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Pegasus · Orbital Sciences Corporation

Pegasus Hybrid

retired
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Specifications

Status
retired
Height
15.5 m
Diameter
1.28 m
Mass
18,000 kg
Stages
3
Payload to LEO
350 kg
Payload to GTO
0
First flight
1995-04-03
Total launches
4
Success / Fail
4 / 0

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.

Payloads it launched · 6

HETE-2
LEO
SCD 2
LEO
MSTI 3
LEO
ORBCOMM FM01
OrbComm · LEO
ORBCOMM FM02
OrbComm · LEO
ORBVIEW 1 (MICROLAB)
LEO