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Nova MM 34
Part of Nova
Nova Model 34
Nova Model 34
Nova Martin Marietta Model 34
Credit: © Mark Wade
American heavy-lift orbital launch vehicle. Nova 1 1/2 stage design with 4 new 3 million kgf LH2/LOx engines in the jettisonable booster section and a single 3 million kgf sustainer. Operational date would have been June 1976.

Status: Study 1963. Payload: 531,000 kg (1,170,000 lb). Thrust: 133,512.70 kN (30,014,849 lbf). Gross mass: 10,990,200 kg (24,229,200 lb). Height: 102.00 m (334.00 ft). Diameter: 24.40 m (80.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 531,000 kg (1,170,000 lb) to a 185 km orbit.

Stage Data - Nova MM 34



Family: heavy-lift, orbital launch vehicle. Country: USA. Engines: L6H. Stages: Nova MM 34-0, Nova MM 34-1. Agency: Martin.
Photo Gallery

Nova 24G, 34, and 33Nova 24G, 34, and 33
Nova Martin Marietta designs 24G, 34, and 33
Credit: Lockheed Martin



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