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Nova DAC ISI-1
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Gross Mass: 3,084,000 kg (6,799,000 lb). Empty Mass: 142,000 kg (313,000 lb). Thrust (vac): 70,146.000 kN (15,769,448 lbf). Isp: 350 sec. Burn time: 141 sec. Propellants: Lox/LH2. Isp(sl): 320 sec. Diameter: 21.30 m (69.80 ft). Span: 28.00 m (91.00 ft). Length: 30.50 m (100.00 ft). Country: USA. No Engines: 14. Engine: Chamber/single nozzle. Status: Study 1963. Operational date would have been July 1977. Recoverable stage. 10% plug nozzle.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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