X-8 (original) (raw)

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X-8

X-8
Credit: Boeing / Rocketdyne

Rocketdyne LOx/LH2 rocket engine. Booster applications. Gas generator, pump-fed. Thrust and specific impulse values are at sea level.

Date: 1961. Thrust: 400.10 kN (89,946 lbf). Specific impulse: 408 s. Specific impulse sea level: 408 s.

Thrust (sl): 400.100 kN (89,946 lbf). Thrust (sl): 40,800 kgf.

Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne.

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