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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|