Centaur IIA
Class: Tug. Nation: USA.

Upper stage / space tug - out of production. Launched by Atlas IIA.

Unit Cost $: 30.000 million. Length: 10.10 m (33.10 ft). Basic Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Mass: 19,073 kg (42,048 lb). Main Engine: RL-10A-4. Main Engine: 168 kg (370 lb). Main Engine Thrust: 185.012 kN (41,592 lbf). Main Engine Propellants: Lox/LH2. Main Engine Propellants: 16,780 kg (36,990 lb). Main Engine Isp: 449 sec.  
 
 
 
 
 
 
 
 


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.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z