2012
DOI: 10.1007/978-3-642-30229-9_2
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Analyses of Hubble Space Telescope Aluminized-Teflon Insulation Retrieved After 19 Years of Space Exposure

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Cited by 5 publications
(5 citation statements)
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“…The electron irradiation doses of the outer layer of thermal blankets of the Hubble Space Telescope in the low Earth orbit roughly range from 100 kGy to about 1 MGy for the shortest servicing missions up to the defined end-of-life duration respectively [2,24]. The electron irradiation doses investigated in this study cover this dose range.…”
Section: Methodsmentioning
confidence: 99%
“…The electron irradiation doses of the outer layer of thermal blankets of the Hubble Space Telescope in the low Earth orbit roughly range from 100 kGy to about 1 MGy for the shortest servicing missions up to the defined end-of-life duration respectively [2,24]. The electron irradiation doses investigated in this study cover this dose range.…”
Section: Methodsmentioning
confidence: 99%
“…The exposure levels, based on equivalent solar hours, were estimated to be 24,300 hours for region 1 of Bay 5, 30,300 hours for the patched region (region 11) of Bay 8, and 89,300 hours for the un-patched region (region 1) of Bay 8 [4] . These equivalent solar hour estimates were determined by accounting for the time in orbit, the percent of time the material was shielded by the earth, and a region's nominal angle with respect to the sun.…”
Section: Baymentioning
confidence: 99%
“…In terms of thermal fluctuations, both bays and all regions underwent 110,000 cycles with temperatures estimated to range from -175°C to 0°C for Bay 5 and between -175°C to 40°C for Bay 8 [4] . The as-fabricated material consisting of the FEP film [14] with a thin layer of vapor deposited Al had a nominal thickness of 127μm; however, prolonged exposure to space resulted in cracking of FEP as well as cracking and partial delamination of the Al coating.…”
Section: Baymentioning
confidence: 99%
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