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Way to launch a two-stage guided missiles with AIR CARRIER

机译:用航空母舰发射两阶段制导导弹的方法

摘要

a way to launch a two-tier u0443u043fu0440u0430u0432u043bu00a0u0435u043cu043eu0439 missiles from the air u043du043eu0441u0438u0442u0435u043bu00a0, including the launch of a rocket by the seed u0434u0432u0438u0433u0430u0442u0435u043bu00a0 of u043au043eu043du0442u0435u0439u043d freight limited era (tap) is placed on the launcher, the separation of the missile after u043eu043au043eu043du0447u0430u043du0438u00a0 of seed u0434u0432u0438u0433u0430u0442u0435u043bu00a0, ballistic flight starting stage, cb u0440u0430u0432u043bu00a0u0435u043cu044bu0439 flight u043cu0430u0440u0448u0435u0432u043eu0439 stage u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 orderthe office of a u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 since its withdrawal from the tap, the starting step carried out in the form of a perfect, aerodynamically stable u043eu043fu0435u0440u0435u043du043du043eu0433u043e body u0432u0440u0430u0449 u0435u043du0438u00a0, u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 after u0434u043eu0441u0442u0438u0436u0435u043du0438u00a0 missile flight speed and turn on the tap to launch missiles.pre calculated u0434u043bu00a0 specific regimes of flight u043du043eu0441u0438u0442u0435u043bu00a0 according to the nature of the u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 missile and aerodynamic characteristics of a missile and star sheet position, in which the set of possible trajectories u0432u0441u00a0 u043eu0442u0434u0435u043bu0438u0432u0448u0435u0439u0441u00a0 starting level is below the height of the flight u043du043eu0441u0438u0442u0435u043bu00a0.
机译:一种从空中发射两层 u0443 u043f u0440 u0430 u0432 u043b u00a0 u0435 u043c u043e u0439导弹的方法 u043d u043e u0441 u0438 u0442 u0432 u0435 u043b u0040 ,包括货运限制时代(tap)的种子 u0434 u0432 u0438 u0433 u0430 u0442 u0435 u043b u00b0放在发射器上之后, u043e u043a u043e u043d u0447 u0430 u043d u0438 u00a0种子 u0434 u0432 u0432 u0438 u0433 u0430 u0442 u0442 u0435 u043b u00b0弹道飞行开始阶段,cb u0440 u0430 u0432 u043b u00a0 u0435 u043c u044c u044b u0439航班 u043c u0430 u0440 u0448 u0435 u0432 u043e u0439阶段 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0订购 u043e u0441 u0443 u0449 u0435 u0441 u0442 u0432 u043b u00a0 u044e u0442的办公室,则以完美的,空气动力学稳定的 u043e u043f u0435 u0440 u0435 u043d u043d u04 3e u0433 u043e主体 u0432 u0440 u0430 u0449 u0435 u043d u0438 u00a0, u043f u0440 u043e u0438 u0437 u0432 u043e u043e u0434 u00a0 u0442在 u0442 u0438 u0436 u0435 u043d u0438 u00a0并打开水龙头以发射导弹。预先计算了 u0434 u043b u00a0的特定飞行情况 u043d u043e u0441 u0438 u0442 u0435 u043b u00a0根据 u0443 u043f u0440 u0430 u0432 u043b u0435 u043d u0438 u00a0的性质和导弹的空气动力学特性以及星表位置,在其中可能的轨迹集u0432 u0441 u00a0 u043e u0442 u0434 u0435 u043b u0438 u0432 u0448 u0435 u0439 u0441 u00a0起始高度低于飞行高度 u043d u043e u0441 u0438 u0442 u0435 u043b u00a0。

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