Aeronautics and astronautics – Aircraft structure
Patent
1986-08-04
1988-04-26
Peters, Jr., Joseph F.
Aeronautics and astronautics
Aircraft structure
244158A, B64C 100
Patent
active
047399520
ABSTRACT:
An integral cooling system for high temperature missile structures which is essentially a passive cooling system integrated into the missile structure. An evaporative material carried in the missile structure is ejected by vapor pressure through openings in the missile's outer skin and cools the missile as it flows along the outer surface thereof.
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W. D. Allingham, "Vapor-Cooled Insulation for Thermal Protection of Hypersonic Glide Vehicles", ARS Journal, June 1962, pp 945-948.
Bush Freddie M.
Fiorito L. M.
Garvin, Jr. John C.
Peters Jr. Joseph F.
The United States of America as represented by the Secretary of
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