Orel V6

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Orel V6

Part of Orel

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.

Status: Study 1997. Payload: 10,000 kg (22,000 lb). Thrust: 12,000.00 kN (2,697,000 lbf). Gross mass: 930,000 kg (2,050,000 lb). Height: 58.00 m (190.00 ft). Diameter: 32.00 m (104.00 ft). Apogee: 200 km (120 mi).

LEO Payload: 10,000 kg (22,000 lb) to a 200 km orbit at 51.00 degrees.

Family: orbital launch vehicle, Winged. Country: Russia.

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