发明名称 METHOD FOR LOCATION OF ROCKET IN FLIGHT TRAJECTORY
摘要 FIELD: armament test. ^ SUBSTANCE: at the moment of bursting of the rocket warhead the mutual position of the injurious component of the rocket warhead in the section of the spatial field of their dispersion after blasting is registered and determined with the aid of an indicator of the position of injurious components, and then, according to the characteristics of the field of injury of the position indicator, the position of the injurious components of the warhead at the moment of bursting is determined on the thin-walled easily pierceable screen stationary installed in the spatial area of their dispersion between the underlying surface and the rocket, and connected to the underlying surface. ^ EFFECT: enhanced accuracy of rocket location relative to the underlying surface at the moment of bursting in any meteorological condition, simplified procedure of test, and reduced time of obtaining of information. ^ 3 dwg
申请公布号 RU2241202(C2) 申请公布日期 2004.11.27
申请号 RU20010122612 申请日期 2001.08.09
申请人 发明人 DUDKA V.D.;KUZNETSOV V.M.;FROLOV V.A.;KAPUSTIN A.S.;FERULENKOV A.V.;EHNTIN A.P.;MAKHONIN V.V.
分类号 F42B12/40;F42B8/14 主分类号 F42B12/40
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