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E-1
E-1
E-1
Credit: Boeing / Rocketdyne
Rocketdyne LOx/Kerosene rocket engine. Study 1957. Developed by USAF in late 1950's. Cancelled and decision to go direct to 1,500,000 lbf F-1 as next step. Booster applications. Gas generator, pump-fed.

Status: Study 1957. Date: 1957. Thrust: 1,884.59 kN (423,673 lbf). Specific impulse: 290 s. Specific impulse sea level: 260 s.

Thrust (sl): 1,689.600 kN (379,837 lbf). Thrust (sl): 172,300 kgf. Propellant Formulation: Lox/RP-1.



Country: USA. Launch Vehicles: Super-Jupiter. Propellants: Lox/Kerosene. Stages: Super-Jupiter-2, Super-Jupiter stage. Agency: Rocketdyne.
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E-1 EngineE-1 Engine
Credit: © Mark Wade



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