A and 4B.
5 Aerospace systems, equipment including production and test equipment, related technology, and specially designed components and accessories therefor.
5A Rocket Systems (including ballistic missiles, space launch vehicles and sounding rockets)
5A1 Systems 5A101 Systems for missiles and rockets, including:
a. complete rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets)
b. complete rocket stages with engines
c. solid or liquid fuel rocket engines and their control systems including liquid propellant apogee engines designed or modified for satellites
Note: 5A101 does not control JATO units, propulsion units for flares, ejection seats, emergency escape equipment and rockets for display fireworks.
5A102

Subsystems and components usable in missiles and rockets including:
a. rocket motor cases, interior lining, insulation and nozzles;
b. rocket staging mechanisms, separation mechanisms and inter-stages;

c. liquid and slurry propellant (including oxidizers), control systems, and components thereof, specially designed or modified for resistance to vibration;
d. re-entry vehicles and equipment including
1. Heat-shields and components thereof, fabricated of ceramic or ablative materials;
2. Heat sinks and components thereof, fabricated of light weight, high heat capacity materials;
3. Electronic equipment specially designed for re-entry vehicles.
e. guidance systems and their components such as gyros and inertial reference units;
f. thrust-vector control subsystems including methods of achieving thrust vector control such as flexible nozzle, fluid or secondary gas injection, movable engine or nozzle, deflection of exhaust gas stream (jet vanes or probes) and use of thrust tabs;
g. hybrid rocket motors and components thereof;
h. safing, arming, fusing and firing mechanisms for weapons or warhead.
i. software specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.
5A2 Production and Test Equipment. 5A201 Transonic, supersonic, hypersonic wind tunnels; gun tunnels; aeroballistic ranges.
5A202 Test and production equipment and facilities designed to handle systems in 5A1.
5A203 Test benches/stands, usable for complete rocket systems and subsystems (including ballistic missile systems, space launch vehicles and sounding rockets) which have the capacity to handle solid or liquid propellant rockets, motors or engines, or which are capable of simultaneously measuring the three axial thrust components.
5A204 Vibration test equipment (vibration test systems and vibration thrusters) and components using digital control techniques and feedback or closed loop test equipment and software thereof (Refer 4A006).
5A205 Flow-forming machines and specially designed components thereof which, according to the manufacturers technical specification,
1. can be equipped with numerical control units or a computer control, even when not equipped with such units at delivery; and
2. have more than two axes which can be coordinated simultaneously for contouring control.
Note: Item 5A205 includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.
5A206 Filament winding machines for which the motion for positioning wrapping and winding fibres can be coordinated and programmed in two or more axes; precision mandrels thereof, and coordinating and programming controls;
5A207 Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes;
5A208 Isostatic presses having all of the characteristics of maximum working pressure equal to or greater than 69 MPa or greater; designed to achieve and maintain a controlled thermal environment of 600oC or greater; and possessing a chamber cavity with an inside diameter of 152 mm or greater.
5A209 Environmental chambers simulating vibration environments, with altitudes equal to or greater than 15 km, or temperature ranging between minus 50 and plus 125 degrees centigrade.
5A210 Environmental chambers simulating acoustic pressure level of 140 dB or greater or rated acoustic power output of 4 KW or greater, with altitudes equal to or greater than 15 km, or temperature ranging between minus 50 and plus 125 degrees centigrade.
5A211 Accelerators delivering electro-magnetic radiation produced by Bremsstrahlung from accelerated electrons.
5A212 Pulsed electron accelerators
5A213 Radial ball bearings having all tolerances specified in accordance with ISO 492 Tolerance Class 2 or better and having all the following characteristics:
a. An inner ring bore diameter between 12 and 50 mm;
b. An outer ring outside diameter between 25 and 100 mm; and
c. A width between 10 and 20 mm.
5A214 Liquid propellant tanks specially designed for the propellants controlled in Item 3A3 or other liquid propellants used in the systems specified in 5A and 5B.
5A215 Production facilities and production equipment specially designed for equipment or materials for 5A101 and 5A102.
5A216 Production equipment and specially designed components thereof, for the production, handling or acceptance testing of liquid propellants or propellant constituents as referred in 3A3;
5A217 Launch and ground support equipment and facilities usable for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned airborne system and cruise missiles as follows:-
a. apparatus, devices and vehicles, designed or modified for the transport, handling, control, activation and launching of the systems.
b. gravity meters (gravimeters), gravity gradiometers, and specially designed components thereof, designed or modified for airborne or marine use usable for complete rocket systems and for complete unmanned aerial vehicle systems (including cruise missile systems target drones and reconnaissance drones)
c. telemetry and tele-command equipment, including ground equipment, designed or modified for complete rocket systems and complete unmanned aerial vehicle systems and cruise missiles, excluding control equipment designed or modified for manned aircraft or satellites, control ground based equipment designed or modified for terrestrial or marine application, and control equipment designed for commercial, civil or ‘safety of life’ (e.g. data integrity, flight safety) GNSS services
d. radomes designed to withstand a combined thermal and pressure shock usable in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (eg. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
e. Software which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path.
5A218 Systems, specially designed for radar cross section measurement, usable for rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned airborne system and cruise missiles and their subsystems.
5A3 Technology
5A301 Technology related to the development, production, testing and use of items in 5A1 and 5A2.
5A302 Software for the development, production, and testing and use of items in 5A1 and 5A2.
5A303 Software which coordinates the function of more than one subsystem, specially designed or modified for use in the systems specified in 5A1 and 5A2.
5B Unmanned aerial vehicles including cruise missiles, target drones and reconnaissance drones and related equipment, and specially designed components therefor:
a. Unmanned aerial vehicles including Remotely Piloted air Vehicles (RPVs) and autonomous programmable vehicles;
b. Associated launchers and ground support equipment;
c. Related equipment for command and control.
d. Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones)
e. Light weight Turbojet and turbofan engines (including turbo compound engines).
f. Ramjet / Scramjet / pulse jet/ combined cycle engines, including devices to regulate combustion, and specially designed components.
g. Complete unmanned aerial vehicle systems having an autonomous flight control and navigation capability or capability of controlled flight out of the direct vision range involving a human operator, designed or modified to incorporate an aerosol dispensation mechanism, or capable of carrying elements of a payload in the form of a particulate or liquid other than fuel components of such vehicles.
Note: This category does not control unpowered airborne vehicles such as gliders, hot air balloons etc.
h. Safing, arming, fusing and firing mechanisms for weapons or warhead.
i Production facilities and Production equipment specially designed for equipment or materials for 5B.
j. Technology, for the development, production or use of equipment, materials or software specified for 5B.
k. Software, for the development, production or use of equipment or materials specified for 5B.
l. Software which coordinates the function of more than one subsystem, specially designed or modified for use in the systems specified in 5B.
5C Avionics and navigation systems designed or modified for use in, or usable in rocket systems (including ballistic missile systems, space launch vehicles and sounding rockets), unmanned aerial vehicles and cruise missiles
5C001 Guidance systems and their components such as gyros and inertial reference units, and specially designed components therefor;
5C002 Integrated flight instrument systems which include gyrostabilizers or automatic pilots, and specially designed components therefor;
5C003 Compasses (including gyro-astro compasses), gyroscopes, accelerometers and inertial equipment and specially designed software thereof and specially designed components therefor.
5C004 Inertial or other equipment using accelerometers or systems incorporating such equipment, and specially designed integration software therefor;
5C005 Encrypted telemetry systems, equipment and software thereof.
5C006 Flight control system (including servo valves) designed or modified for the systems as follows:
a. Hydraulic, mechanical, electro-optical or electro-mechanical flight control systems (including fly-by-wire systems);
b. Attitude control equipment;
c. Design technology for integration of flight control, guidance, and propulsion data into a flight management system for optimisation of rocket system trajectory.
d. Specially designed test, calibration, and alignment thereof.
5C007 Integrated navigation system incorporating an inertial measurement device (example: an attitude and heading reference system, inertial reference unit, or inertial navigation system); one or more external sensor used to update the position and/or velocity, either periodically or continuously throughout the flight (example: satellite navigation receiver, radar altimeter and/or Doppler radar); integration hardware and software
5C008 Production equipment and other test, calibration and alignment equipment, designed or modified to be used with equipment specified in 5C001 – 5C004 and 5C007.
5C009

Equipment used to characterize mirrors for laser gyros such as scatterometer, reflectometer and profilometer and for other inertial equipments such as Inertial measurement unit (IMU Module) tester, IMU Platform tester, IMU stable element handling fixture, Gyro tuning test station, Gyro dynamic balance station, Gyro run-in/motor test station, Gyro evacuation and filling station, Centrifuge fixture for gyro bearings, Accelerometer axis align station  and Accelerometer test station.
5C010 Avionics equipment and embedded or specially designed software and components thereof, including but not limited to:
a. Radar and laser radar system including altimeter;
b. Electronic assemblies and components;
c. Design technology for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards from external sources.
d. Passive sensors for determining bearings to electromagnetic sources (direction finding devices) or terrain characteristics
e. Receiving equipment for Global Navigation Satellite Systems (GNSS: e.g. GPS, GLONASS, GALILEO), capable of operating at aircraft speeds and altitudes or above.
f. Terrain contour mapping equipment, Scene mapping and correlation (both digital and analogue) equipment, Doppler navigation radar equipment, Passive interferometer equipment and Imaging sensor equipment (both active and passive)
g. Design technology for electromagnetic shielding systems, the configuration of hardened electrical circuits and subsystems and for the determination of hardening criteria.
5C011 On-board electronic equipment, devices and their design and manufacturing know-how (except warhead fuses, timers and sequencers), and embedded or specially designed software thereof.
5C012 Detectors designed or modified, in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (eg. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
5C013 Radiation Hardened microcircuits usable in protecting rocket systems, unmanned aerial vehicles and cruise missiles against nuclear effects (e.g. electro-magnetic pulse (EMP), X-rays, combined blast and thermal effects).
5C014 Precision tracking systems using a code translator installed on the rocket or unmanned aerial vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurement of inflight position and velocity; Range instrumentation radars including associated optical/infrared trackers and related software.
5C015 Balancing machines capable of balancing rotors/assemblies and correcting unbalance in two planes or more.
5C016 Indicator heads or balancing instrumentation designed or modified for use with balancing machines
5C017 Motion simulators/rate tables (equipment capable of simulating motion) having all of the following characteristics two axes or more slip rings capable of transmitting electrical power and/or signal information
5C018 Position tables (equipment capable of precise rotary positioning in any axes) having two axes or more and a position accuracy equal to or better than 5 arc second
5C019 Centrifuges capable of imparting accelerations and having slip rings capable of transmitting electrical power and signal information
5C020 Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces designed or modified for the unmanned aerial vehicle systems to optimize aerodynamic performance throughout the flight regime of an unmanned aerial vehicle system
5C021 Design technology for integration of the flight control, guidance, and propulsion data into a flight management system, designed or modified for the complete rocket systems, unmanned aerial vehicles and cruise missiles for optimization of the trajectory.
5C022 Technology for the development, production, or use of items in 5C.
5C023 Software for the development, production and use of items in 5C.
5C024 Software specially designed or modified for use in the systems specified in 5C.
5D Manned-aircraft, aero-engines, related equipment and components:
Note: This category does not control foreign military aircraft or an Indian aircraft carrying a military registration number.
5D001 Combat aircraft and specially designed components thereof;
a. Other aircraft specially designed or modified for military use, including military reconnaissance, assault, military training, transporting and air-dropping troops or military equipment, logistics support, and specially designed components thereof;
b. Aero-engines specially designed or modified for military use, and specially designed components thereof;
c. Airborne equipment, including airborne refuelling equipment, specially designed for use with the aircraft controlled by 5D001a or 5D001b or the aero-engines controlled by 5D001c, and specially designed components thereof;
d. Pressure refuellers, pressure refuelling equipment, equipment specially designed to facilitate operations in confined areas and ground equipment, developed specially for aircraft controlled by 5D001a or 5D001b or for aero-engines controlled by 5D001c;
e. Pressurized breathing equipment and partial pressure suits for use in aircraft anti-g suits, military crash helmets and protective masks, liquid oxygen converters used for aircraft or missiles, and catapults and cartridge actuated devices for emergency escape of personnel from aircraft;
f. Parachutes:
1. Paragliders, drag parachutes, drogue parachutes for stabilization and attitude control of dropping bodies, (e.g. recovery capsules, ejection seats, bombs);
2. Drogue parachutes for use with ejection seat systems for deployment and inflation sequence regulation of emergency parachutes;
3. Recovery parachutes for guided missiles, drones or space vehicles;
4. Approach parachutes and landing deceleration parachutes.
g. Automatic piloting systems for parachuted loads, equipment specially designed or modified for military use for controlled opening jumps at any height, including oxygen equipment.
Note 1: 5D001b does not control aircraft or variants of those aircraft specially designed for military use which:
1. Have been certified for civil use by the civil aviation authority of India, and
2. Are not configured for military use and are not fitted with equipment or attachments specially designed or modified for military use;
Note 2: The control in 5D001b and 5D001c on specially designed components and related equipment for non-military aircraft or aero-engines modified for military use applies only to those military components and to military related equipment required for the modification to military use.
5E Microlight aircraft and powered ‘hang-gliders’
Category 6 [Reserved]
Category 7: Electronics, computers, and information technology including information security
7A Electronics
7A001 High-power microwave devices including tubes, travelling wave tubes (TWT) and phase shifters, and continuous wave and pulsed high power microwave travelling wave tube amplifiers (TWTA) operating at frequencies higher than 31 GHz, and their power supplies.
7A002 Microwave monolithic integrated circuits (MMIC) operating at frequencies above 3 GHz and surface acoustic wave (SAW) devices operating at frequencies above 2.5 GHz.
7A003 Phased array antennas and their elements
7A004 Radiation-hardened microprocessors, field programmable gate arrays and solid state memory devices
7A005 Microprocessor microcircuits, microcomputer microcircuits, microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converter, and digital-to-analogue converter, printed circuit boards or modules, electro-optical or optical integrated circuits designed for signal processing, field programmable logic devices, neural network integrated circuits, custom integrated circuits for which either the function is unknown or the control status of the equipment in which the integrated circuit will be used is unknown, Fast Fourier Transform (FFT) processors, electrical erasable programmable read-only memories (EEPROMs), flash memories or static random-access memories (SRAMs), having any of the following:
a. Rated for operation at an ambient temperature above 398 K (+125°C);
b. Rated for operation at an ambient temperature below 218 K (-55°C); or
c. Rated for operation over the entire ambient temperature range from 218 K (-55°C) to 398 K (+125°C).
7A006 Radiation-hardened analogue-to-digital and digital-to-analogue converter integrated circuits, as follows:
a. Analogue-to-digital converters having any of the following:
1. A resolution of 8 bit or more, but less than 12 bit, with a total conversion time of less than 5 ns;
2. A resolution of 12 bit with a total conversion time of less than 200 ns; or
3. A resolution of more than 12 bit with a total conversion time of less than 2 µs;
b. Digital-to-analogue converters with a resolution of 12 bit or more, and a settling time of less than 10 ns.
7A007 Detector units operating in the thermal infrared, ultraviolet, x-ray and gamma ray spectrum.
7A008 Focal plane assemblies for imaging cameras operating in the visible, near and thermal infrared spectrum
7A009 Technology for the development, production or use of items specified in 7A005 and 7A006.
7B Electronic test equipment
7B001 Frequency synthesized signal generators with maximum frequency greater than 31 GHz
7B002 Network analysers operating at frequencies above 40 GHz
7C Computers
7C001 Digital computers and software as follows:
a. Digital computers having a composite theoretical performance (CTP) exceeding 75000 (seventy-five thousand) million theoretical operations per second (Mtops)
b. Software, and/or computer inter-connection schemes, whether or not co-supplied with (a) designed to ‘parallelise’ digital computers (individually of any CTP rating) enabling a CTP of more than 75000 Mtops to be achieved by the ‘parallelised’ configuration
Technical notes: 1. The Composite Theoretical Performance (CTP) rating is to be calculated in accordance with the calculation scheme separately notified in this regard.
2. Individual digital computers each with a CTP rating of 75000 Mtops or less do not require an export license to any destination or end-user, unless supplied with (b) above.
3. Digital Computers’ includes (1) hybrid computers incorporating ‘digital computers’ or specified in (a) above, systolic array computers, neural computers, optical computers, vector processors, digital signal processors, logical processors (2) digital electronic equipment designed for ‘image enhancement’ or signal processing other than when supplied as integral adjuncts to medical imaging (eg CAT-scanning) equipment.
7C002 Analogue, digital or hybrid computers, digital differential analysers, and specially designed software therefor, for use in, or for modelling, simulation, or design integration of rocket systems, unmanned aerial vehicles and cruise missiles.
7C003 Technology for the development, production or use of items in 7C002.
7D Information technology including information security
7D001 Data processing security equipment, data security equipment and transmission and signalling line security equipment, using ciphering processes.
7D002 Identification, authentication and keyloader equipment and key management, manufacturing and distribution equipment.
7E [Reserved]

]
 

ANNEXURE - 1

PROFORMA FOR
INFORMATION TO BE SUBMITTED BY SUPPLIER IN DOMESTIC TARIFF AREA (DTA) TO DEVELOPMENT COMMISSIONER, SEZ FOR SUPPLY OF SCOMET ITEMS TO SEZ UNITS UNDER NOTIFICATION NO. 93 (RE-2010)/2009-2014 DATED 6TH JANUARY, 2012

(Report to be submitted within 1(one) week of the supplies getting effected)

1. Name and address of the Development Commissioner, SEZ :
2. Name and address of the Supplier :
3. Importer-Exporter Code (IEC) :
4. Details of SCOMET items supplied :
Sl. No. Description of items SCOMET Category ITC(HS) Code, if available Qty SEZ Unit to which supplied Date of Supply FOB Value
Rs US$
                 
                 
                 
                 
5. I hereby declare that I am authorized to verify and sign this declaration.
Date : Signature :

Name :
Place : Designation :

Telephone :

FAX :

Email address :


ANNEXURE - 2

PROFORMA FOR

INFORMATION TO BE SUBMITTED ANNUALLY(*) BY DEVELOPMENT COMMISSIONER, SEZ TO SCOMET CELL, DGFT (HQRS), DEPARTMENT OF COMMERCE, UDYOG BHAWAN, MAULANA AZAD ROAD, NEW DELH – 110011, UNDER NOTIFICATION NO. 93 (RE-2010)/2009-2014 DATED 6TH JANUARY, 2012
 

1. Name of the SEZ :
2. Details of SCOMET items supplied from DTA :
Sl. No. Description of items SCOMET Category ITC(HS) Code, if available Qty Name of Supplier Importer-Exporter Code (IEC) SEZ Unit to which supplied Date of Supply FOB Value
Rs US$
                     
                     
                     
                     


Official Seal/Stamp :


Date :		 Signature of Development Commissioner/ authorized officer of the SEZ


Name :

Designation :

Telephone :

FAX :

Email address :


(*) Note : Report to be submitted by 15thMay of every financial year for the supplies effected during the preceding financial year. [ e.g. Report for the period 1st April 2011 to 31st March 2012 must be submitted by 15th May 2012.]
 

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