Oreol Variant 6
Fully reusable vertical takeoff / horizontal landing single stage to orbit launch vehicle. The preferred long-term alternative of the Russian Orel launch vehicle study of the 1990's.
LEO Payload: 10,000 kg (22,000 lb) to a 200 km orbit at 51.00 degrees.
Status: Study 1997.
More... - Chronology...
Gross mass: 930,000 kg (2,050,000 lb).
Payload: 10,000 kg (22,000 lb).
Height: 58.00 m (190.00 ft).
Diameter: 32.00 m (104.00 ft).
Thrust: 12,000.00 kN (2,697,000 lbf).
Apogee: 200 km (120 mi).
Orel In the late 1990's the Russian space industry undertook the Orel programme to evaluate technology for future launch vehicles. The goals included evaluation of possible concepts for a future Russian launcher, reusable launch vehicle key technology research and analysis of "X-vehicle" flight demonstrators for technology validation. More...
Winged In the beginning, nobody (except Jules Verne) thought anybody would be travelling to space and back in ballistic cannon balls. The only proper way for a space voyager to return to earth was at the controls of a real winged airplane. More...
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