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Pegasus/HAPS
Part of Pegasus
American air-launched orbital launch vehicle. Five stage version consisting of 1 x NB-52 + 1 x Orion 50S + 1 x Orion 50 + 1 x Orion 38 + 1 x HAPS

Status: Retired 1994. First Launch: 1991-07-17. Last Launch: 1994-05-19. Number: 2 . Payload: 250 kg (550 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: 250 kg (550 lb).

More at: Pegasus/HAPS.
Family: aircraft-launched, orbital launch vehicle. Country: USA. Spacecraft: Microsat, Eagle, STEP. Launch Sites: Point Arguello WADZ. Stages: Pegasus-4, L-1011, Pegasus-1, Pegasus-2, Pegasus-3. Agency: OSC.
1991 July 17 - . 17:33 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Edwards.. Launch Platform: NB-52 008. LV Family: Pegasus. Launch Vehicle: Pegasus/HAPS. Failed Stage: G.
1994 May 19 - . 17:03 GMT - . Launch Site: Point Arguello. Launch Complex: Point Arguello WADZ. Launch Pad: Aircraft from Edwards.. Launch Platform: NB-52 008. LV Family: Pegasus. Launch Vehicle: Pegasus/HAPS.
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