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Ballistic missile mid-course interception method and system

A ballistic missile and interception system technology, applied in defensive devices, offensive equipment, etc., can solve problems such as national security threats and real warhead attacks, and achieve the effect of protecting homeland security

Inactive Publication Date: 2019-01-04
BEIJING LANDSPACETECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In addition, when the payload is multiple warheads, it is almost impossible to intercept all missile warheads by the traditional impact interception method, so a large number of real warheads will attack the defender's homeland, which has caused serious damage to the national security of the attacked party. serious threat

Method used

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  • Ballistic missile mid-course interception method and system

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Embodiment Construction

[0030] The technical scheme of the present invention will be further described below in conjunction with the accompanying drawings and through specific embodiments. Spatially relative terms such as "below", "beneath", "under", "lower", "above", "on", "higher", etc. are used for convenience of description to explain the relative position of an element relative to the The orientation of two elements means that these terms are intended to encompass different orientations of the device in addition to orientations other than those shown in the figures. In addition, for example, "one element is on / under another element" may mean that two elements are in direct contact, or that there are other elements between the two elements. In addition, terms such as "first", "second", etc. are also used to describe various elements, regions, sections, etc. and should not be taken as limitations. Similar terms refer to similar elements throughout the description.

[0031]In describing the proce...

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Abstract

The invention provides a ballistic missile mid-course interception method and system. The method comprises the steps that the flying trajectory and the flying speed of an incoming missile are detected; according to the flying speed and the flying trajectory, the preset launching time and the preset flying trajectory of an interrupter are calculated; the interrupter carries shrapnel; the interrupter is launched at the preset launching time and flies along the preset flying trajectory so as to enter an ammunition placing area for the incoming missile in first time; and the interrupter throws shrapnel to the incoming missile in the ammunition placing area, and therefore the shrapnel is exploded in the interruption area to destroy the incoming missile. By means of the method, since shrapnel isarranged nearby the flying trajectory of the incoming missile, various suspicious targets existing during mid-course flying of the trajectory missile can be removed in a large range, and therefore the country under attack is protected against threat of the load carried by the trajectory missile.

Description

technical field [0001] The invention relates to the technical field of missile defense, in particular to a method and system for mid-stage interception of ballistic missiles. Background technique [0002] With the rapid development of missile weapon technology, it has gradually become the core weapon in modern warfare. It can be said that missile weapons are the epitome of a country's military strength. As an important component of the missile family, ballistic missiles are key vehicles for delivering payloads. In order to ensure that ballistic missiles can reach the attacked country, ballistic missiles usually have a certain penetration capability, which is also an important indicator of whether ballistic missiles can survive. [0003] For the defensive side, in order to avoid devastating attacks such as nuclear weapons on the homeland, it is necessary to effectively intercept the ballistic missiles of the attacking side. At present, military powers such as the United St...

Claims

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Application Information

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IPC IPC(8): F41H11/02
CPCF41H11/02
Inventor 张春林陈志愿宋晓伟戴政刘媛媛刘亮李谊红葛明和康永来
Owner BEIJING LANDSPACETECH CO LTD
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