NASA NTRS · 19690000568
Design of multilayer insulation systems
Abstract
Analytical 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.
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Cunnington, G. R., Jr., Stread, E. R.. 1969-11-01. Design of multilayer insulation systems. https://ntrs.nasa.gov/citations/19690000568
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