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Shuttle LCR-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 Shuttle LCR-1 Part of Shuttle-1 stage series LOx/LH2 propellant rocket stage. Swept winged configuration.

Status: Study 1969. Thrust: 27,054.52 kN (6,082,097 lbf). Gross mass: 1,512,381 kg (3,334,229 lb). Unfuelled mass: 286,621 kg (631,891 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 193 s. Height: 75.15 m (246.55 ft). Diameter: 10.00 m (32.00 ft). Span: 46.04 m (151.04 ft).

No Engines: 13.

Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle LCR. 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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