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Thermal control surfaces experiment flight system performanceThe Thermal Control Surfaces Experiment (TCSE) is the most complex system, other than the LDEF, retrieved after long term space exposure. The TCSE is a microcosm of complex electro-optical payloads being developed and flow by NASA and the DoD including SDI. The objective of TCSE was to determine the effects of the near-Earth orbital environment and the LDEF induced environment on spacecraft thermal control surfaces. The TCSE was a comprehensive experiment that combined in-space measurements with extensive post flight analyses of thermal control surfaces to determine the effects of exposure to the low earth orbit space environment. The TCSE was the first space experiment to measure the optical properties of thermal control surfaces the way they are routinely measured in a lab. The performance of the TCSE confirms that low cost, complex experiment packages can be developed that perform well in space.
Document ID
19910020880
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wilkes, Donald R.
(AZ Technology Huntsville, AL., United States)
Hummer, Leigh L.
(AZ Technology Huntsville, AL., United States)
Zwiener, James M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:105036
NASA-TM-105036
Report Number: NAS 1.15:105036
Report Number: NASA-TM-105036
Accession Number
91N30194
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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