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L-1011

L1011 Pegasus Launch

L1011 Pegasus Launch
L1011 Pegasus Launcher

Subsonic rocket launch aircraft. 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

Status: Active. Payload: 36,800 kg (81,100 lb). Thrust: 561.90 kN (126,320 lbf). Gross mass: 156,000 kg (343,000 lb). Unfuelled mass: 109,629 kg (241,690 lb). Specific impulse: 9,900 s. Specific impulse sea level: 9,000 s. Burn time: 4,590 s. Height: 54.00 m (177.00 ft). Diameter: 16.86 m (55.31 ft). Span: 47.00 m (154.00 ft). Location: 240.

Cost $ : 30.000 million. No Engines: 3. Release velocity: 240 m/s (780 ft/sec). Release altitude: 12 m (39 ft). Release conditions: 925 kph at 11.9 km.

Country: USA. Engines: RB-211-22B. Launch Vehicles: Pegasus/HAPS, Pegasus XL, Pegasus H, Pegasus XL/HAPS. Propellants: Air/Kerosene. More at: 9671.



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