Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p236
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 673503–676727

Specified by 9A001; or
b. Whose design or production origins are either not from a Wassenaar Arrangement Participating State or unknown to the manufacturer.
9. A. 004. Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft payloads", "spacecraft" on-board systems or equipment, terrestrial equipment, air-launch platforms and "sub-orbital craft", as follows:
N.B.: SEE ALSO 9A104.
a. Space launch vehicles;
b. "Spacecraft";
c. "Spacecraft buses";
d. "Spacecraft payloads" incorporating items specified by 3A001.b.1.a.4., 3A002.g., 5A001.a.1., 5A001.b.3., 5A002.c., 5A002.e., 6A002.a.1., 6A002.a.2., 6A002.b., 6A002.d., 6A003.b., 6A004.c., 6A004.e., 6A008.d., 6A008.e., 6A008.k., 6A008.l. or 9A010.c.;
9. A. 004. e. On‑board systems or equipment, specially designed for "spacecraft" and having any of the following functions:
1. 'Command and telemetry data handling';
Note: For the purpose of 9A004.e.1., 'command and telemetry data handling' includes bus data management, storage, and processing.
2. 'Payload data handling'; or
Note: For the purpose of 9A004.e.2., 'payload data handling' includes payload data management, storage, and processing.
3. 'Attitude and orbit control';
Note: For the purpose of 9A004.e.3., 'attitude and orbit control' includes sensing and actuation to determine and control the position and orientation of a "spacecraft".
           N.B.: For equipment specially designed for military use, see ML 11.c.
9. A. 004. f. Terrestrial equipment specially designed for "spacecraft", as follows:
1. Telemetry and telecommand equipment specially designed for any of the following data processing functions:
a.  Telemetry data processing of frame synchronisation and error corrections, for monitoring of operational status (also known as health and safe status) of the "spacecraft bus"; or
b.  Command data processing for formatting command data being sent to the "spacecraft" to control the "spacecraft bus";
9. A. 004. f. 2. Simulators specially designed for 'verification of operational procedures' of "spacecraft";
Technical Note:
For the purposes of 9A004.f.2., 'verification of operational procedures' is any of the following:
1. Command sequence confirmation;
2. Operational training;
3. Operational rehearsals; or
4. Operational analysis.
9. A. 004. g. "Aircraft" specially designed or modified to be air‑launch platforms for space launch vehicles;
9. A. 004. h. "Sub‑orbital craft".
Note: Certain items specified in 9A004. may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. A. 005. Liquid rocket propulsion systems containing any of the systems or components, specified by 9A006.
N.B.: SEE ALSO 9A105 AND 9A119.
Note: Certain items specified in 9A005 may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. A. 006. Systems and components, specially designed for liquid rocket propulsion systems, as follows:
N.B.: SEE ALSO 9A106, 9A108 AND 9A120.
a. Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30% per year;
b. Cryogenic containers or closed‑cycle refrigeration systems,