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Gross Mass: 150,000 kg.
Empty Mass: 10,000 kg. Thrust (vac): 300,000 kgf. Isp: 130 sec. Burn time: 137 sec. Propellants: Lox/Kerosene Isp(sl): 256 sec. Diameter: 6.1 m. Span: 6.1 m. Length: 16.0 m. Country: USA. No Engines: 4. LR-89-5 Status: Study 1959. Comments: Masses estimated (cluster of four Titan I first stages).
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Last update 12 March 2001.
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© Mark Wade, 2001 .