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Saturn MS-IC-25(S)

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 MS-IC-25(S) Part of Saturn IC LOx/Kerosene propellant rocket stage. S-IC with 41.5 foot stretch, 6,640,0000 lbs propellant, uprated F-1 engines. Status: Study 1968. Thrust: 45,925.50 kN (10,324,463 lbf). Gross mass: 3,223,800 kg (7,107,200 lb). Unfuelled mass: 211,900 kg (467,100 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 192 s. Height: 54.70 m (179.40 ft). Diameter: 10.06 m (33.00 ft). Span: 19.00 m (62.00 ft). No Engines: 5. Country: USA. Engines: F-1A. Launch Vehicles: Saturn V-25(S)B, Saturn V-4X(U), Saturn V-25(S)U. 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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