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Fusée

Pegasus XL

Orbital Sciences Corporation · États-Unis

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.

Constructeur
Orbital Sciences Corporation
Premier vol
27 juin 1994
Lancements
32
Réussis
29
Échoués
3
Taux de réussite
90,6%
Hauteur
17,6 m
Diamètre
1,27 m
Masse au décollage
23 t
Charge utile en orbite basse
443 kg
Réutilisable
non

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