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Saturn S-IB-2

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 Saturn S-IB-2 Part of S-I stage LOx/Kerosene propellant rocket stage. . Status: Study 1960. Thrust: 13,339.96 kN (2,998,941 lbf). Gross mass: 725,491 kg (1,599,433 lb). Unfuelled mass: 68,014 kg (149,945 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 139 s. Height: 34.50 m (113.10 ft). Diameter: 8.25 m (27.06 ft). Span: 10.00 m (32.00 ft). No Engines: 2. Country: USA. Engines: F-1. Launch Vehicles: Saturn C-3. 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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