HEAT RESISTANT RADOME FOR MISSILE

PURPOSE:To reduce temperature rise due to pneumatic heating of a radome body and to attain a high speed by so mounting a heat resistant structure as to cover the outer surface of a radome structure, and providing a separable clamping mechanism immediately before a missile is end-guided. CONSTITUTION...

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Bibliographic Details
Main Author OGURA EIJI
Format Patent
LanguageEnglish
Published 01.11.1990
Subjects
AMMUNITION
BLASTING
ELECTRIC COMMUNICATION TECHNIQUE
ELECTRICITY
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
HEATING
LIGHTING
MECHANICAL ENGINEERING
SELECTING
WEAPONS
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Summary:PURPOSE:To reduce temperature rise due to pneumatic heating of a radome body and to attain a high speed by so mounting a heat resistant structure as to cover the outer surface of a radome structure, and providing a separable clamping mechanism immediately before a missile is end-guided. CONSTITUTION:A heat resistant metal cover A6, a heat resistant metal cover B7 have structures for covering a radome 1, and a split shape. Heat insulating gaps 9 for holding heat insulation between the radome 1 and the cover A6, between the radome 1 and the cover B7 are provided. An igniter 14 is ignited immediately before a missile is introduced to the end induction, high pressure gas is filed in pressure gap 16, and a clamping cap 15 ls separated forward. Ths covers A6, B7 lost with clamping force are separately rotated by high pressure gas and blowing pneumatic pressure of the igniter 14. When it is rotated to a predetermined rotating angle, it is removed from a bearing 12 by means of the effect of the end shape of a shaft 11, pressed to be separated. Thereafter, the missile is launched.
Bibliography:Application Number: JP19890090050