RM-1-2 (original) (raw)

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RM-1-2

Part of RM-1-1

RM-1-2
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Satellite Reaction Control. Pressure-fed.

Date: 1967. Thrust: 4.41 N (0.99 lbf). Specific impulse: 238 s.

Family: Storable liquid. Country: USA. Propellants: N2O4/MMH. Agency: Rocketdyne.

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