Shuttle R134C-2

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 R134C-2

Part of Shuttle-2 stage series

LOx/LH2 propellant rocket stage. Delta winged configuration.

Status: Study 1970. Thrust: 4,804.13 kN (1,080,011 lbf). Gross mass: 424,449 kg (935,749 lb). Unfuelled mass: 138,910 kg (306,240 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 264 s. Height: 64.02 m (210.03 ft). Diameter: 4.57 m (14.99 ft). Span: 37.80 m (124.00 ft).

No Engines: 2.

Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle R134C. 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