Reusable thermal protection member for an object subject to grea

Stock material or miscellaneous articles – Sheet facing and longitudinally noncoextensive with web or...

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Details

244158A, 244117A, B64G 158

Patent

active

048045713

ABSTRACT:
The present invention relates to a reusable thermal protection member for an object subject to great heating, e.g. an aircraft or spacecraft.
The member comprises in per se known manner a refractory shield and an insulating layer between the refractory shield and the structure of the craft. According to the invention the refractory shield comprises at least one thin film of refractory material having an adequate flexibility to adapt to the shape of the structure of the craft in the area to be protected.
Application to the thermal protection of aircraft or spacecraft.

REFERENCES:
patent: 3878356 (1975-04-01), Royu
patent: 4124732 (1978-11-01), Leger
patent: 4151800 (1979-05-01), Dotts et al.
patent: 4344591 (1982-08-01), Jackson
patent: 4439968 (1984-04-01), Dunn
patent: 4456208 (1984-06-01), MacConochie et al.

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