Thermal control material

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

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Details

244117A, 244 1A, 427 38, B64G 158

Patent

active

044899068

ABSTRACT:
Spacecraft are subject to electron bombardment resulting in electrical charge build-up on dielectric materials, such as thermal blankets, used to control heat gain and loss from the craft. The invention provides a multiple-layer material including inner and outer thermally insulating layers and an intermediate conductive layer, the outer insulating layer having a thickness such that many of the bombarding electrons will come to rest at or near the conductive layer and the resulting charge conducted away. Material may be in the form of a blanket with e.g. Kapton inner and outer layers or in the form of a glass tile. Material is also usable in other situations where electrical charge build-up may be a problem, e.g. for insulating explosive liquid containers.

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Krusos, J. N. "Study of Ceramic Heat Shields for Lifting Reentry Vehicles", NASA Contractor (Bell Aerosystems Co.) Report NASACR-861.

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