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Spacemaster-1


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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 Spacemaster-1 Part of Starlifter LOx/LH2 propellant rocket stage. Unique Catamaran configuration.

Status: Study 1967. Thrust: 28,082.54 kN (6,313,206 lbf). Gross mass: 1,224,490 kg (2,699,530 lb). Unfuelled mass: 203,342 kg (448,292 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 155 s. Height: 57.93 m (190.05 ft). Diameter: 8.00 m (26.20 ft). Span: 45.12 m (148.03 ft).

No Engines: 14.

Country: USA. Engines: SSME Study. Launch Vehicles: Spacemaster. Propellants: Lox/LH2. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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