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Space · launch vehicle

Pegasus

OSC RETIRED
At a glance
Launches
4
Success rate
100%
4 ok · 0 failed
Payload to LEO
443 kg
Payload to GTO
0 kg
Status
Retired
First flight
05 Apr 1990
Reusable
No
Height
16.9 m
Diameter
1.27 m
Launch mass
18 t
Liftoff thrust
580 kN
Stages
3
Launch cost
$40,000,000
Booster landings
—
About

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.