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 DC-3-2
Part of Shuttle-2 stage series
LOx/LH2 propellant rocket stage. Faget Configuration - Cross Range 323 km.

Status: Study 1970. Thrust: 2,940.00 kN (660,930 lbf). Gross mass: 199,238 kg (439,244 lb). Unfuelled mass: 54,422 kg (119,979 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 218 s. Height: 37.40 m (122.70 ft). Diameter: 4.45 m (14.59 ft). Span: 27.68 m (90.81 ft).

Cost $ : 18.000 million.



Country: USA. Engines: SSME Study. Launch Vehicles: Shuttle DC-3. Propellants: Lox/LH2.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use