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NASA standard GAS Can satelliteThe Get-Away Special canister (GAS Can) satellite is a small, (150 lb) low-cost satellite making it possible for commercial and scientific institutions to conduct experiments in space on an economical and short-term basis. The current model is called Xsat (Exceptional Satellite) and is designed to be launched from a GAS canister on the STS Orbiter; also provided is a low-cost automated PC-operated ground station for commercial, scientific, and government users. The Xsat structure is diagrammed, and details such as payload interface, weight restrictions, and structural loads are described in detail, pointing out that Xsat has a maximum payload weight of 50 lbs, and has a natural vibration frequency of around 45 Hz, with a minimum requiremet of 35 Hz. Thermal designs, power system, electronics, computer design and bus system, and satellite operations are all outlined.
Document ID
19900063555
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cudmore, Patrick H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mcintosh, W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Edison, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Nichols, S.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mercier, E.
(Defense Systems, Inc. McLean, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90A50610
Distribution Limits
Public
Copyright
Other

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