Nova MM 1B-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 1,361,000 kg (3,000,000 lb). Empty Mass: 122,000 kg (268,000 lb). Thrust (vac): 13,346.000 kN (3,000,300 lbf). Isp: 428 sec. Burn time: 383 sec. Propellants: Lox/LH2. Diameter: 20.00 m (65.00 ft). Span: 20.00 m (65.00 ft). Length: 45.40 m (148.90 ft). Country: USA. No Engines: 2. Engine: M-1. Status: Study 1963.

Operational date would have been February 1973

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