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Pegasus

Pegasus

Pegasus family · built by Orbital Sciences Corporation · maiden flight 1990-04-05

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.

Specifications

16.9 mLength
1.27 mDiameter
18 tLaunch mass
3Stages
580 kNLiftoff thrust

Payload Capacity

443 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.

4Total launches
4Successful
0Failed
0Upcoming

Launches Tracked on This Site

4In our archive
100.0%Success rate
Apr 05, 1990 19:10 UTCEarliest tracked
Aug 03, 1994 14:38 UTCMost recent
MissionDateStatus
Pegasus | APEX Aug 03, 1994 14:38 UTC Success
Pegasus | Array of Low Energy X-ray Imaging Sensors (ALEXIS) Apr 25, 1993 13:56 UTC Success
Pegasus | Satélite de Coleta de Dados-1 (SCD-1) Feb 09, 1993 14:30 UTC Success
Pegasus | Pegsat, NavySat Apr 05, 1990 19:10 UTC Success

Wikipedia