R129 |
NAR S&T NEW MOTOR CERTIFICATION |
May 29, 2009 |
The following motor has been certified by NAR Standards & Testing for
general use as a High Power Rocket Motor effective May 29, 2009.
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Alpha:
I250
54mm x 711mm
540 Newton-seconds total impulse
375 Newtons Peak Thrust
231 Newtons Average Thrust
Propellant mass: 353.8 grams (includes fuel grain and nitrous oxide)
Candlepower/nitrous oxide propellant
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NAR Standards & Testing
s-and-t@nar.org
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