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Pegasus · Orbital Sciences Corporation

Pegasus XL HAPS

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Specifications

Status
active
Height
17.6 m
Diameter
1.27 m
Mass
23,000 kg
Stages
4
Payload to LEO
443 kg
Payload to GTO
0
First flight
1997-12-23
Total launches
5
Success / Fail
5 / 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. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.

Payloads it launched · 33

ORBCOMM FM30
OrbComm · LEO
ORBCOMM FM36
OrbComm · LEO
ORBCOMM FM34
OrbComm · LEO
ORBCOMM FM35
OrbComm · LEO
ORBCOMM FM33
OrbComm · LEO
ORBCOMM FM31
OrbComm · LEO
ORBCOMM FM32
LEO
MUBLCOM
LEO
TERRIERS
LEO
ORBCOMM FM23
OrbComm · LEO
ORBCOMM FM28
OrbComm · LEO
ORBCOMM FM27
LEO
ORBCOMM FM25
OrbComm · LEO
ORBCOMM FM24
OrbComm · LEO
ORBCOMM FM26
OrbComm · LEO
ORBCOMM FM22
OrbComm · LEO
ORBCOMM FM21
OrbComm · LEO
ORBCOMM FM15
OrbComm · LEO
ORBCOMM FM19
LEO
ORBCOMM FM20
LEO
ORBCOMM FM18
OrbComm · LEO
ORBCOMM FM16
OrbComm · LEO
ORBCOMM FM14
OrbComm · LEO
ORBCOMM FM17
OrbComm · LEO