Nova 2 F-1 Module
Nova NASA 8 F-1
Nova NASA 8 F-1 Modular
Credit - © Mark Wade
Gross Mass: 1,134,000 kg (2,500,000 lb). Empty Mass: 77,000 kg (169,000 lb). Thrust (vac): 15,121.000 kN (3,399,336 lbf). Isp: 304 sec. Burn time: 200 sec. Propellants: Lox/Kerosene. Isp(sl): 265 sec. Diameter: 10.10 m (33.10 ft). Span: 10.10 m (33.10 ft). Length: 28.70 m (94.10 ft). Country: USA. No Engines: 2. Engine: F-1. Status: Study 1960.

Short Nova building block. Four used in stage 1, one in stage 2.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
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