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Performance of multilayer insulation systems for the 300 deg to 800 deg k temperature range.Multilayer insulation system materials and design data for use on spacecraft in temperature range from 300 to 800 degrees K
Document ID
19650053008
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cunnington, G. R.
Streed, E. R.
Zierman, C. A.
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 65-663
Report Number: AIAA PAPER 65-663
Accession Number
65A35712
Funding Number(s)
CONTRACT_GRANT: NAS2-2441
Distribution Limits
Public
Copyright
Other
Keywords
THERMAL INSULATION
MULTILAYER STRUCTURE
INSULATED STRUCTURE
SPACECRAFT SHIELDING

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