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NASA NTRS ยท 20170004323

Thermal Insulation System for Non-Vacuum Applications Including a Multilayer Composite

Abstract

The thermal insulation system of the present invention is for non-vacuum applications and is specifically tailored to the ambient pressure environment with any level of humidity or moisture. The thermal insulation system includes a multilayered composite including i) at least one thermal insulation layer and at least one compressible barrier layer provided as alternating, successive layers, and ii) at least one reflective film provided on at least one surface of the thermal insulation layer and/or said compressible barrier layer. The different layers and materials and their combinations are designed to provide low effective thermal conductivity for the system by managing all modes of heat transfer. The thermal insulation system includes an optional outer casing surrounding the multilayered composite. The thermal insulation system is particularly suited for use in any sub-ambient temperature environment where moisture or its adverse effects are a concern. The thermal insulation system provides physical resilience against damaging mechanical effects including compression, flexure, impact, vibration, and thermal expansion/contraction.

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BibTeXRIS

Fesmire, James E.. 2017-04-11. Thermal Insulation System for Non-Vacuum Applications Including a Multilayer Composite. https://ntrs.nasa.gov/citations/20170004323

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