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Pegasus Hybrid (Orbital Sciences Corporation)

Pegasus Hybrid
Photo Credit: NASA

The Pegasus Hybrid is a non-reusable, inactive launch vehicle manufactured by Orbital Sciences Corporation. It undertook its inaugural launch on 04/03/1995.

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.

Pegasus Hybrid Specifications

Technical specifications for Pegasus Hybrid
VariantHybrid
Length15.5 m
Diameter1.28 m
Stages3
Launch Mass18 T
Takeoff Thrust580 kN
Apogee4000 km
LEO Capacity350 kg

Pegasus Hybrid Launch Record

Launch statistics for Pegasus Hybrid
Total Launches4
Successful Launches4
Consecutive Successful Launches4

Manufacturer

Orbital Sciences Corporation (OSC)
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