Temir Kazyk

Rockets / Pegasus XL

PEGASUS XL

EXPENDABLE 3-STAGE LAUNCH VEHICLE

ACTIVE
Pegasus XL

Technical Overview

Length height
17.6 m
Diameter radio_button_unchecked
1.3 m
Launch Mass scale
23 t
Payload to LEO rocket
443 kg

Engine Details

Pegasus XL

Pegasus XL

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.

Reusability

Expendable

Stages

3

Liftoff Thrust

580 kN

Launch Cost

$40,000,000

Maiden Flight

1994-06-27

Fastest Turnaround

P6DT6H6M15S

Flight History

*Since 1994-06-27
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Total Launches

31

trending_up 25 consecutive successes
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Successful Launches

28

verified 90% success rate
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Failed Launches

3

schedule 1 pending