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
SSME Plus
Part of SSME Family
Notional LOx/LH2 rocket engine. VTOHL studies, 1978.

Status: Study 1978. Thrust: 3,728.70 kN (838,245 lbf). Unfuelled mass: 2,973 kg (6,554 lb). Specific impulse: 467 s. Specific impulse sea level: 385 s. Burn time: 500 s.

Thrust (sl): 3,073.900 kN (691,040 lbf). Thrust (sl): 313,458 kgf. Engine: 2,973 kg (6,554 lb). Area Ratio: 55. Thrust to Weight Ratio: 127.89.



Country: USA. Launch Vehicles: VTOHL 45t, VTOHL 9t. 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use