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Pegasus XL

Pegasus familyOrbital Sciences CorporationActive

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.

Pegasus XL vehicle

Specifications

Thrust
580 kN
Height
17.6 m
Diameter
1.27 m
Launch mass
23 t
Stages
3
Launch cost
$40M
LEO capacity
443 kg
GTO capacity
0 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

32flightswith a definitive outcome
90.6%success rate29 of 32
3failuresincluding partial failures
26success streakcurrent

First flight June 27, 1994 · latest July 3, 2026 · 08:36 UTC

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Pegasus XL flights per year
Pegasus XL flights per year
YearSuccessfulFailedTotal
1994011
1995011
1996314
1997404
1998303
1999101
2000101
2001000
2002101
2003404
2004000
2005101
2006202
2007101
2008202
2009000
2010000
2011000
2012101
2013101
2014000
2015000
2016101
2017000
2018000
2019101
2020000
2021101
2022000
2023000
2024000
2025000
2026101

Flights

5 of 32

All 32 flights