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Pegasus XL HAPS

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. The HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.

Pegasus XL HAPS vehicle

Specifications

Thrust
580 kN
Height
17.6 m
Diameter
1.27 m
Launch mass
23 t
Stages
4
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

5flightswith a definitive outcome
100%success rate5 of 5
0failuresincluding partial failures
5success streakcurrent

First flight December 23, 1997 · 19:11 UTC · latest December 4, 1999

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 HAPS flights per year
Pegasus XL HAPS flights per year
YearSuccessfulFailedTotal
1997101
1998202
1999202

Flights

5 of 5