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
Venturestar
Part of X-33 Family
American SSTO winged orbital launch vehicle. Production reusable single-stage-to-orbit launch vehicle using technology developed in X-33 test bed.

Status: Cancelled 1999. Payload: 26,800 kg (59,000 lb). Thrust: 13,390.00 kN (3,010,190 lbf). Gross mass: 991,000 kg (2,184,000 lb). Height: 39.70 m (130.20 ft). Diameter: 39.00 m (127.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 26,800 kg (59,000 lb) to a 185 km orbit at 28.00 degrees.



Family: orbital launch vehicle, Spaceplane, SSTO, US Rocketplanes, Winged. Country: USA. Engines: RS-2200. Launch Vehicles: Venturestar. Propellants: Lox/LH2. Agency: Lockheed.

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