Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p261
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 745427–749398

Manned, untethered submersible vehicles…

8A001.c.    Unmanned submersible vehicles...

8A001.d.    Not used since 2018

8A002.b.    Systems specially designed or modified for the automated control of the motion of submersible vehicles specified by 8A001 of this List using navigation data having closed loop servo‑controls and having any of the following:
            1. Enabling…
            2. Maintaining…
            3. Maintaining…

8A002.h.    "Robots" specially designed for underwater use...

8A002.j.    Air independent power systems...

8A002.o.3.  Noise reduction systems for use on vessels...

8A002.p.    Pumpjet propulsion systems...

8D001       "Software" specially designed for the "development" or "production" of equipment in 8A of this List.

8D002       Specific "software"…

8E001       "Technology" according to the General Technology Note for the "development" or "production" of equipment specified by 8A of this List.

8E002.a.    Other "technology"...

Category 9                        SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES

9A011                             Ramjet, scramjet or combined cycle engines...

9A104                             Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.
                                  N.B.: See also 9A004.

9A105.a.                          Liquid propellant rocket engines integrated, or designed or modified to be integrated, into a liquid propellant propulsion system, as follows:
                                  N.B.: See also 9A119.
                                  a. Liquid propellant rocket engines usable in "missiles", other than those specified by 9A005, having a total impulse capacity equal to or greater than 1.1 MNs; except liquid propellant apogee engines integrated, or designed or modified to be integrated, into a liquid propellant propulsion system, designed or modified for satellite applications and having all of the following:
                                  1. Nozzle throat diameter of 20 mm or less; and
                                  2. Combustion chamber pressure of 15 bar or less.

9A106                             Systems or components, other than those specified by 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems:
                                  c. Thrust vector control sub‑systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.
                                     Technical Note:
                                     Examples of methods of achieving thrust vector control specified by 9A106.c. are:
                                        1. Flexible nozzle;
                                        2. Fluid or secondary gas injection;
                                        3. Movable engine or nozzle;
                                        4. Deflection of exhaust gas stream (jet vanes or probes); or
                                        5. Thrust tabs.

9A108.c.                          Components, other than those specified by 9A008, usable in "missiles" as follows, specially designed for solid rocket propulsion systems:
                                  c. Thrust vector control sub‑systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.

                                  Technical Note:
                                  Examples of methods of achieving thrust vector control specified by 9A108.c. are:
                                     1. Flexible nozzle;
                                     2. Fluid or secondary gas injection;
                                     3. Movable engine or nozzle;
                                     4. Deflection of exhaust gas stream (jet vanes or probes); or
                                     5. Thrust tabs.