This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 22,517 kg.
Empty Mass: 13,394 kg. Thrust (vac): 10,766 kgf. Isp: 2,020 sec. Burn time: 6,000 sec. Propellants: Air/Kerosene Isp(sl): 1,836 sec. Diameter: 5.0 m. Span: 11.7 m. Length: 19.2 m. Country: USA. No Engines: 2. J79-17 Status: Hardware. Comments: McDonnell Fighter-cropped delta. Maximum release conditions: 5,442 kg at 2,353 kph at 17,820 m altitude.
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 .