Shuttle LS200-1

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

Shuttle LS200-1

Part of Starlifter

LOx/LH2 propellant rocket stage. High-fineness lifting-body configuration. Cross Range 2,419 km.

AKA: Starlifter. Status: Study 1971. Thrust: 27,422.00 kN (6,164,711 lbf). Gross mass: 1,730,803 kg (3,815,767 lb). Unfuelled mass: 133,514 kg (294,347 lb). Specific impulse: 455 s. Specific impulse sea level: 352 s. Burn time: 256 s. Height: 47.71 m (156.52 ft). Diameter: 4.57 m (14.99 ft). Span: 28.05 m (92.02 ft).

No Engines: 9.

Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle LS200. Propellants: Lox/LH2.

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