Shooting mode guided artillery rockets with homing on final flight path and DEVICE FOR IMPLEMENTATION

摘要

1.method of firing u0443u043fu0440u0430u0432u043bu00a0u0435u043cu044bu043c artillery rocket u0441u043du0430u0440u00a0u0434u043eu043c with u0441u0430u043cu043eu043du0430u0432u0435u0434u0435u043du0438u0435u043c after the flight path, including the exit from the barrel u043eu0440u0443u0434u0438 u0441u043du0430u0440u00a0u0434u0430 u00a0 and launch a rocket in the flight path of u0434u0432u0438u0433u0430u0442u0435u043bu00a0 u0441u043du0430u0440u00a0u0434u0430, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0441u043du0430u0440u00a0u0434 shoots on u043cu043eu0440u0442u0438u0440u043du043eu0439 trajectorya jet engine includes a u0432u043eu0441u0445u043eu0434u00a0u0449u0435u0439 or u043du0438u0441u0445u043eu0434u00a0u0449u0435u0439 u0432u0435u0442u0432u00a0u0445 flight path u0441u043du0430u0440u00a0u0434u0430 in shooting at the range u0441u043du0430u0440u00a0u0434u0430 with big or small of course.;2.u0443u043fu0440u0430u0432u043bu00a0u0435u043cu044bu0439 artillery rocket u0441u043du0430u0440u00a0u0434 with u0441u0430u043cu043eu043du0430u0432u0435u0434u0435u043du0438u0435u043c after the flight path of a jet engine with u043fu0438u0440u043eu0442u0435u0445u043du0438u0447u0435u0441u043au0438u043c u0432u043eu0441u043fu043bu0430u043c u0435u043du0438u0442u0435u043bu0435u043c, source u043fu0438u0442u0430u043du0438u00a0, electrically connected to the programmed before the start of the electronic equipment, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u044du043bu0435u043au0442u0440u043eu043du043du0430u00a0 equipment u0432u044bu043fu043e u043bu043du0435u043du0430 for timer functions u0434u0432u0438u0433u0430u0442u0435u043bu00a0 launch rocket.and u043fu0438u0440u043eu0442u0435u0445u043du0438u0447u0435u0441u043au0438u0439 igniter is equipped with u044du043bu0435u043au0442u0440u043eu0437u0430u043fu0430u043bu043eu043c, electrically connected to the electronic equipment.