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Super-Jupiter stage

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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 Super-Jupiter stage Part of S-I stage E-1 Engine Credit: © Mark Wade LOx/Kerosene propellant rocket stage. Earliest member of what would become the Saturn family. Masses estimated. AKA: Super-Jupiter. Status: Study 1957. Thrust: 7,538.30 kN (1,694,677 lbf). Gross mass: 317,600 kg (700,100 lb). Unfuelled mass: 19,600 kg (43,200 lb). Specific impulse: 290 s. Specific impulse sea level: 260 s. Burn time: 110 s. Height: 22.00 m (72.00 ft). Diameter: 5.23 m (17.15 ft). Span: 5.23 m (17.15 ft). No Engines: 4. Country: USA. Engines: E-1. Launch Vehicles: Super-Jupiter. Propellants: Lox/Kerosene. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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 © 1997-2019 Mark Wade - Contact © / Conditions for Use

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