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 H33-2
Part of Shuttle-2 stage series Family
LOx/LH2 propellant rocket stage. Delta wing configuration with drop tanks - Cross Range 1,774 km.

Status: Study 1971. Thrust: 7,079.45 kN (1,591,524 lbf). Gross mass: 474,199 kg (1,045,429 lb). Unfuelled mass: 100,153 kg (220,799 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 234 s. Height: 47.87 m (157.05 ft). Diameter: 8.07 m (26.47 ft). Span: 29.57 m (97.01 ft).

No Engines: 3.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle H33. 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