发明名称 Flight vehicle
摘要 A flight vehicle such as a guided weapon has a radiation emitter or receiver 3 carried behind a radiation transparent window 4 formed within an open recess 5 in a surface 2 of the weapon nose which diverges rearwardly from the vehicle axis, the recess being such that at supersonic speeds it forms shock waves which trap air within the recess to provide a measure of kinetic heat insulation for the window and also a minimum of supersonic drag. An elongate nose region 13 is provided ahead of the recess to house a further radiation emitter or receiver as an external wrapping 14 or an internal device 15.
申请公布号 GB2433305(A) 申请公布日期 2007.06.20
申请号 GB19810009256 申请日期 1981.03.26
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY;MATRA BAE DYNAMICS;MBDA UK LIMITED 发明人 STANLEY LEEK;HUGH ROEBUCK JOINER
分类号 F42B15/01;F42B15/34;F42C13/02 主分类号 F42B15/01
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