Orbital Sciences Corporation

Pegasus HAPS

HAPS

Pegasus HAPS
Retired

Overview

/01

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. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.

Manufacturer

Orbital Sciences Corporation

Variant

HAPS

Alias

N/A

Maiden Flight

July 17, 1991

Technical Specifications

/02
15.5 m

Length

1.28 m

Diameter

0 t

Launch Mass

580 kN

Liftoff Thrust

250 kg

LEO Capacity

0 kg

GTO Capacity

Launch Record

/03
2

Total Launches

2

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

← Back to Launchers