|
Centaur G
|
|
Gross Mass: 23,880 kg (52,640 lb). Empty Mass: 2,775 kg (6,117 lb). Thrust (vac): 146.800 kN (33,002 lbf). Isp: 444 sec. Burn time: 625 sec. Propellants: Lox/LH2. Diameter: 4.33 m (14.20 ft). Span: 4.33 m (14.20 ft). Length: 9.00 m (29.50 ft). Country: USA. No Engines: 2. Engine: RL-10A-3A. Cost $ : 23.000 million. First Flight: 1989. Last Flight: 2005. No Launched: 39. Centaur for Titan 4 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.
|
|
|
|