Orel V7 RSSLV-3 (original) (raw)

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

Orel V7 RSSLV-3

Part of Orel

Russian VTOVL orbital launch vehicle. 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.

Status: Study 1997. Payload: 10,000 kg (22,000 lb). Gross mass: 1,058,000 kg (2,332,000 lb). Height: 39.90 m (130.90 ft). Diameter: 15.10 m (49.50 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.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z