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Pegasus HAPS

Pegasus HAPS

Pegasus family · built by Orbital Sciences Corporation · maiden flight 1991-07-17

Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-17

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.

Specifications

15.5 mLength
1.28 mDiameter
18 tLaunch mass
580 kNLiftoff thrust

Payload Capacity

250 kgTo LEO

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

2Total launches
2Successful
0Failed
0Upcoming

Launches Tracked on This Site

2In our archive
100.0%Success rate
Jul 17, 1991 17:33 UTCEarliest tracked
May 19, 1994 17:03 UTCMost recent
MissionDateStatus
Pegasus HAPS | Space Test Experiments Platform 2 (STEP-2) May 19, 1994 17:03 UTC Success
Pegasus HAPS | 7 microsats Jul 17, 1991 17:33 UTC Success

Wikipedia