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
Spacemaster-2
Part of Starlifter
LOx/LH2 propellant rocket stage. Delta Winged, Cross Range 2,742 km.

Status: Study 1967. Thrust: 4,549.05 kN (1,022,667 lbf). Gross mass: 362,812 kg (799,863 lb). Unfuelled mass: 80,000 kg (176,000 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 276 s. Height: 48.78 m (160.03 ft). Diameter: 6.71 m (22.01 ft). Span: 32.62 m (107.02 ft).

No Engines: 2.



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
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