S-4 engine (original) (raw)

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S-4 engine

Part of LR105

Rocketdyne LOx/Kerosene rocket engine. Design ca. 1957. Version of Atlas sustainer tailored to Redstone Arsenal upper-stage requirements. Paper study only. Used on Super Jupiter launch vehicle.

AKA: S-4. Status: Design ca. 1957. Date: 1957. Thrust: 412.80 kN (92,801 lbf).

Country: USA. Launch Vehicles: Super-Jupiter. Propellants: Lox/Kerosene. Stages: Super-Jupiter-3. Agency: Rocketdyne.

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