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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