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Pegasus·Orbital Sciences Corporation

Pegasus XL

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Specifications

Status
active
Height
17.6 m
Diameter
1.27 m
Mass
23,000 kg
Stages
3
Thrust
580 kN
Payload to LEO
443 kg
Payload to GTO
0
First flight
1994-06-27
Total launches
32
Success / Fail
29 / 3

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

39 loaded
ODYSSEY
LEO
ICON
LEO
CYGFM04
LEO
CYGFM08
LEO
CYGFM02
LEO
CYGFM06
LEO
CYGFM03
LEO
CYGFM07
LEO
CYGFM05
LEO
CYGFM01
LEO
IRIS
LEO
NUSTAR
LEO
IBEX
HEO
C/NOFS
LEO
AIM
LEO
ST5-B
LEO
ST5-C
LEO
ST5-A
MEO
DART
LEO
SCISAT 1
LEO
ORBVIEW 3
LEO
GALEX
LEO
SORCE
LEO
RHESSI
LEO
TSX-5
LEO
WIRE
LEO
SWAS
LEO
TRACE
LEO
BATSAT
LEO
SNOE
LEO
STEP M4
LEO
FORTE
LEO
ORBVIEW 2 (SEASTAR)
LEO
MINISAT 01
LEO
CELESTIS-01 & PEGASUS R/B
LEO
SAC-B & HETE & PEGASUS
LEO
FAST
MEO
TOMS EP
LEO
REX 2
LEO