Nova DAC 2-2
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit - © Mark Wade
Gross Mass: 1,633,000 kg (3,600,000 lb). Empty Mass: 113,000 kg (249,000 lb). Thrust (vac): 13,346.000 kN (3,000,300 lbf). Isp: 426 sec. Burn time: 468 sec. Propellants: Lox/LH2. Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft). Length: 21.30 m (69.80 ft). Country: USA. No Engines: 4. Engine: M-1. Status: Study 1963.

Operational date would have been July 1977. Recoverable stage.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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