High temperature heat shield system

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

Patent

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Details

244117A, B64G 100

Patent

active

049251341

ABSTRACT:
A high temperature heat shield system for re-entry vehicles and high speed ircraft is assembled from separate insulating panels made of metal foil layers diffusion soldered together and with a ceramic fiber material filled into interspaces between the metal foil layers. In this arrangement structural metal foil layers carry mechanical loads while separate reflecting foil layers and the ceramic fiber material are non-load bearing.

REFERENCES:
patent: 1625061 (1927-04-01), Trout
patent: 2746892 (1956-05-01), Elfving
patent: 3009600 (1961-11-01), Matsch
patent: 4344591 (1982-08-01), Jackson
patent: 4456208 (1984-06-01), MacConochie et al.

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