Nova DAC 2-1
Nova Douglas 2
Nova Douglas Aircraft Model 2
Credit - © Mark Wade
Gross Mass: 4,943,000 kg (10,897,000 lb). Empty Mass: 311,000 kg (685,000 lb). Thrust (vac): 102,293.000 kN (22,996,381 lbf). Isp: 410 sec. Burn time: 179 sec. Propellants: Lox/LH2. Isp(sl): 345 sec. Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft). Length: 82.30 m (270.00 ft). Country: USA. No Engines: 15. Engine: M-1. Status: Study 1963.

Operational date would have been July 1977. Recoverable stage. 10% plug nozzle.


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