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Pegasus XL (Orbital Sciences Corporation)

Pegasus XL
Photo Credit: NASA/Laurie Losey

The Pegasus XL is a non-reusable, active launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 06/27/1994.

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.

Pegasus XL Specifications

Technical specifications for Pegasus XL
Length17.6 m
Diameter1.27 m
Stages3
Launch Mass23 T
Takeoff Thrust580 kN
Apogee4000 km
LEO Capacity443 kg
Launch Cost$40,000,000

Pegasus XL Launch Record

Launch statistics for Pegasus XL
Total Launches32
Successful Launches29
Failed Launches3
Consecutive Successful Launches26

Manufacturer

Orbital Sciences Corporation (OSC)
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