GOVERNMENT OF INDIA
MINISTRY OF COMMERCE AND INDUSTRY
DEPARTMENT OF COMMERCE
NOTIFICATION No.38 (RE-2010) /2009-2014
DATED: 31st MARCH, 2011
S.O. (E) In exercise of powers conferred by Section 5 and Section 14 A of the
Foreign Trade (Development & Regulation) Act, 1992 {FT(D&R) Act,1992} as amended
in 2010, the Central Government hereby notifies the list of specified goods,
services and technologies, i.e. Special Chemicals, Organisms, Materials,
Equipment and Technologies (SCOMET) as per Annexure to this notification. Export
of SCOMET items included in the Annexure shall be regulated as per conditions
enumerated in the Annexure. 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 Annexure.
- Annexure to this notification will replace the existing ‘Appendix 3’ to
Schedule- 2 of ITC (HS) Classifications of Export and Import Items, 2009-14.
- Purpose of the notification: The FT(D&R) Act,1992 was amended in 2010. By
this amendment, a new Chapter IV A has been introduced in the FT(D&R) Act,1992.
It deals with controls on export of specified goods, services and technologies
and empowers the Central Government to notify list of such goods, services and
technologies. This notification lists the goods, services and technologies to
which provisions of Chapter IV A of the FT (D&R) Act, 1992 as amended in 2010
shall apply. ‘Appendix 3’ to Schedule 2 of ITC (HS) Classifications of Export
and Import Items, popularly known as SCOMET List, would accordingly be replaced
by this list.
(Anup K. Pujari)
Director General of Foreign Trade
[email protected]
Phone : 23063436, 23062777
(Issued from File No. 01/91/171/14/AM-11/Export Cell)
Annexure to Notification No. 38
Dated 31st March, 2011
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.
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:
- Accept data;
- Store data or instructions in fixed or alterable (writable) storage
devices;
- Process data by means of a stored sequence of instructions which is
modifiable; and
- 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:
- Continuous “monofilaments”;
- Continuous “yarns” and “rovings”;
- “Tapes”, fabrics, random mats and braids;
- Chopped fibres, staple fibres and coherent fibre blankets;
- Whiskers, either monocrystalline or polycrystalline, of any length;
- Aromatic polyamide pulp.
“Hybrid computer” means equipment which can perform all of
the following:
- Accept data;
- Process data, in both analogue and digital representations; and
- 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:
- 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’;
- Can be considered as indivisibly associated; and
- 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 :
- Sold from stock at retail selling points without restriction, by means
of:
-
- Over-the-counter transactions;
- Mail order transactions; or
- Telephone call transactions; and
- 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:
- the development, production or use of any goods or software;
- 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 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.
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.
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 ( <C10 , incl. cycloalkyl) alky1 (Me, Et,n-Pr or i-Pr)
phosphonofluoridates |
|
e.g. Sarin: O-Isopropy1 methylphosphonofluoridate |
|
Soman: O-Pinacolyl methylphosphonofluoridate |
|
|
(2). O-Alkyl, ( <C10, incl. cycloalkyl) N,N-dialky1 (Me, Et, n-Pr or i-Pr)
phosphoramidocyanidates |
|
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, toxinsbr
|
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: |
22A001 |
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 tuberculosisbr |
22A016 |
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 |
ibrio 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 |
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:
- Select five machines of a model to be evaluated;
- Measure the linear axis accuracies according to ISO 230/2 (1988);
- 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;
- Determine the average accuracy value of each axis. This average value becomes
the stated positioning accuracy of each axis for the model (Âx, Ây...);
- Since Item 4A002 refers to each linear axis, there will be as many stated
positioning accuracy values as there are linear axes;
- 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 Iem 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 |
|
|
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
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 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. 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 |
|
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] |
|