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Pegasus (trademark) launch operations and the PegaStar integrated spacecraft busThe Pegasus air launched space booster, which successfully flew its maiden flight on 5 Apr. 1990, provides the international satellite community with a flexible cost effective means for delivering small payloads into low Earth orbit. The vehicle's simple, robust design and horizontal integration methods ensure maximum reliability and significantly reduce launch base infrastructure requirements. The vehicle's air launched approach and ability to launch over open ocean regions provide unmatched flexibility in launch location and approach used to ensure range safety. The PegaStar integrated spacecraft bus, which complements the Pegasus launch system, can provide a turnkey means for delivering instrument and sensor packages into low Earth orbit and providing extended (5 to 10 year) on orbit operational support. Pegasus and PegaStar are described, including payload interfaces, delivery capability; integration methods, facility and ground support equipment requirements; and typical launch operations.
Document ID
19920011487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mosier, Marty
(Orbital Sciences Corp. Fairfax, VA, United States)
Lindberg, Robert
(Orbital Sciences Corp. Fairfax, VA, United States)
Lyon, Keith
(Orbital Sciences Corp. Fairfax, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Publication Information
Publication: ESA, Launch Bases and Control Infrastructures for Spacecraft
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
92N20729
Distribution Limits
Public
Copyright
Other

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