Pegasus Hybrid Vehicle Overview
A complete overview of the Pegasus Hybrid launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Pegasus Hybrid
Family
Pegasus
Manufacturer
First Launch
3 Apr 1995
Successful Launches
4
Failed Launches
0
Rocket Info
Status
Inactive
Stages
0-3
Length
15.5 m
Diameter
1.28 m
Launch Mass
18 tons
Thrust
580 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
350 kg
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.
Launch Sites used by Pegasus Hybrid
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.
Vandenberg SFB
U.S. Space Force facility in California for spacecraft launches and missile testing.
