Pegasus Hybrid
Orbital Sciences Corporation
Hersteller
Orbital Sciences Corporation
Familie
Pegasus
Erstflug
1995-04-03
Länge
15.5 m
Durchmesser
1.28 m
Nutzlast LEO
350 kg
Starts
4
Erfolgreich
4
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 HybridSuccess
High Energy Transient Explorer 2 (HETE-2) · Orbital Sciences Corporation
Montag, 09.10.2000, 05:38 UTC

Pegasus HybridSuccess
Satélite de Coleta de Dados-2 (SCD-2) · Orbital Sciences Corporation
Freitag, 23.10.1998, 00:02 UTC

Pegasus HybridSuccess
Miniature Sensor Technology Integration 3 (MSTI-3) · Orbital Sciences Corporation
Freitag, 17.05.1996, 02:44 UTC

Pegasus HybridSuccess
Orbcomm F1 - F2 & OrbView-1 · Orbital Sciences Corporation
Montag, 03.04.1995, 13:48 UTC