|
VTOVL orbital launch vehicle. Year: 1992. Family: VTOVL. Country: Russia. Status: Study 1997. Fully reusable vertical takeoff / vertical landing single stage to orbit. Concept abandoned in favor of Orel V6 by 1998 due to engine reliability concerns. Tripropellant Lox/Kerosene (RG-1)/LH2 version. LEO Payload: 10,000 kg (22,000 lb). to: 200 km Orbit. at: 51.00 degrees. Total Mass: 1,058,000 kg (2,332,000 lb). Core Diameter: 15.10 m (49.50 ft). Total Length: 39.90 m (130.90 ft).
|