line item No.

Name <*>

Code of the CN FEA EEU <*>

Category I

Section 1. The finished delivery systems

1.1.

Equipment, assembly units and component parts

1.1.1.

Rockets (including ballistic missiles, carrier rockets and research rockets), capable to deliver payload at least 500 kg to range at least 300 km

8802 60;

9306 90

1.1.2.

Atmospheric unmanned aerial vehicles (including cruise missiles, radio-controlled airplanes targets and radio-controlled reconnaissance aircrafts), capable to deliver payload at least 500 kg to range at least 300 km

8806 29 002 1;

8806 29 002 2;

8806 29 002 3;

8806 29 002 5;

8806 29 002 9;

8806 99 002 1;

8806 99 002 2;

8806 99 002 3;

8806 99 002 5;

8806 99 002 9;

9306 90

1.2.

Test and production equipment

1.2.1.

The production capacities which are specially developed for the delivery systems specified in line item 1.1

1.3.

Materials - are not present

1.4.

Software

1.4.1.

The software, specially developed or modified for use of the production capacities specified in line item 1.2

1.4.2.

The software for functioning coordination more than one system, specially developed or modified for the delivery systems specified in line item 1.1

Note.

For the unmanned aerial vehicles specified in line item 1.1.2, of the piloted airplanes re-equiped from, the line item 1.4.2 includes also following software:

1. Specially developed or modified for integration of the equipment transforming the piloted airplane to the unmanned aerial vehicle with functional systems of the airplane.

2. Specially developed or modified for operation of the piloted airplane as the unmanned aerial vehicle.

1.5.

Technology

1.5.1.

Technology according to the general note for technology for development, production or use of the equipment or the software specified in line items 1.1, 1.2 or 1.4

Section 2. The finished systems used for the finished delivery systems

2.1.

Equipment, assembly units and component parts

2.1.1.

The finished systems used in the delivery systems specified in line item 1.1:

2.1.1.1.

The separate steps of rockets used in the delivery systems specified in line item 1.1

8807 90 000 3;

9306 90

2.1.1.2.

The returned devices and the equipment which is stated below developed or modified for them used in the delivery systems specified in line item 1.1, excepting the equipment of the returned devices intended for not military useful loads:

8807 90 000 9;

9306 90

2.1.1.2.1.

The heat-shielding and its elements made of ceramic or ablative materials;

8807 90 000 3;

8807 90 000 9;

9306 90

2.1.1.2.2.

The heat insulation and its elements made of the lungs having the high specific heat of materials;

8807 90 000 3;

8807 90 000 9;

9306 90

2.1.1.2.3.

The electronic equipment which is specially developed for the returned devices

8541 51 000 0;

8541 59 000 0;

9014 20;

9306 90 100 1;

9306 90 100 9;

9306 90 900 0

2.1.1.3.

The liquid, solid-fuel, hybrid rocket engines and rocket engines on gel fuel providing as a part of propulsion systems of the delivery systems specified in line item 1.1, composite pulse of draft equal or more 1, to 1 x 106 N · with

8412 10 000 9

Note.

The liquid apogean engines and engines of orientation specified in line item 2.1.1.3, developed or modified for application in the artificial Earth satellites (AES), can be considered as belonging to the category II if they have draft in vacuum no more than 1 kN and their export in the declared quantity are performed in the presence of obligations about end use in the artificial satellite

2.1.1.4.

The systems of targeting used in the delivery systems specified in line item 1.1, deliveries of useful load of no more 3,33 of percent providing accuracy from range (for example, the circular probable variation (CPV) constitutes 10 km or less in case of range of 300 km), except for the systems developed for rockets with range less than 300 km or the piloted aircraft

8541 51 000 0;

8541 59 000 0;

9014 20;

9306 90 100 1;

9306 90 100 9;

9306 90 900 0

Technical notes:

1. The equipment of system of targeting combines process of measurement and calculation of provision and speed of flight of the aircraft (navigation parameters) with process of calculation and submission of commands in management system its flight for adjustment of trajectory.

2. QUO is criterion of accuracy of hit. Its value is in number equal to circle radius with the center in the middle of the purpose if in it there are 50 percent of points of fall of useful loads (head parts)

2.1.1.5.

The subsystems of management of draft vector used in the delivery systems specified in line item 1.1, excepting those subsystems which are developed for rockets which range and useful load do not exceed the parameters specified in line item 1.1

8412 90 200 9

Technical note.

The line item 2.1.1.5 includes the following methods of management of draft vector:

a) use of nozzle of changeable geometry;

b) or having blown injection of liquid secondary gas (into nozzle);

c) use of the rotary engine or nozzle;

d) use of gas wheels or nozzles for variation of stream of exhaust gases;

e) use of traction trimmers

2.1.1.6.

The mechanisms of safety, raising and blasting detonator of warhead or warhead used in the delivery systems specified in line item 1.1, except for of mechanisms, intended for other delivery systems which are not specified in line item 1.1

8541 51 000 0;

8541 59 000 0;

8807 90 000 9;

9306 90 100 1;

9306 90 100 9;

9306 90 900 0

Note.

The equipment provided in exceptions on line items 2.1.1.2, 2.1.1.4 - 2.1.1.6, can be considered as belonging to the category II if it is exported taking into account guarantees about end use in stated purposes, and the exported quantity does not allow to use it for the purpose of, the specified line items given in

2.2.

Test and production equipment

2.2.1.

The production capacities which are specially developed for the systems specified in line item 2.1

2.2.2.

The production equipment which is specially developed for the systems specified in line item 2.1

2.3.

Materials - are not present

2.4.

Software

2.4.1.

The software, specially developed or modified for use of the production capacities specified in line item 2.2.1

2.4.2.

The software, specially developed or modified for use of the rocket engines specified in line item 2.1.1.3 and in the note to it

2.4.3.

The software, specially developed or modified for use of the systems of targeting specified in line item 2.1.1.4

Note.

The line item 2.4.3 includes the software, specially developed or modified for the purpose of improvement of characteristics of the systems of targeting specified in line item 2.1.1.4, for achievement or exceeding of value of accuracy of delivery of useful load

2.4.4.

The software, specially developed or modified for use of the electronic equipment specified in line item 2.1.1.2.3

2.4.5.

The software, specially developed or modified for use of the subsystems specified in line item 2.1.1.5

2.4.6.

The software, specially developed or modified for use of the mechanisms specified in line item 2.1.1.6

Note.

The software controlled by line items 2.4.2 - 2.4.6, can be considered as belonging to the category II if it is exported taking into account guarantees about end use in the stated purposes other than the purposes specified in these line items and answers the following conditions:

1) the software on line item 2.4.2 - if it is specially developed or modified for the liquid apogean engines or engines of the navigation system developed or modified for application in the artificial satellite as it is specified in the note to line item 2.1.1.3;

2) the software on line item 2.4.3 - if it is developed for rockets with range less than 300 km or the piloted aircraft;

3) the software on line item 2.4.4 - if it is specially developed or modified for the returned devices intended for not military useful loads;

4) the software on line item 2.4.5 - if it is developed for rockets which range and useful load do not exceed the parameters specified in line item 1.1;

5) the software on line item 2.4.6 - if it is developed for other delivery systems, than are specified in line item 1.1

2.5.

Technology

2.5.1.

Technology according to the general note for technology for development, production or use of the equipment or the software specified in line item 2.1, 2.2 or 2.4

Category II

Section 3. Elements of propulsion systems and equipment

3.1.

Equipment, assembly units and component parts

3.1.1.

Turbojet and turbofan engines:

3.1.1.1.

The engines having everything the following characteristics:

a) the maximum value of draft (reached on bench testing) more than 400 N, excepting the engines certified for civil application with the maximum value of draft over 8890 N;

b) the specific fuel consumption is not higher than kg/N 0,15 · h, measured in case of the maximum long capacity at sea level in static conditions of use in case of the standard atmosphere accepted by International Civil Aviation Organization

8411 11 000