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Hubble Space Telescope Thermal Blanket Repair Design and ImplementationSubstantial damage to the outer layer of Hubble Space Telescope (HST) thermal blankets was observed during the February 1997 servicing mission. After six years in LEO, many areas of the aluminized Teflon(R) outer blanket layer had significant cracks, and some material was peeled away to expose inner layers to solar flux. After the mission, the failure mechanism was determined, and repair materials and priorities were selected for follow-on missions. This paper focuses on the thermal, mechanical, and EVA design requirements for the blanket repair, the creative solutions developed for these unique problems, hardware development, and testing.
Document ID
20000075210
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ousley, Wes
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Skladany, Joseph
(Orbital Sciences Corp. United States)
Dell, Lawrence
(Lockheed Martin Technical Operations, Inc. Greenbelt, MD United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Astronomy
Meeting Information
Meeting: 30th International Conference on Environmental Systems (ICES)
Location: Toulouse
Country: France
Start Date: July 10, 2000
End Date: July 14, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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