Multiwall thermal protection system

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

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Details

244132, 428594, 428604, 428607, 428608, B64C 158

Patent

active

043445918

ABSTRACT:
Multiwall insulating sandwich panels are provided for thermal protection of hypervelocity vehicles and other enclosures. In one embodiment of the invention the multiwall panels are formed of alternate layers of dimpled and flat metal (titanium alloy) foil sheets and beaded scarfed edge seals to provide enclosure thermal protection up to 1000.degree. F. An additional embodiment employs an intermediate fibrous insulation for the sandwich panel to provide thermal protection up to 2000.degree. F. and a third embodiment employs a silicide coated columbium waffle as the outer panel skin and fibrous layered intermediate protection for thermal environment protection up to 2500.degree. F.
The use of multiple panels of the present invention on an enclosure facilitate repair and refurbishment of the thermal protection system due to the simple support provided by the tab and clip attachment for the panels.

REFERENCES:
patent: 2945653 (1960-07-01), Atkin
patent: 3236476 (1966-02-01), White
patent: 3243313 (1966-03-01), Aves
patent: 3270908 (1966-09-01), Faget
patent: 3395035 (1968-07-01), Strauss
patent: 3490718 (1970-01-01), Vary
patent: 3799056 (1974-03-01), Colignon
patent: 4071194 (1978-01-01), Eckert
patent: 4151800 (1979-05-01), Dotts
patent: 4161567 (1979-07-01), Sturgeon
patent: 4161567 (1964-10-01), Jackson
patent: 4164339 (1979-08-01), McClenny
"R" reference, pp. 28-29, 38-39, 40-41.
Niblock and Reeder, Four Space Shuttle Wing Leading Edge Concepts, 11 J. Spacecraft 314-20 (No. 5, May 1974).
Levy, Locke & Leggett, Composite Ceramic-Metal Systems,Astronautics (Apr. 1961), pp. 27-29.

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