H-1c (original) (raw)

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H-1c

Part of LR79

Rocketdyne LOx/Kerosene rocket engine. Study Saturn IB-A, Saturn IB-B, 1965.

Status: Study 1965. Thrust: 1,130.00 kN (254,030 lbf). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 128 s.

Country: USA. Launch Vehicles: Saturn IB-A, Saturn IB-B. Propellants: Lox/Kerosene. Stages: Saturn S-IB-A. Agency: Rocketdyne.

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