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Pegasus H
Part of Pegasus

Pegasus

Pegasus
Credit: Orbital Sciences Corporation

American air-launched orbital launch vehicle. Four stage vehicle consisting of 1 x L-1011 + 1 x Orion 50S + 1 x Orion 50 + 1 x Orion 38

Status: Retired 2000. First Launch: 1995-04-03. Last Launch: 2000-10-09. Number: 4 . Payload: 350 kg (770 lb). Thrust: 580.00 kN (130,380 lbf). Gross mass: 18,500 kg (40,700 lb). Height: 15.50 m (50.80 ft). Diameter: 1.28 m (4.19 ft). Apogee: 4,000 km (2,400 mi).

LEO Payload: 350 kg (770 lb).


More at: Pegasus H.

Family: aircraft-launched, orbital launch vehicle. Country: USA. Spacecraft: Orbcomm, MSTI, SCD, Microstar, HETE. Launch Sites: Point Arguello WADZ, Mayport DZ, Kwajalein DZ. Stages: L-1011, Pegasus-1, Pegasus-2, Pegasus-3. Agency: OSC.

1995 April 3 - . 13:48 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.
1996 May 17 - . 02:44 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Vandenberg.. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.
1998 October 23 - . 00:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Mayport DZ. Launch Pad: 29.0 N x 78.3 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.
2000 October 9 - . 05:38 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein DZ. Launch Pad: RW06/24. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus H.

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