Shuttle H33-1

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Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- 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 H33-1 Part of Shuttle-1 stage series LOx/LH2 propellant rocket stage. Swept wing configuration.

Status: Study 1971. Thrust: 24,973.40 kN (5,614,243 lbf). Gross mass: 1,489,717 kg (3,284,263 lb). Unfuelled mass: 224,431 kg (494,785 lb). Specific impulse: 442 s. Specific impulse sea level: 392 s. Burn time: 216 s. Height: 74.70 m (245.00 ft). Diameter: 10.00 m (32.00 ft). Span: 54.12 m (177.55 ft).

No Engines: 12.

Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle H33. Propellants: Lox/LH2. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- 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 © 1997-2019 Mark Wade - Contact © / Conditions for Use

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