X-1

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X-1

Part of LR79

X-1
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Booster applications. Gas generator, pump-fed. Thrust from 165,000 to 198,000 lbs.

Date: 1957. Thrust: 880.44 kN (197,931 lbf).

Propellant Formulation: Lox/RP-1.

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

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