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Nova MM 34-1
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Gross Mass: 10,126,000 kg (22,324,000 lb). Empty Mass: 544,000 kg (1,199,000 lb). Thrust (vac): 30,685.000 kN (6,898,262 lbf). Isp: 439 sec. Burn time: 388 sec. Propellants: Lox/LH2. Isp(sl): 382 sec. Diameter: 24.40 m (80.00 ft). Span: 24.40 m (80.00 ft). Length: 84.80 m (278.20 ft). Country: USA. No Engines: 4. Engine: L6H. Status: Study 1963. Operational date would have been June 1976. Sustainer stage (required 4-engine booster stage).
Used on Launch Vehicles:
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