Pegasus XL HAPS
HAPS

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. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.
Manufacturer
Variant
Alias
Maiden Flight
Technical Specifications
/02Length
Diameter
Launch Mass
Liftoff Thrust
LEO Capacity
GTO Capacity
Launch Record
/03Total Launches
Successful
Failed
Success Rate
Attempted Landings
Successful Landings
Failed Landings
Consecutive Successes