Pegasus XL HAPS
Orbital Sciences Corporation
Manufacturer
Orbital Sciences Corporation
Family
Pegasus
Maiden flight
1997-12-23
Length
17.6 m
Diameter
1.27 m
Payload to LEO
443 kg
Launches
5
Successful
5
The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.


Pegasus XL HAPSSuccess
Orbcomm-D2 - D8 · Orbital Sciences Corporation
Saturday, Dec 4, 1999, 18:53 UTC

Pegasus XL HAPSSuccess
MUBLCOM & TERRIERS · Orbital Sciences Corporation
Tuesday, May 18, 1999, 05:09 UTC

Pegasus XL HAPSSuccess
Orbcomm-C1 - C8 · Orbital Sciences Corporation
Wednesday, Sep 23, 1998, 05:06 UTC

Pegasus XL HAPSSuccess
Orbcomm-B1 - B8 · Orbital Sciences Corporation
Sunday, Aug 2, 1998, 16:24 UTC

Pegasus XL HAPSSuccess
Orbcomm-A1 - A8 · Orbital Sciences Corporation
Tuesday, Dec 23, 1997, 19:11 UTC