Pegasus XL

Active

Orbital Sciences Corporation (OSC)

June 27, 1994

Description

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.

Specifications
  • Max Stage
    3
  • Length
    17.6 m
  • Diameter
    1.27 m
  • Fairing Diameter
  • Launch Mass
    23.0 T
  • Thrust
    580.0 kN
  • Apogee (Sub-Orbital)
    4000.0 km
Family
  • Name
    Pegasus XL
  • Family
  • Variant
  • Alias
  • Full Name
    Pegasus XL
Payload Capacity
  • Launch Cost
    $40000000
  • Low Earth Orbit
    443.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Orbital Sciences Corporation

Commercial
None
OSC

Upcoming Spaceflights


Pegasus XL | Swift Rescue Mission

Orbital Sciences Corporation | United States of America
Air launch to orbit
TBD June, 2026
Status: To Be Determined
Mission:

Contracted by NASA under the Small Business Innovation Research Phase 3 contract, Katalyst Space Technologies' LINK servicing spacecraft will rendezvous and attach to NASA’s Neil Gehrels Swift Observatory to re-boost its orbit. This aims to demonstrate a key capability for the future of space exploration and extending the Swift mission’s science lifetime in gamma ray astronomy.

Low Earth Orbit
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