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Orel V4
Part of Orel
Russian winged orbital launch vehicle. Fully reusable vertical takeoff, horizontal landing two stage to orbit concept. Abandoned in favor of Orel V6.

Status: Study 1997. Payload: 10,000 kg (22,000 lb). 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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