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Nova MM T10RR-3-2
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Gross Mass: 1,229,000 kg (2,709,000 lb). Empty Mass: 136,000 kg (299,000 lb). Thrust (vac): 12,052.000 kN (2,709,397 lbf). Isp: 454 sec. Burn time: 397 sec. Propellants: Lox/LH2. Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft). Length: 21.80 m (71.50 ft). Country: USA. No Engines: 2. Engine: CD Module. Status: Study 1963. Operational date would have been July 1977. Recoverable stage.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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