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Testing and numerical modeling of hypervelocity impact damaged Space Station multilayer insulationResults are presented of experiments measuring the degradation of the insulating capabilities of the multilayer insulation (MLI) of the Space Station Freedom, when subjected to hypervelocity impact damage. A simple numerical model was developed for use in an engineering design environment for quick assessment of thermal effect of the impact. The model was validated using results from thermal vacuum tests on MLI with simulated damage. The numerical model results agreed with experimental data.
Document ID
19930028020
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rule, William K.
(Alabama Univ. Tuscaloosa, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1992
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 29
Issue: 5
ISSN: 0022-4650
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93A12017
Funding Number(s)
CONTRACT_GRANT: NAS8-38555
Distribution Limits
Public
Copyright
Other

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