|
R-36-0-1
|
|
Gross Mass: 125,000 kg (275,000 lb). Empty Mass: 8,500 kg (18,700 lb). Thrust (vac): 2,640.000 kN (593,490 lbf). Isp: 301 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 269 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 18.90 m (62.00 ft). Country: Ukraine. No Engines: 1. Engine: RD-251. Status: Out of production. Cost $ : 6.000 million. First Flight: 1965. Last Flight: 1971. No Launched: 25.
Used on Launch Vehicles:
|
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2007 except where otherwise noted.
|
|
|
|