Venturestar
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
American SSTO winged orbital launch vehicle. Production reusable single-stage-to-orbit launch vehicle using technology developed in X-33 test bed.
LEO Payload: 26,800 kg (59,000 lb) to a 185 km orbit at 28.00 degrees.
Related
- Country
- USA
- Engines
- RS-2200
- Launch Vehicles
- Venturestar
- Propellants
- Lox/LH2
- Agency
- Lockheed