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Thermal testing of aluminized MylarThe effect of heat on aluminized Mylar film is summarized. A summary of the procedure used in testing the material, background information describing the physical properties of the material, and the experimental results of heating the material at various temperatures are included. It is revealed that aluminized Mylar film is thermally stable within the temperature range of 50 to 200 C. The information compiled will be used to determine if aluminized Mylar can be useful in space applications.
Document ID
19940006703
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lowe, D. L., II (NASA Marshall Space Flight Center Huntsville, AL, United States)
Edwards, D. L. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.15:108414
NASA-TM-108414
Report Number: NAS 1.15:108414
Report Number: NASA-TM-108414
Accession Number
94N11175
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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