This page no longer updated from 31 October 2001. Latest version can be found at 260 inch solid TL

Gross Mass: 561,000 kg. Empty Mass: 60,600 kg. Thrust (vac): 1,030,455 kgf. Isp: 275 sec. Burn time: 130 sec. Propellants: Solid Diameter: 6.6 m. Span: 6.6 m. Length: 21.6 m. Country: USA. No Engines: 1. AJ-260-1/3 Status: Study NASA 1969. Comments: Study NASA 1969.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .