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Pegasus · Orbital Sciences Corporation

Pegasus

retired
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Specifications

Status
retired
Height
16.9 m
Diameter
1.27 m
Mass
18,000 kg
Stages
3
Payload to LEO
443 kg
Payload to GTO
0
First flight
1990-04-05
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

APEX
LEO
ALEXIS
LEO
OXP 1
LEO
SCD 1
LEO
PEGSAT
LEO
USA 55
LEO