This page no longer updated from 31 October 2001. Latest version can be found at L-1011

L1011 Pegasus Launch
L1011 Pegasus Launch
L1011 Pegasus Launcher

20,913 bytes. 596 x 210 pixels.

Gross Mass: 156,000 kg. Empty Mass: 109,629 kg. Thrust (vac): 57,300 kgf. Isp: 9,900 sec. Burn time: 4,590 sec. Propellants: Air/Kerosene Isp(sl): 9,000 sec. Diameter: 16.9 m. Span: 47.0 m. Length: 54.0 m. Country: USA. No Engines: 3. RB-211-22B Status: Hardware. Comments: Lockheed airliner swept wing. Release conditions: Belly-mounted, 36,800 kg, 17.1 m length x 7.9 m span at 925 kph at 11,890 m altitude.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .