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RM-01
RM-01
RM-01
Credit: Boeing / Rocketdyne
Date: 1969. Thrust: 0.0441 N (0.0099 lbf). Specific impulse: 91 s.

Propellant Formulation: Tridyne.



Family: Monopropellant. Country: USA. Agency: Rocketdyne.

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