发明名称 TURBOJET SHELL FOR SET-UP OF THERMAL TARGETS
摘要 FIELD: military equipment, mainly associated with protection of objects, for example, of surface ships against shells with homing heads by oncoming formation of interference clouds. ^ SUBSTANCE: the shell has a turbojet engine, nose cone with a useful load and a fuse rigidly interconnected. The fuse is provided with an ignition system, and the nose cone-with mechanisms of destruction of its inner wall, protection of the useful load against stretches, ignition and ejection of the useful load, which contain successively installed charges of fuse cut-off, ignition and ejection of the useful load, which contain successively installed charges of fuse cut-off, ignition and ejection of the useful load. The shell is made for an axial spin. ^ EFFECT: reduced time of set-up of the cloud of thermal targets. ^ 5 cl, 1 dwg
申请公布号 RU2242703(C1) 申请公布日期 2004.12.20
申请号 RU20030106033 申请日期 2003.03.03
申请人 发明人 LANG V.F.;NASONOV A.N.;PETRJAKOV A.P.;SKUDARNOV A.JA.;JUROVSKIJ E.K.
分类号 F42B12/48 主分类号 F42B12/48
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