Orbital Sciences Corporation
Pegasus Hybrid
Hybrid

Retired
Overview
/01The 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.
Manufacturer
Orbital Sciences Corporation
Variant
Hybrid
Alias
N/A
Maiden Flight
April 3, 1995
Technical Specifications
/0215.5 m
Length
1.28 m
Diameter
0 t
Launch Mass
580 kN
Liftoff Thrust
350 kg
LEO Capacity
0 kg
GTO Capacity
Launch Record
/034
Total Launches
4
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes