Space · launch vehicle
Pegasus Hybrid
OSC
RETIRED
At a glance
Launches
4
Success rate
100%
4 ok · 0 failed
Payload to LEO
350 kg
Payload to GTO
0 kg
Manufacturer
Orbital Sciences CorporationStatus
RetiredFirst flight
03 Apr 1995Reusable
NoHeight
15.5 mDiameter
1.28 mLaunch mass
18 tLiftoff thrust
580 kNStages
3Launch 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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
