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The Pegasus air-launched space booster payload interfaces and processing procedures for small optical payloadsPegasus and the PegaStar integrated spacecraft bus are described, and an overview of integration and launch operations is provided. Payload design issues include payload volume and mass capability, payload interfaces, and design loads. Vehicle and payload processing issues include integration and handling methods, facilities, contamination control, and launch operations. It is noted that Pegasus provides small satellite users with a cost-effective means for delivering payloads into the specific orbits at the optimal time to meet the most demanding mission requirements. PegaStar provides a flexible cost-effective means for providing long-term on-orbit support while minimizing total program risk and cost.
Document ID
19930040173
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mosier, Marty
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Harris, Gary
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Whitmeyer, Charlie
(Orbital Sciences Corp. Fairfax, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Small-satellite technology and applications; Proceedings of the Meeting, Orlando, FL, Apr. 4, 5, 1991 (A93-24151 08-18)
Publisher: Society of Photo-Optical Instrumentation Engineers
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
93A24170
Distribution Limits
Public
Copyright
Other

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