Space · launch vehicle
Pegasus HAPS
OSC
RETIRED
At a glance
Launches
2
Success rate
100%
2 ok · 0 failed
Payload to LEO
250 kg
Payload to GTO
0 kg
Manufacturer
Orbital Sciences CorporationStatus
RetiredFirst flight
17 Jul 1991Reusable
NoHeight
15.5 mDiameter
1.28 mLaunch mass
18 tLiftoff thrust
580 kNStages
5Launch cost
—Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
