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Design of multilayer insulation systemsAnalytical models for insulation system heat transfer studies the types of materials best suited for a near solar environment. This multilayer insulation system for spacecraft can operate at temperatures in the 300 to 700 degree K range.
Document ID
19690000568
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Cunnington, G. R., Jr.
Stread, E. R.
Date Acquired
August 5, 2013
Publication Date
November 1, 1969
Subject Category
Mechanics
Report/Patent Number
ARC-10166
Report Number: ARC-10166
Accession Number
69B10615
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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