Nova MM T10RR-2-1
Nova Model T10RR-2
Nova Martin Marietta Model T10RR-2
Credit - © Mark Wade
Gross Mass: 9,089,000 kg (20,037,000 lb). Empty Mass: 680,000 kg (1,490,000 lb). Thrust (vac): 176,686.000 kN (39,720,592 lbf). Isp: 304 sec. Burn time: 139 sec. Propellants: Lox/LH2. Isp(sl): 271 sec. Diameter: 21.30 m (69.80 ft). Span: 30.10 m (98.70 ft). Length: 43.50 m (142.70 ft). Country: USA. No Engines: 24. Engine: CD Module. Status: Study 1963.

Operational date would have been December 1976. Recoverable stage.


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.

 
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