FIELD: weapons and ammunition.
SUBSTANCE: in a nose fairing of a missile comprising a ceramic shell connected by elastic glue with a frame made of an adapter arranged from metal, matched by temperature coefficient of linear expansion with the shell material, and a titanium joint element connected to each other by pins and collars, sealing elements and a shell of heatproof material, installed with the gap relative to external surfaces of the ceramic shell and the joint element, the internal surface of the shell and the external surface of the shell are arranged as mirror ones.
EFFECT: reduced temperature of a frame compared to a prototype with the same border conditions on the external surface of the fairing.
1 dwg
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Authors
Dates
2012-08-20—Published
2010-12-08—Filed