RM-25 (original) (raw)

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RM-25

RM-25-1
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

Date: 1967. Thrust: 107 N (24 lbf). Specific impulse: 286 s.

Subtopics

	RM-25-1 Rocketdyne N2O4/MMH rocket engine. Spacecraft. Pressure-fed.

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

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