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Lightweight thermal insulation for Mars surface applicationsThe intent of this paper is to present a novel insulation design approach, to report the comparison testing against fiberglass batt material, and to summarize the design parameters such as effective thermal conductivity, mass, cost, and delivery time for the fiberglass batt material and this new insulation.
Document ID
20210004881
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Stultz, J.
Novak, K.
Birur, G.
Tsuyuki, G. T.
Date Acquired
January 2, 2001
Publication Date
January 2, 2001
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
carbon
dioxide
insulation
lightweight
Mars
thermal

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