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Saturn MS-II-3B

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-II-3B Part of Saturn II LOx/LH2 propellant rocket stage. S-II with 15.5 foot stretch, 1.29 million pounds propellant, 7 x 400,000 lb thrust toroidal engines. Status: Study 1967. Thrust: 12,455.40 kN (2,800,085 lbf). Gross mass: 643,200 kg (1,418,000 lb). Unfuelled mass: 53,500 kg (117,900 lb). Specific impulse: 447 s. Specific impulse sea level: 200 s. Burn time: 204 s. Height: 29.56 m (96.98 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft). No Engines: 5. Country: USA. Engines: Toroidal 400k. Launch Vehicles: Saturn V-3B. Propellants: Lox/LH2. 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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