Pegasus Hybrid
OSC
Details
Height
15.5 m
Diameter
1.28 m
GTO
0 kg
LEO
350 kg
Thrust at Liftoff
580 kN
Apogee
4,000 km
Launch Cost
Unknown
Maiden Flight
April 3, 1995
Description
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.