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Hubble Space telescope thermal cycle test report for large solar array samples with BSFR cells (Sample numbers 703 and 704)The Hubble space telescope (HST) solar array was designed to meet specific output power requirements after 2 years in low-Earth orbit, and to remain operational for 5 years. The array, therefore, had to withstand 30,000 thermal cycles between approximately +100 and -100 C. The ability of the array to meet this requirement was evaluated by thermal cycle testing, in vacuum, two 128-cell solar cell modules that exactly duplicated the flight HST solar array design. Also, the ability of the flight array to survive an emergency deployment during the dark (cold) portion of an orbit was evaluated by performing a cold-roll test using one module.
Document ID
19930001621
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Alexander, D. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-TM-108373
NAS 1.15:108373
Report Number: NASA-TM-108373
Report Number: NAS 1.15:108373
Accession Number
93N10809
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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