LR101-NA-7

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LR101-NA-7

Part of LR101

RS-32
Credit: Boeing / Rocketdyne

Rocketdyne N2O4/MMH rocket engine. Upper Stage Target Engine Systems. Pressure-fed. Derived from Atlas vernier.

AKA: RS-32. Date: 1976. Thrust: 5.15 kN (1,157 lbf). Specific impulse: 251 s.

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

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