|
R-1
|
|
Gross Mass: 12,630 kg (27,840 lb). Empty Mass: 4,066 kg (8,963 lb). Thrust (vac): 307.085 kN (69,035 lbf). Isp: 233 sec. Burn time: 63 sec. Propellants: Lox/Alcohol. Isp(sl): 206 sec. Diameter: 1.65 m (5.42 ft). Span: 3.54 m (11.61 ft). Length: 14.15 m (46.42 ft). Country: Russia. No Engines: 1. Engine: RD-100. First Flight: 1948. Last Flight: 1964. No Launched: 184. No Failed: 15. Other designations: 8A11. Payload 815 / 483 kg. Range 270 km. Maximum altitude 77 km. Time of flight 5 minutes. Max velocity at burnout 1465 m/s. Accuracy 8 km in range, 4 km laterally.
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.
|
|
|
|