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S-4 engine
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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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