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Thermal control surfaces experiment (SOO69) flight systems performanceThe thermal control surfaces experiment (TCSE) was the most complex hardware system aboard the Long Duration Exposure Facility (LDEF). The TCSE system consists of a scanning spectroreflectometer that measured test samples mounted on a rotatable carousel assembly. A microprocessor based data system controlled all aspects of TCSE system operation. Power was provided by four primary batteries. Flight measurement and housekeeping data were stored on a tape recorder for postflight analysis. The TCSE is a microcosm of complex electro-optical payloads being developed by NASA, DoD, and the aerospace community. The TCSE provides valuable data on the performance of these systems in space. The TCSE flight system and its excellent performance on the LDEF mission are described. A few operational anomalies were encountered and are discussed. Initial post-flight tests show that the TCSE system remains functional although some degradation in the optical measurements were observed. The results of these tests are also presented.
Document ID
19910015774
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilkes, Donald R.
(AZ Technology Huntsville, AL, United States)
Hummer, Leigh L.
(AZ Technology Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1991
Publication Information
Publication: NASA, Langley Research Center, First LDEF Post-Retrieval Symposium Abstracts
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N25088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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