The following motor has been certified by NAR Standards & Testing for
general use as a High Power Rocket Motor effective May 30, 2008
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Aerotech/RCS(AT):
G142-6, 10, 14
29 x 113 mm
Single Use Motor
84.3 Newton-seconds total impulse
173.9 Newtons Peak Thrust
135.9 Newtons Average Thrust
Propellant mass: 38.6 gm.

8222ALF Propellant
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NAR Standards & Testing
s-and-t@nar.org

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