This page no longer updated from 31 October 2001. Latest version can be found at MLLV-0

Gross Mass: 1,920,200 kg. Empty Mass: 192,000 kg. Thrust (vac): 4,511,100 kgf. Isp: 263 sec. Burn time: 99 sec. Propellants: Solid Isp(sl): 238 sec. Diameter: 6.6 m. Span: 6.6 m. Length: 54.8 m. Country: USA. No Engines: 1. AJ-260X Status: Development 1968. Comments: Boeing study, 1969.
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Last update 12 March 2001.
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© Mark Wade, 2001 .