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Model: Nova DAC-2. Gross Mass: 2,268,000 kg (5,000,000 lb). Empty Mass: 143,000 kg (315,000 lb). Thrust (vac): 26,683.000 kN (5,998,577 lbf). Isp: 426 sec. Burn time: 327 sec. Propellants: Lox/LH2. Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft). Length: 27.40 m (89.80 ft). Country: USA. No Engines: 4. Motor: M-1. Status: Study 1963. Operational date would have been July 1977. Recoverable stage.
Model: Nova DAC 2-2. 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. Motor: M-1. Status: Study 1963. Operational date would have been July 1977. Recoverable stage.
Model: Nova DAC ISI-2. Gross Mass: 1,696,000 kg (3,739,000 lb). Empty Mass: 107,000 kg (235,000 lb). Thrust (vac): 33,754.000 kN (7,588,201 lbf). Isp: 455 sec. Burn time: 206 sec. Propellants: Lox/LH2. Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft). Length: 30.50 m (100.00 ft). Country: USA. No Engines: 8. Motor: Chamber/single nozzle. Status: Study 1963. Operational date would have been July 1977. Recoverable stage.
Used on Launch Vehicles:
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