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The performance of thermal control coatings on LDEF and implications to future spacecraftThe stability of thermal control coatings over the lifetime of a satellite or space platform is crucial to the success of the mission. With the increasing size, complexity, and duration of future missions, the stability of these materials becomes even more important. The Long Duration Exposure Facility (LDEF) offered an excellent testbed to study the stability and interaction of thermal control coatings in the low-Earth orbit (LEO) space environment. Several experiments on LDEF exposed thermal control coatings to the space environment. This paper provides an overview of the different materials flown and their stability during the extended LDEF mission. The exposure conditions, exposure environment, and measurements of materials properties (both in-space and postflight) are described. The relevance of the results and the implications to the design and operation of future space vehicles are also discussed.
Document ID
19940026508
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilkes, Donald R.
(AZ Technology Huntsville, AL., United States)
Miller, Edgar R.
(AZ Technology Huntsville, AL., United States)
Mell, Richard J.
(AZ Technology Huntsville, AL., United States)
Lemaster, Paul S.
(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
December 1, 1993
Publication Information
Publication: LDEF Materials Results for Spacecraft Applications
Subject Category
Nonmetallic Materials
Accession Number
94N31013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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