APPENDIX-3
- Document type
- Policy
- Dated
List of Special Chemicals, Organisms , Materials , Equipment and Technologies permitted for export against the export licences issued in this behalf (Part - II)
(Please refer NTF. NO.27/2007, DT. 07/09/2007 for amended Appendix 3 - List of Special Chemicals, Organisms, Materials, Equipment and Technologies)
[OLD- Part - II of APPENDIX-3 to Schedule 2 of ITC(HS) (HS) Classification
PRIVIOUS
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 having all of the following characteristics:
1. Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;
2. Specially designed to fabricate composite structures or laminates from “fibrous or filamentary materials”; and
3. Capable of winding cylindrical rotors of diameter between 75 and 400 mm, and length of 600 mm or greater.
b. Coordinating and programming controls for the filament winding machines specified in Item 4A022a;
c. Precision mandrels for the filament winding machines specified in Item 4A022a.
4A023 - Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.
Notes:
1. Item 4A023 includes separators capable of enriching stable isotopes as well as those for uranium.
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 223 to 373 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, and related technology |
| 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, unguided rocket-propelled munitions, propulsion units for flares, ejection seats, emergency escape equipment and rockets for display fireworks. |
| 5A102 |
Subsystems and components for missiles and rockets including: a. rocket motor cases, interior lining, insulation and nozzles; b. rocket staging mechanisms, separation mechanisms and inter-stages; c. liquid and slurry propellant (including oxidizers), control systems, and components thereof, specially designed or modified for resistance to vibration; d. re-entry vehicles and equipment including 1. Heat-shields and components thereof, fabricated of ceramic or ablative materials; 2. Heat sinks and components thereof, fabricated of light weight, high heat capacity materials; 3. Electronic equipment specially designed for re-entry vehicles. e. guidance systems and their components such as gyros and inertial reference units; f. thrust-vector control subsystems including methods of achieving thrust vector control such as flexible nozzle, fluid or secondary gas injection, movable engine or nozzle, deflection of exhaust gas stream (jet vanes or probes) and use of thrust tabs; g. hybrid rocket motors and components thereof; h. safing, arming, fusing and firing mechanisms for weapons or warhead. |
| 5A2 | Production and Test Equipment |
| 5A201 | Supersonic, hypersonic wind tunnels; gun tunnels; aeroballistic ranges. |
| 5A202 | Test and production facilities designed to handle solid or liquid fuel rockets, rocket stages, re-entry vehicles. |
| 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 are coordinated and programmed in three 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 are 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, high altitudes or temperature ranging between minus 50 and plus 125 degrees centigrade. |
| 5A210 | Anechoic chambers simulating acoustic environment with sound pressure level greater than 140 dB or rated power greater than 4 KW. |
| 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 | “Production facilities” and “production equipment” specially designed for equipment or materials for 5A101 (b and c) and 5A102(a – h) |
| 5A215 | Technology” , for the “development”, “production” or “use” of equipment, materials or “software” specified for 5A101 (b and c) and 5A102(a – h) and 5A214. |
| 5A216 | Software specially designed or modified for the use of production facilities for rocket motors / engines, guidance sets/ and those systems specified in 5A101 (b and c) and 5A102(a – h) |
| 5A217 | “Production equipment” and specially designed components thereof, for the “production”, handling or acceptance testing of liquid propellants or propellant constituents as referred in 3A3; |
| 5A218 |
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 but not control equipment designed or modified for manned aircraft or satellites, control ground based equipment designed or modified for terrestrial or marine application, 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). |
| 5A3 |
Technology Technology related to the production and testing of items 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 designed or modified to dispense an aerosol, capable of carrying elements of a payload in the form of a particulate or liquid other than fuel components of such vehicles, and having an autonomous flight control and navigation capability; or capability of controlled flight out of the direct vision range involving a human operator. Note: This category does not control unpowered airborne vehicles such as gliders, hot air balloons etc. h. Production facilities” and “Production equipment” specially designed for equipment or materials for 5B. i. Technology”, for the “development”, “production” or “use” of equipment, materials or “software” specified for 5B. |
| 5C | Avionics and navigation systems designed or modified for use 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 |
| 5C002 | Integrated flight instrument systems which include gyrostabilizers or automatic pilots |
| 5C003 | Compasses (including gyro-astro compasses), gyroscopes, accelerometers and inertial equipment and specially designed software thereof and specially designed components thereof. |
| 5C004 | Inertial or other equipment using accelerometers or systems incorporating such equipment, and specially designed integration software thereof; |
| 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 optimization of rocket system trajectory. d. Specially designed test, calibration, and alignment thereof. e. “Software” specially designed or modified for the “use” of systems specified above. |
| 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, electromagnetic sources (direction finding devices) or terrain characteristics e. Receiving equipment for Global Navigation Satellite Systems (GNSS: i.e. GPS, GLONASS, GALILEO), capable of operating at high speeds and altitudes. 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 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 (eg. 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 | “Software” and Integration “Software” designed or modified for the inertial navigation systems |
| 5D |
Manned-aircraft, aero-engines, related equipment and components: Note: This category does not control foreign military aircraft or an Indian aircraft carrying a military registration number. |
| 5D001 |
Combat “aircraft” and specially designed components thereof; a. Other “aircraft” specially designed or modified for military use, including military reconnaissance, assault, military training, transporting and air-dropping troops or military equipment, logistics support, and specially designed components thereof; b. Aero-engines specially designed or modified for military use, and specially designed components thereof; c. Airborne equipment, including airborne refuelling equipment, specially designed for use with the aircraft controlled by 5D001a or 5D001b or the aero-engines controlled by 5D001c, and specially designed components thereof; d. Pressure refuellers, pressure refuelling equipment, equipment specially designed to facilitate operations in confined areas and ground equipment, developed specially for “aircraft” controlled by 5D001a or 5D001b or for aero-engines controlled by 5D001c; e. Pressurized breathing equipment and partial pressure suits for use in “aircraft” anti-g suits, military crash helmets and protective masks, liquid oxygen converters used for “aircraft” or missiles, and catapults and cartridge actuated devices for emergency escape of personnel from “aircraft”; f. Parachutes: 1. Paragliders, drag parachutes, drogue parachutes for stabilization and attitude control of dropping bodies, (e.g. recovery capsules, ejection seats, bombs); 2. Drogue parachutes for use with ejection seat systems for deployment and inflation sequence regulation of emergency parachutes; 3. Recovery parachutes for guided missiles, drones or space vehicles; 4. Approach parachutes and landing deceleration parachutes. g. Automatic piloting systems for parachuted loads, equipment specially designed or modified for military use for controlled opening jumps at any height, including oxygen equipment. Note 1: 5D001b does not control “aircraft” or variants of those “aircraft” specially designed for military use which: 1. Have been certified for civil use by the civil aviation authority of India, and 2. Are not configured for military use and are not fitted with equipment or attachments specially designed or modified for military use; Note 2: The control in 5D001b and 5D001c on specially designed components and related equipment for non-military “aircraft” or aero-engines modified for military use applies only to those military components and to military related equipment required for the modification to military use. |
| 5E | Microlight aircraft and powered ‘hang-gliders’ |
| Category 6: | [RESERVED] |
| Category 7: | Electronics, computers, and information technology including information security |
| 7A | Electronics |
| 7A001 | High-power microwave devices including tubes, travelling wave tubes (TWT) and phase shifters, and continuous wave and pulsed high power microwave travelling wave tube amplifiers (TWTA) operating at frequencies higher than 31 GHz, and their power supplies. |
| 7A002 | Microwave monolithic integrated circuits (MMIC) operating at frequencies above 3 GHz and surface acoustic wave (SAW) devices operating at frequencies above 2.5 GHz. |
| 7A003 | Phased array antennas and their elements |
| 7A004 | Radiation-hardened microprocessors, field programmable gate arrays and solid state memory devices |
| 7A005 |
“Microprocessor microcircuits”, “microcomputer microcircuits”, microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analogue-to-digital converters, digital-to-analogue converters, 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 |
| 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 | Specially designed software, and/or related specially designed analogue or hybrid computers, digital differential analysers for modelling, simulation, or design integration of rocket systems, unmanned aerial vehicles and cruise missiles. |
| 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] |
(Above Appendix 3 to Schedule 2 has been amended vide NTF NO. 15/2005, DT. 15/07/2005)
[OLD-
List of Special Chemicals, Organisms , Materials , Equipment and Technologies permitted for export against the export licences issued in this behalf
Note: Please see the Policy stated at Code No. 0005 in Table A of Schedule 2 of ITC(HS) Classifications of Export and Import items
Export of Special Chemicals, Organisms, Materials, Equipment and Technologies (SCOMET) listed below shall be permitted only against an export license issued in this behalf unless it is prohibited or permitted without a licence subject to fulfillment of conditions, if any, as indicated under/against any specific category or item.
Note 1: Export or attempt to export in violation of any of the conditions of license to export shall, inter alia, and without prejudice to prosecution under any other Act for the time being in force, invite criminal prosecution under the Customs Act, 1962.
Note 2: Export of items listed in this schedule, (other than those listed under Categories 0, 1 and 2) solely for the purposes of display/exhibition abroad are subject to condition of re-import within a period not exceeding six months from the date of exports. Exporters are entitled to apply for a standard SCOMET export license for such items exhibited abroad if offered for sale during the exhibition abroad. Such sale shall not take place without a valid SCOMET license.
Exhibition licenses will not require any end-use/end-user certifications.
(No exhibition licences shall be issued for items under categories 0, 1 and 2)
Note 3: The export of items in Category 2 of this list may also be controlled by other applicable guidelines issued from time-to-time. Exporters of items in this category are advised to seek guidance from the DGFT.
Note 4: Destination License: Exporters are entitled to apply for a ‘destination license’ for countries and/or group of countries for export to which only re-export conditionalities need be imposed. Exporters may also request that only such conditions need be imposed as are the subject of government-to-government instruments of accord over export of some or all SCOMET items.
Note: The licensing authority for items in this category is the Department of Atomic Energy. Export of these items is regulated under Sections 14 & 16 of the Atomic Energy Act, 1962 and rules framed, and notifications/orders issued thereunder from time-to-time by the Department of Atomic Energy. An application for licenses to export prescribed equipment or/and prescribed substances shall be made in writing to the Joint Secretary, Department of Atomic Energy, Anushakti Bhavan, Chatrapathi Shivaji Marg, Mumbai - 400 001.
(Please refer POLICY CIR NO. 11/2005-09, DT. 27/06/2005 - Re-assignment of 8 digit Codes of ITC(HS) to the Scheduled Chemicals of CWC as given against Category 1 B and 1 C to Appendix 3 to Schedule 2 of ITC(HS) Classification of Export & Import items, 2004-2009)
| 0A | Prescribed substances |
| 0A001 | Uranium, its compounds and minerals/ores/concentrates containing uranium including tailings containing uranium. |
| 0A002 | Thorium, its compounds and minerals/concentrates containing thorium including monazite. |
| 0A003 | Zirconium, its alloys and compounds and minerals/concentrates including zircon. |
| 0A004 | Beryllium, its compounds and its minerals/concentrates including beryl but excluding beryllium windows used for medical x-ray machines and gamma ray machines. |
| 0A005 | Lithium, its compounds and its minerals/concentrates including lepidolite. |
| 0A006 | Deuterium and its compounds (including Heavy Water) |
| 0A007 | Plutonium and its compounds. |
| 0A008 | Neptunium and its compounds. |
| 0A009 | Columbite and Tantalite. |
| 0A010 | Titanium ores and concentrates (ilmenite, rutile, and leucoxene) |
| 0A011 | Nuclear grade graphite |
| 0A012 | Tritium and its compounds. |
| 0B | Prescribed equipment |
| 0B001 | Nuclear reactors; associated equipment, components and systems specially designed or adapted or used or intended to be used in such reactors. |
| 0B002 | Plants for processing of Prescribed Substances, associated equipment, components and systems specially designed or adapted or used or intended to be used in such plants. |
| 0B003 | Plants for reprocessing of irradiated nuclear fuel and plants for treatment of radioactive wastes from nuclear reactors or from plants for processing Prescribed Substances or from nuclear reprocessing plants, associated equipment, components and systems specially designed or adapted or used or intended to be used in such plants. |
| 0B004 | Plants or systems for production, handling, storage and transportation of radioisotopes in quantities exceeding 100 Curies (3.7 x 1012 (ten-raised-to-the-power-twelve) Becquerel). |
| 0B005 |
Equipment specially used for handling, storage and transportation of: a) radioactive wastes from nuclear reactors or from plants for processing Prescribed Substances or from nuclear reprocessing plants; b) irradiated nuclear fuel; c) plutonium; d) plutonium containing fuel. |
| 0B006 | All systems, associated equipment and components for use in isotope enrichment. |
| 0B007 | All systems, associated equipment and components for the manufacture of nuclear fuel. |
| 0B008 | Neutron generators including neutron chain reacting assemblies and fusion assemblies of all kinds for producing fissile materials. |
| 0B009 | High power lasers giving an output in excess of 10 joules in a pulse duration less than 100 pico seconds, or an oscillator-amplifier laser chain capable of delivering greater than 500 joules in 1 nano second. |
| 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) 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 considered prohibited unless explicitly exempted. (1) O-Alky( e.g. Sarin: O-Isopropy1 methylphosphonofluoridate Soman: O-Pinacolyl methylphosphonofluoridate (2) O-Alkyl(, incl. Cycloalkyl) N,N-dialky1 (Me Et,n-Pr or I-Pr) phosphoramidocyanidates e.g. Tabun: O-Ethyl N,N,-dimethyl phosphoramidocyanidates (3) O Alkyl(H or, 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-disopropylaminoethyl methyl phosphonothiolate (4) Sulfur mustards:
Mustard gas: Bis(2-chloroethyl)sulfide 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
Lewisite 2: Bis (2-Chlorovinyl) chloroarsine Lewisite 3: Tris (2-Chlorovinyl) arsine
HN2: Bis(2-chloroethyl) Chloroarsine HN3: Tris(2-chloroethyl) amine (8) Ricin (9) Alkyl (Me, Et, n-Pr or I-Pr) phosphonyldifluorides e.g. DF: Methyl phosphonyldifluoride (10) O-Alkyl (H or , 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 Chemical 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. 40-G, South Block, New Delhi) or at the official website of the Organisation 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 & Petro-chemicals 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 considered prohibited 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 Dimethyle ethylphosphonate 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 |
| 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, Chemical Weapon 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 (Appendix 16-A as reproduced in the Handbook of Procedures, 2002-2007 ) 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 license and in that case also exporters shall submit to DGFT a copy of bill of entry into destination country within 30 days of exports. (This corresponds to Schedule 3 to the Chemical Weapons Convention) (1) Phosgene: carbonyl dichloride (2) Cyanogen chloride (3) Hydrogen cyanide (4) Chloropicrin: Trichloronitromethane (5) Phosphorus oxychloride (6) Phosphorus trichloride (7) Phosphorus pentachloride (8) Trimethyl phosphite (9) Triethyl phosphite (10) Dimethyl phosphite (11) Diethyl phosphite (12) Sulfur monochloride (13) Sulfur dichloride (14) Thionyl chloride (15) Ethyldiethanolamine (16) Methyldiethanolamine (17) Triethanolamine |
| Category 2: | Micro-organisms, toxins |
| 2A | Bacteria, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following: |
| 2A001 | Bacillus anthracis |
| 2A002 | Bordetella bronchoseptica |
| 2A003 | Brucella abortus, |
| 2A004 | Brucella melitensis |
| 2A005 | Brucella suis |
| 2A006 | Chlamydia psittaci |
| 2A007 | Clostridium botulinum |
| 2A008 | Clostridium perfringes |
| 2A009 | Corynebacterium diphtheriae |
| 2A010 | Francisella tularensis |
| 2A011 | Klebsiella pneumoniae |
| 2A012 | Legionlla pneumophila |
| 2A013 | Leptospira interrogans - all serotypes reported in India |
| 2A014 | Mycobacterium bovis |
| 2A015 | Mycobacterium tuberculosis |
| 2A016 | Mycoplasma mycoides - var mycoides |
| 2A017 | Mycoplasma mycoides - var Capri |
| 2A018 | Neisseria meningitidis |
| 2A019 | Paseturella multicoda type B |
| 2A020 | Pseudomonas mallei |
| 2A021 | Pseudomonas pseudomallei |
| 2A022 | Salmonella paratyphi |
| 2A023 | Shigella dysenteriae |
| 2A024 | Staphylococcus aureus |
| 2A025 | Streptococcus pneumoniae |
| 2A026 | Vibrio cholerae elter |
| 2A027 | Vibrio Cholerae 0139 |
| 2A028 | Yersinia pestis |
| 2B | Fungi, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following: |
| 2B001 | Blastomyces dermatitidis |
| 2B002 | Coccidiodes immitis |
| 2B003 | Histoplasma capulatum |
| 2B004 | Nocardia asteroides |
| 2B005 | Paracoccidioides braziliensis |
| 2C | Parasites, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following: |
| 2C001 | Entamoeba histolytica |
| 2C002 | Babesia microti |
| 2C003 | Babesia divergens |
| 2C004 | Blostidium coli |
| 2C005 | Cryptosporidium spp. |
| 2C006 | Leishmania species |
| 2C007 | Naegleria australiensis |
| 2C008 | Naegleria fowleri |
| 2C009 | Plasmodium falciparum |
| 2C010 | Pneumocystis carinii |
| 2C011 | Schistosoma mansoni |
| 2C012 | Schistosoma japonicum |
| 2C013 | Schistosoma hemotobium |
| 2C014 | Toxoplasma gondii |
| 2C015 | Trichinella spiralis |
| 2C016 | Trypanosoma bruiei |
| 2D | Viruses, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following: |
| 2D001 | African Horse Sickness virus |
| 2D002 | African Swine Fever virus |
| 2D003 | Avian influenza virus |
| 2D004 | Blue tongue virus |
| 2D005 | Camel pox virus |
| 2D006 | Chikungunya virus |
| 2D007 | Crimean-Congo hemorrhagic fever virus |
| 2D008 | Dengue virus |
| 2D009 | Eastern equine encephalitis virus |
| 2D010 | Ebola fever virus |
| 2D011 | Encephalomyocarditis virus (EMC) |
| 2D012 | Foot and Mouth Disease virus (all serotypes and subtypes) |
| 2D013 | Guanirito virus |
| 2D014 | Goatpox virus |
| 2D015 | Hantaan virus |
| 2D016 | Herpes virus simiae (monkey B virus) |
| 2D017 | Herpes ateles, Herpes saimiri |
| 2D018 | HIV- 1 & HIV-2 and other strains of SIV |
| 2D019 | Hog cholera virus |
| 2D020 | Human T-cell Leukemia virus |
| 2D021 | Junin virus |
| 2D022 | Japanese encephalitis virus |
| 2D023 | Kyasanur Forest Disease virus and Central European encephalitis viruses. |
| 2D024 | Korean hemorrhagic fever virus |
| 2D025 | Lymphocytic choriomeningitis virus (LCM) |
| 2D026 | Lassa virus |
| 2D027 | Marburg virus |
| 2D028 | Murrey valley encephalitis virus |
| 2D029 | Marchupo virus |
| 2D030 | Mason-pfizer monkey virus |
| 2D031 | Monkey pox virus |
| 2D032 | Newcastle disease virus |
| 2D033 | Omsk hemorrhagic fever virus |
| 2D034 | Peste des petits ruminant virus |
| 2D035 | Porcine enterovirus type I |
| 2D036 | Powassan virus |
| 2D037 | Rabies virus -all strains |
| 2D038 | Respiratory syncitial virus |
| 2D039 | Rift Valley Fever virus |
| 2D040 | Rinderpest virus |
| 2D041 | Sabia virus |
| 2D042 | Sheep pox (field strain) |
| 2D043 | Sin Nombre virus |
| 2D044 | Smallpox virus |
| 2D045 | St.Louis encephalitis virus |
| 2D046 | Swine Fever virus |
| 2D047 | Tick-borne encephalitis virus (Russian Spring Summer Encephalitis virus) |
| 2D048 | Teschen disease virus (Porcine entero virus type 1) |
| 2D049 | Variola virus |
| 2D050 | Venezuelan encephalitis virus |
| 2D051 | Vesicular stomatitis virus |
| 2D052 | Western encephalitis virus |
| 2D053 | Yellow fever virus, 17 D vaccine strain |
| 2E | Rickettsials, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures for the following: |
| 2E001 | Coxiella burnetti |
| 2E002 | Rickettsiae rickettsii |
| 2E003 | Rickettsia quintana |
| 2E004 | Rickettsia prowazebi |
| 2F | Toxins |
| 2F001 | Abrins |
| 2F002 | Aflatoxins |
| 2F003 | Anatoxins |
| 2F004 | Botulinum toxin (s) (clostradium botulinum) |
| 2F005 | Bungarotoxins |
| 2F006 | Clostridium perfringens toxins |
| 2F007 | Corynebacterium diphtheriae toxins |
| 2F008 | Cyanginosins (Microcystins) (Microcystic aeuginosa) |
| 2F009 | Enterotoxin (Staphylococcus aureus) |
| 2F010 | Neurotoxin (Shigella dysenteriae) |
| 2F011 | Ricins |
| 2F012 | Shigatoxins |
| 2F013 | Saxitoxins |
| 2F014 | Trichothecene mycotoxins |
| 2F015 | Tetanus toxin (clostridium tetani) |
| 2F016 | Tetrodotoxin (Spheroides rufripes) |
| 2F017 | Verrucologen (M. verrucadia) |
| 2G | Plant pathogens |
| 2G001 | Bemisia tabaci |
| 2G002 | Colletotrichum coffeanum var. virulans |
| 2G003 | Clavicep purpurea |
| 2G004 | Dothistroma pini (Scirrhia pini) |
| 2G005 | Erwinia amylovora |
| 2G006 | Frankliniella occidentalis |
| 2G007 | Microcyclus ulei |
| 2G008 | Peronospora hyoscyami de Bary f.sp. tabacina (Adam) skalicky |
| 2G009 | Phytophthora infestans |
| 2G010 | Puccinia graminis |
| 2G011 | Puccinia erianthi |
| 2G012 | Puccinia striiformiis (Puccinia glumarum) |
| 2G013 | Pyricularia oryzae |
| 2G014 | Pseudomonas solanacearum |
| 2G015 | Peronospora hyscyami de Bary |
| 2G016 | Ralstonia solanacearum |
| 2G017 | Sugar cane Fiji disease virus |
| 2G018 | Sclerotinia sclerotiorum |
| 2G019 | Tilletia indica |
| 2G020 | Thrips palmi |
| 2G021 | Ustilago Maydis |
| 2G022 | Xanthomonas albilineans |
| 2G023 | Xanthomonas campestris pv citri |
| 2G024 | Xanthomonas campestris pv oryzae |
| 2H | Genetically Modified Organisms |
| 2H001 | Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity and are derived from organisms specified above in 2A, 2B, 2C, 2D, 2E and 2H. |
| 2H002 | Genetically-modified micro-organisms or genetic elements that contain nucleic acid sequences coding for any of the toxins specified above in 2F. |
| Category 3: | Special Materials, Materials Processing Equipment, and related technologies |
| 3A | Special Materials |
| 3A001 | Magnesium of purity greater than 99.9% |
| 3A002 | Maraging steel except forms in which no linear dimension exceeds 75 mm. |
| 3A003 | Tungsten, molybdenum, and alloys of those metals in the form of uniform spherical or atomized particles of 500 micrometer diameter or less with a purity of 97% or higher. |
| 3A004 | Germanium |
| 3A005 | Gallium |
| 3A006 | Hafnium |
| 3A007 | Indium |
| 3A008 | Niobium |
| 3A009 | Titanium-Uranium alloys. |
| 3A010 | Articles made of materials (including waste & scrap) appearing at items 3A005 to 3A009 above and items at 3A011 |
| 3A011 |
Aluminium alloys in any form ‘capable of acquiring’ an ultimate tensile strength of 460 Mega Pascals or more at 293 K (20 degree C) Note: The phrase ‘ capable of acquiring’ encompasses alloys before or after heat treatment. |
| 3B | Materials processing equipment and related technologies: |
| 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. |
Equipment, technical data and procedures for the production of structural composites for rocket systems including:- (a) Carbon - carbon composites; (b) Filament winding machines of which the Motion for positioning wrapping and winding fibres are coordinated and programmed in three or more axes; and coordinating and programming controls (c) Tape-laying machines of which the motions for positioning and laying tape and sheets are coordinated and programmed in two or more axes; (d) 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 the above end; (e) Equipment designed or modified for production of fibrous or filamentary materials as follows: converting polymeric substances; vapor deposition on heated filament substrates; wet spinning of refractory ceramics. (f) Technical data (including processing conditions) and procedures for the regulation of temperature, pressure or atmosphere in autoclaves when used for the production of composites or partially processed composites. |
| 3B003 |
Pyrolytic deposition and densification equipment: (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 therefor, specially designed for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips. |
| 3B004 | Production technology or production equipment 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. |
| 3B005 | Sputter ion pumps |
| 3B006 | Refrigeration units and equipment capable of cooling hydrogen or helium to -250 degrees Celcius (23K) or lower. |
| 3B007 | Continuous nitrators; |
| 3B008 | Dehydration presses; |
| 3B009 | Screw extruders specially designed or modified for military explosive extrusion; |
| 3B010 | Cutting machines for the sizing of extruded propellant; |
| 3B011 | Sweetie barrels (tumblers) 1.85 m or more in diameter and having over 227 kg product capacity; |
| 3B012 | Continuous mixers for solid propellants; |
| 3B013 | Fluid energy mills for grinding or milling the ingredients military explosive; |
| 3B014 | Equipment to achieve both sphericity and uniform particle size in metal powders. |
| 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: (i) Nickel , or alloys with more than 40% nickel by weight (ii) Alloys with more than 25% nickel and 20% chromium by weight (e.gs; ‘Hastelloy’ , ‘Illium’, ‘Inconel’, Incoloy’) (iii) Fluoropolymers (iv) Glass or glass lined (including vitrified or enameled coating) (v) Graphite (vi) Tantalum or tantalum alloys (vii) Titanium or titanium alloys (viii) Zirconium or zirconium alloys (ix) Ceramics (x) Ferrosilicon Note 3D001 does not control the following items: (i) 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.) (ii) Ceramic or 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, crucibles, 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 (1,000 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: (i) Alloys with more than 25% nickel and 20% chromium by weight; (e.gs; ‘Hastelloy’ , ‘Illium’, ‘Inconel’, ‘Incoloy’) (ii) Nickel, or alloys with more than 40% nickel by weight; or (iii) Titanium; (iv) Ceramics; |
| 3D004: | Equipment related to P3, P4 facilities such as protective suits and class III safety cabinets. |
| 3D005: | Complete containment facilities at P3, P4, containment level as specified in the WHO biosafety manual. |
| (Entry 3D004 & 3D005 has been added vide NTF. NO. 11/2004, DT. 16/12/2004) | |
| Category 4 |
Avionics and Navigation (i) Guidance systems and their components such as gyros and inertial reference units (ii) Compasses, gyroscopes, accelerometers and inertial equipment and specially designed software therefor and specially designed components therefor for use in rocket systems; (a) Integrated flight instrument systems; (b) Gyro-astro compasses; (c) Accelerometers; (d) Gyroscopes; (e) Inertial or other equipment using accelerometers or systems incorporating such equipment, and specially designed integration software therefor; (iii) Encrypted telemetry systems, equipment and software therefor. (iv) Flight control system for use in rocket systems as follows as well as the specially designed test, calibration, and alignment therefor. (a) Hydraulic, mechanical, electro-optical or electro-mechanical flight control systems (including fly-by-wire systems) specially designed or modified for rocket systems; (b) Attitude control equipment specially designed or modified for rocket system; (c) Design technology for integration of flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory. (vi) Integrated flight instrument systems; (vii) Avionics equipment specially designed or suitable for use in rocket systems and specially designed software and components therefor for use in rocket systems, including but not limited to. (a) Radar and laser radar system; (b) Electronic assemblies and components for rocket system; (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, electromagnetic sources or terrain characteristics (e) Global Positioning System (GPS) capable of operating at speeds greater than 500 m/s and at altitudes greater than 18 kms. (viii) On-board electronic equipment, devices and their design and manufacturing know-how (except warhead fuses, timers and sequencers), and embedded or specially designed software therefor, for rocket systems. (ix) Telemetering and telecontrol equipment suitable for use with rocket systems; (x) Precision tracking systems and related software. |
| Category 5: | Aerospace materials, equipment, systems and related technologies |
| 5A | Materials |
| 5A001 |
Structural materials such as: (a) Composite Structures, laminates, and manufacturers thereof, including resin impregnated fibre prepregs and metal coated fibre preforms therefor, specially designed for use in rocket systems and subsystems made either with an organic matrix or metal matrix utilizing fibrous or filamentary reinforcements; (b) Resaturated pyrolized (i.e. Carbon-Carbon) materials specially designed for rocket systems; (c) Fine grain artificial graphites and pyrolytic or fibrous reinforced graphites for rocket nozzles and reentry vehicles nosetips; (d) Ceramic composite materials for use in missile radomes and nose tips; (e) Structured materials and coatings for reduced radar reflectivity |
| 5A002 |
Rocket propellants and constituent chemicals for propellants as follows:- (a) Propulsive substances-Hydrazine, Monomethylhydrazine (MMH), Unsymmetrical di-methyl hydrazine (UDMH), ammonium perchlorate, spherical aluminium powder, Nitroamines (Cyclotetetramethylene-tetranitramine (HMX), cyclotetramethylenetrinitramine (RDX), (b) Metal Fuels consisting of any of the following: Zirconium, titanium, uranium, tungsten, boron, zinc, and alloys of these magnesium, Misch metal, when specially formulated as propulsive substances; (c) Polymeric substances: Carboxyl-terminated polybutadiene (CIPB), Hydroxy-Terminated Polybutadiene (HTPB); Glycidyl azide polymer (GAP), Polybutadiene acrylic acid (PBAA), Polybutadiene acrylic acid acrylonitrile (PBAN); (d) Composite propellants and composite modified double base propellants; (e) High energy density fuels such as boron slurry; (f) Oxidizers/fuels - Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components; Dinitrogen trioxide, Nitrogen dioxide / Dinitrogen tetroxide, Dinitrogen pentoxide, Inhibited red fuming nitric acid (IRFNA), Ammonium perchlorate, Ammonium Dinitramide (ADM); (g) Bonding agents - Tris (1-2 (2-methyl)) aziridinyl phosphine oxide (MAPO), Trimesoyl-1-(2-ethyl) aziridene (HX-868, BITA), Tepanol (HX-878), Tepan (HX-879), HX-752, HX-874, HX-877; (h) Curing agents and catalysts - Triphyenyl bismuth (TPB); (i) Burning rate modifyers - Catocene, N-butyl ferrocene, Butacene, Ferrocene derivatives, Carboranes, Decarboranes, Pentaboranes; (j) Esters and plasticizers - Triethylene glycol dinitrate (TEGDN), Trimethloethane trinitrate (TMETN), 1,2,4-Butanetriol trinitrate (BTTN), Diethylene glycol dinitrate (DEGDN) (k) Stabilisers - 2-Nitrodiphenylamine, N-methyl-p-nitroaniline |
| 5A003 |
High explosives, propellants or substances or mixtures containing more than 2% of any of the following; (a) Cycloteramethylenetetranitramine (HMX); (b) Cyclotrimethylenetrinitramine (RDX); (c) Triaminotrinitrobenzene (TATE); (d) Hexanitrostilbene (HNS). |
| 5B | Equipment and systems |
| 5B001 | Pulsed electron accelerators |
| 5B002 |
Hardware, technology, production facilities and components for missiles and rockets (other than JATO units, unguided rocket-propelled munitions, and propulsion units for flares ejection seats and like emergency escape equipment), including: (a) complete rocket systems, individual rocket stages with or without engines such as: (b) solid or liquid fuel rocket engines and their control systems, except for satellite control; (c) Heat shields fabricated of ceramic or ablative materials; (d) Electronic equipment specially designed or modifiable for use in rockets. |
| 5B003 |
Sub-systems, design, technology, know-how components and manufacturing equipment for 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 control systems, and components thereof, specially designed or modified for resistance to vibration. (d) Re-entry systems, heat-shields; (e) Solid or liquid propellant rocket engines; (f) Guidance systems and their components such as gyros and inertial reference units; (g) Thrust-vector control; (h) Hybrid rocket motors and components therefor |
| 5B005 |
Launch and ground support equipment and facilities usable for rocket system as follows:- (a) Apparatus and devices specially designed or modified for launching of the system. |
| 5C | Test Equipment |
| 5C001 | Supersonic, hypersonic and hypervelocity wind tunnels; gun tunnels; aeroballistic ranges. |
| 5C002 | Test facilities designed to handle solid or liquid fuel rockets except for satellite control. |
| 5C003 | Vibration test equipment and components using digital control techniques and feedback or closed loop test equipment and software therefor |
| 5C004 | Environmental chambers simulating altitudes above 15 km, temperature ranging between minus 50 and plus 125 degrees centigrade. |
| 5C005 | Acoustic test facility with sound pressure level greater than 140 dB or rated power output greater than 4KW. |
| 5D |
Manned-aircraft, aero-engines, related equipment and components: Note This category does not control an Indian military aircraft carrying a military registration number. a. Combat "aircraft" and specially designed components therefor; b. 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 therefor; c. Aero-engines specially designed or modified for military use, and specially designed components therefor; d. Airborne equipment, including airborne refuelling equipment, specially designed for use with the aircraft controlled by 5Da or 5Db or the aero-engines controlled by 5Dc, and specially designed components therefor; e. Pressure refuellers, pressure refuelling equipment, equipment specially designed to facilitate operations in confined areas and ground equipment, developed specially for "aircraft" controlled by 5Da or 5Db or for aero-engines controlled by 5Dc.; f. 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"; g. 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; h. 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 5Db does not control "aircraft" or variants of those "aircraft" specially designed for military use which: (i). Have been certified for civil use by the civil aviation authority of India, and (ii). 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 5Db and 5Dc 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 |
Unmanned airborne vehicles and related equipment, specially designed or modified for military use as follows, and specially designed components therefor; (a). Unmanned airborne 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. Note This category does not control unpowered airborne vehicles such as gliders, hot air balloons etc. |
| 5F |
Micro-light Aircraft and powered hang-gliders and their parts. [OLD-Microlight aircraft and powered ‘hang-gliders’ ] (Entry 5F has been amended vide NTF. NO. 11/2004, DT. 16/12/2004) |
| Category 6 | [RESERVED] |
| Category 7: | Electronics, computers, and information technology including information security |
| 7A | Electronics |
| 7A001 | High-power microwave tubes, travelling wave tubes and microwave phase shifters. |
| 7B | [Reserved] |
| 7C | Computers |
| 7C001 |
Digital computers and software as follows: (i) "Digital computers having a composite theoretical performance (CTP) exceeding 28000 (Twenty eight thousand) million theoretical operations per second (Mtops) (ii) Software, and/or computer inter-connection schemes, whether or not co-supplied with (i) designed to "parallelise" digital computers (individually of any CTP rating) enabling a CTP of more than 28000 (Twenty eight thousand) million theoretical operations per second (Mtops) to be achieved by the "parallelised" configuration" Explanatory notes (a)The Composite Theoretical Performance (CTP) rating is to be calculated in accordance with the calculation scheme separately notified in this regard. (b)Individual digital computers each with a CTP rating of 28000 (Twenty eight thousand) million theoretical operations per second (Mtops) or less do not require an export license to any destination or end-user, unless supplied with (ii) (c) "Digital Computers" includes (1) hybrid computers incorporating "digital computers" or specified in (i) above, systolic array computers, neural computers, optical computers, biological 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 | Specially designed software, and/or related specially designed analogue or hybrid computers, for modelling, simulation, or design integration of rocket systems. |
| 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] -] |
(The applicant exporters are required to submit declarations as given in Annexure-A to TRADE NOTICE. No. 01/2006, DT. 07/06/2005 in all applications for issuance of Advance Licences/Annual Advance licences/DEPB/DFRC) ]