Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006. N.B.: SEE ALSO 9A105 AND 9A119.

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• Rocket propulsion subsystems, usable in the systems specified in 1.A., as follows;1. Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 1,1 × 106Ns;2. Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 × 106Ns;Note:Liquid propellant apogee engines or station-keeping engines specified in 2.A.1.c.2., designed or modified for use on satellites, may be treated as Category II, if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN.
• Individual rocket stages usable in the systems specified in 1.A.;
• Complete subsystems as follows:a. Individual rocket stages, not specified in 2.A.1., usable in systems specified in 19.A.;b. Rocket propulsion subsystems, not specified in 2.A.1., usable in the systems specified in 19.A.1., as follows:1. Solid propellant rocket motors or hybrid rocket motors having a total impulse capacity equal to or greater than 8,41 × 105Ns, but less than 1,1 × 106Ns;2. Liquid propellant rocket engines or gel propellant rocket motors integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 8,41 × 105Ns, but less than 1,1 × 106Ns;