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Pegasus XL HAPS (Orbital Sciences Corporation)

Pegasus XL HAPS
Photo Credit: NASA/Laurie Losey

The Pegasus XL HAPS is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 12/23/1997.

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 HAPS Specifications

Technical specifications for Pegasus XL HAPS
VariantHAPS
Length17.6 m
Diameter1.27 m
Stages4
Launch Mass23 T
Takeoff Thrust580 kN
Apogee4000 km
LEO Capacity443 kg
Launch Cost$40,000,000

Pegasus XL HAPS Launch Record

Launch statistics for Pegasus XL HAPS
Total Launches5
Successful Launches5
Consecutive Successful Launches5

Manufacturer

Orbital Sciences Corporation (OSC)
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