CN103090745A - Guided missile with middle-section speed change and anti-intercept method thereof - Google Patents
Guided missile with middle-section speed change and anti-intercept method thereof Download PDFInfo
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- CN103090745A CN103090745A CN201310043273XA CN201310043273A CN103090745A CN 103090745 A CN103090745 A CN 103090745A CN 201310043273X A CN201310043273X A CN 201310043273XA CN 201310043273 A CN201310043273 A CN 201310043273A CN 103090745 A CN103090745 A CN 103090745A
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Abstract
The invention discloses a guided missile with middle-section speed change and an anti-intercept method of the guided missile, and relates to the technical field of guided missile anti-intercept. The guided missile comprises a third level guided missile warhead, a second level booster and a first level booster. A speed change anti-intercept system which is formed by 4-8 small rockets is arranged on a main body of the second level booster. Four speed change anti-intercept small guided missiles are arranged among the small rockets. The small rockets and the small guided missiles are evenly arranged around a cylinder body of the second level booster. The boosting direction of the small rockets is uniform with the direction of the third level guided missile warhead. The running direction of the small guided missiles after the small guided missiles are launched is opposite to the running direction of the third level guided missile warhead. A sudden anti-guided-missile system is installed on the third level guided missile warhead, the sudden anti-guided-missile system is formed by 4-15 small guided missiles, and the running direction of the small guided missiles is the same as the direction of the third level guided missile warhead. The guided missile with the middle-section speed change can effectively overcome the problem that the guided missile is intercepted easily after the first level drops and the second level (middle section) flies at a uniform speed. The guided missile is an anti-intercept missile with the middle-section speed change, and can effectively realize the anti-intercept function.
Description
Technical field
The present invention relates to the missile interception preventing technical field, particularly a kind of guided missile and interception preventing method with the stage casing speed change.
Background technology
Guided missile is a kind of weapon commonly used in modern war, and guided missile is after the first-stage boost device comes off, and fly with average rate in the second level (stage casing).Be also with rapid changepl. never-ending changes and improvements to the various Interception Technologies of guided missile at present, particularly guided missile when the stage casing average rate is flown, more easily suffers the interception from side, front, back.Along with improving constantly of missilery, be the important topic of scientists study to the anti-Interception Technology of guided missile itself always, although existing various anti-Interception Technologies now, general effect is not very desirable, and complex structure, manufacturing cost are high.
Summary of the invention
The invention provides a kind of guided missile with the stage casing speed change and interception preventing method, the invention solves guided missile when the stage casing average rate is flown, easily suffer the problem from the interception of side, front, back.
For addressing the above problem, the present invention adopts following technical scheme: a kind of guided missile with the stage casing speed change comprises third level guided missile warhead 3, second-stage boost 2 and first-stage boost device 1; The main body of second-stage boost 2 is provided with the anti-intercepting system 4 of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of 4 pieces of speed changes small missile 6 between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is consistent with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction;
A kind of missile interception preventing method with the stage casing speed change:
(1) described guided missile comprises third level guided missile warhead 3, second-stage boost 2 and first-stage boost device 1; The main body of second-stage boost 2 is provided with the anti-intercepting system 4 of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of 4 pieces of speed changes small missile 6 between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is consistent with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction;
(2) anti-interception step:
1) be arranged with that the anti-intercepting system of speed change that many pieces of mouses form and 4 pieces of small missiles form around second-stage boost in parallel.Mouse boosting direction is consistent with third level guided missile warhead direction simultaneously, and after 4 pieces of small missile emissions, traffic direction is opposite with third level guided missile warhead traffic direction;
2) have additional equally many pieces of small missiles around third level guided missile warhead, the emission traffic direction is consistent with third level guided missile warhead direction.The small missile that be arranged in parallel around third level guided missile warhead from the above mentioned is best for 4-12 piece.
The anti-interception of speed change is as follows with prominent anti-step:
1) direction and the speed of the satellite monitoring system of the radar installations by guided missile or ground control cabinet monitoring interception guided missile; When monitoring found that guided missile is subject to the side interception, guided missile fired mouse more than 2 pieces by received signal points, changes missile flight speed, avoids interception guided missile, makes and tackles unsuccessfully;
2) when monitoring finds that guided missile is subject to the front interception, guided missile once can be lighted third level guided missile warhead two pieces of small missiles on every side by receiving signal, shoots down the place ahead interception guided missile;
3) when monitoring finds that guided missile is subject to the back interception, guided missile by receive signal once can light in 4 pieces of small missiles on second-stage boost two pieces backward emission shoot down the tracking guided missile at rear;
4) in the prominent anti-process of guided missile, small missile when missiles ' terminal is attacked to target around (entering the backward target flight of atmosphere a to half-distance begins) third level guided missile warhead is regularly shot to target continuously, be third level guided missile warhead target of attack, clear the path, smash interception guided missile, as can the directtissima target making target be subject to wound without running into interception guided missile, inflict heavy losses on target for the third level guided missile warhead of back and create favorable conditions.
The present invention can effectively overcome guided missile after the first order comes off, the problem of easily being tackled when fly with average rate in the second level (stage casing).The present invention is the anti-interception guided missile of stage casing speed change, can effectively realize anti-interception, and simple in structure, cheap for manufacturing cost.
Description of drawings
Fig. 1 is overall structure schematic diagram of the present invention;
Fig. 2 is the anti-intercepting system structural representation of speed change of the present invention.
Fig. 3 is penetration missile system architecture schematic diagram of the present invention
Symbol description in figure: third level guided missile warhead 3, second-stage boost 2, first-stage boost device 1, the anti-intercepting system 4 of speed change; Penetration missile system 5; The anti-interception of speed change small missile 6.
The specific embodiment
The below is described in detail the present invention with best embodiment.
As Figure 1-3, a kind of guided missile with the stage casing speed change comprises third level guided missile warhead 3, second-stage boost 2 and first-stage boost device 1; The main body of second-stage boost 2 is provided with the anti-intercepting system 4 of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of 4 pieces of speed changes small missile 6 between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is parallel with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction;
A kind of missile interception preventing method with the stage casing speed change:
(1) described guided missile comprises third level guided missile warhead 3, second-stage boost 2 and first-stage boost device 1; The main body of second-stage boost 2 is provided with the anti-intercepting system 4 of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of 4 pieces of speed changes small missile 6 between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is consistent with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction;
(2) anti-interception step:
1) be arranged with that the anti-intercepting system of speed change that many pieces of mouses form and 4 pieces of small missiles form around second-stage boost in parallel.Mouse boosting direction is consistent with third level guided missile warhead direction simultaneously, and after 4 pieces of small missile emissions, traffic direction is opposite with third level guided missile warhead traffic direction;
2) have additional equally many pieces of small missiles around third level guided missile warhead, the emission traffic direction is consistent with third level guided missile warhead direction.The small missile that be arranged in parallel around third level guided missile warhead from the above mentioned is best for 4-12 piece.
The anti-interception of speed change is as follows with prominent anti-step:
1) direction and the speed of the satellite monitoring system of the radar installations by guided missile or ground control cabinet monitoring interception guided missile; When monitoring found that guided missile is subject to the side interception, guided missile fired mouse more than 2 pieces by received signal points, changes missile flight speed, avoids interception guided missile, makes and tackles unsuccessfully;
2) when monitoring finds that guided missile is subject to the front interception, guided missile once can be lighted third level guided missile warhead small missile more than two pieces on every side by receiving signal, shoots down the place ahead interception guided missile;
3) when monitoring finds that guided missile is subject to the back interception, guided missile by receive signal once can light in 4 pieces of small missiles on second-stage boost two pieces backward emission shoot down the tracking guided missile at rear;
4) in the prominent anti-process of guided missile, small missile when missiles ' terminal is attacked to target around (entering the backward target flight of atmosphere a to half-distance begins) third level guided missile warhead is regularly shot to target continuously, be third level guided missile warhead target of attack, clear the path, smash interception guided missile, as can the directtissima target making target be subject to wound without running into interception guided missile, inflict heavy losses on target for the third level guided missile warhead of back and create favorable conditions.
The present invention is after receiving the information that will be tackled that satellite and other communication equipment provide, can light pencil rocket according to intercept speed, change the flying speed of guided missile, the anti-intercepting system of speed change also can or come Remote to reach according to remote console by time and the rate request speed change of original setting, the guided missile of avoiding tackling.This kind changes the method for the flying speed of guided missile, can effectively realize the effect that is difficult to tackle, and simple in structure, and production cost is low, easily implements.
It should be noted that at last: obviously, above-described embodiment is only for example of the present invention clearly is described, and is not the restriction to embodiment.For those of ordinary skill in the field, can also make other changes in different forms on the basis of the above description.Here need not also can't give all embodiments exhaustive.And the apparent variation of being amplified out thus or change still are among protection scope of the present invention.
Claims (4)
1. the guided missile with the stage casing speed change, comprise third level guided missile warhead (3), second-stage boost (2) and first-stage boost device (1); It is characterized in that: the main body of second-stage boost (2) is provided with the anti-intercepting system (4) of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of (4) piece speed change small missile (6) between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is consistent with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction.
2. a kind of guided missile with the stage casing speed change as claimed in claim 1, it is characterized in that, penetration missile system (5) is installed on third level guided missile warhead (3), penetration missile system (5) is made of 4-12 piece of small missile, and small missile emission traffic direction is consistent with third level guided missile warhead direction.
3. missile interception preventing method with the stage casing speed change is characterized in that:
(1) described guided missile comprises third level guided missile warhead (3), second-stage boost (2) and first-stage boost device (1); The main body of second-stage boost (2) is provided with the anti-intercepting system (4) of the speed change that is comprised of 4-8 piece of mouse, be provided with the anti-interception of 4 pieces of speed changes small missile (6) between mouse, mouse and small missile evenly are arranged at the second-stage boost cylinder circumference, mouse boosting direction is consistent with third level guided missile warhead direction, and after the small missile emission, traffic direction is opposite with third level guided missile warhead traffic direction;
Penetration missile system (5) is installed on third level guided missile warhead (3), and penetration missile system (5) is made of 4-12 piece of small missile, and small missile emission traffic direction is consistent with third level guided missile warhead direction;
(2) anti-interception step:
1) be arranged with that the anti-intercepting system of speed change that many pieces of mouses form and 4 pieces of small missiles form around second-stage boost in parallel.Mouse boosting direction is consistent with third level guided missile warhead direction simultaneously, and after 4 pieces of small missile emissions, traffic direction is opposite with third level guided missile warhead traffic direction;
2) have additional equally many pieces of small missiles around third level guided missile warhead, the emission traffic direction is consistent with third level guided missile warhead direction.The small missile that be arranged in parallel around third level guided missile warhead from the above mentioned is best for 4-12 piece.
4. a kind of missile interception preventing method with the stage casing speed change as claimed in claim 3, it is characterized in that: the anti-interception of speed change is as follows with prominent anti-step:
1) direction and the speed of the satellite monitoring system of the radar installations by guided missile or ground control cabinet monitoring interception guided missile; When monitoring found that guided missile is subject to the side interception, guided missile was lighted mouse more than 2 pieces by the signal that receives, and changes missile flight speed, avoids interception guided missile, makes and tackles unsuccessfully;
2) when monitoring finds that guided missile is subject to the front interception, guided missile once can be lighted third level guided missile warhead two pieces of small missiles on every side by receiving signal, shoots down the place ahead interception guided missile;
3) when monitoring finds that guided missile is subject to the back interception, guided missile by receive signal once can light in 4 pieces of small missiles on second-stage boost two pieces backward emission shoot down the tracking guided missile at rear;
4) in the prominent anti-process of guided missile, small missile when third level guided missile warhead is attacked to target around (entering the backward target flight of atmosphere a to half-distance begins) third level guided missile warhead is regularly shot to target continuously, be third level guided missile warhead target of attack, clear the path, smash interception guided missile, as can the directtissima target making target be subject to wound without running into interception guided missile, inflict heavy losses on target for the third level guided missile warhead of back and create favorable conditions.
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105890470A (en) * | 2014-09-12 | 2016-08-24 | 王正铉 | An intercontinental missile capable of intercepting and attacking land-air-sea targets of enemies midway |
| CN110906795A (en) * | 2019-12-13 | 2020-03-24 | 陈忠响 | Middle section interception missile, system and method |
| EP4261490A1 (en) * | 2022-04-13 | 2023-10-18 | Diehl Defence GmbH & Co. KG | Method for migrating a missile in front of a interceptor missile |
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| CN1525135A (en) * | 2003-02-28 | 2004-09-01 | 王建钧 | Active guiding missile |
| US20060065150A1 (en) * | 2000-01-24 | 2006-03-30 | Metal Storm Limited | Anti-missile missiles |
| CN101055164A (en) * | 2000-12-09 | 2007-10-17 | 施仲伟 | Rocket propulsion enhancing design |
| CN102661685A (en) * | 2012-04-17 | 2012-09-12 | 张景军 | Interception preventing missile |
| CN203203482U (en) * | 2013-02-05 | 2013-09-18 | 朱旭望 | Guided missile with variable-speed middle section |
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2013
- 2013-02-05 CN CN201310043273XA patent/CN103090745A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US20060065150A1 (en) * | 2000-01-24 | 2006-03-30 | Metal Storm Limited | Anti-missile missiles |
| CN1430720A (en) * | 2000-05-25 | 2003-07-16 | 斯托姆金属有限公司 | Directional control of missiles |
| CN101055164A (en) * | 2000-12-09 | 2007-10-17 | 施仲伟 | Rocket propulsion enhancing design |
| CN1525135A (en) * | 2003-02-28 | 2004-09-01 | 王建钧 | Active guiding missile |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105890470A (en) * | 2014-09-12 | 2016-08-24 | 王正铉 | An intercontinental missile capable of intercepting and attacking land-air-sea targets of enemies midway |
| CN110906795A (en) * | 2019-12-13 | 2020-03-24 | 陈忠响 | Middle section interception missile, system and method |
| CN110906795B (en) * | 2019-12-13 | 2022-07-05 | 谢勋 | Middle section interception missile, system and method |
| EP4261490A1 (en) * | 2022-04-13 | 2023-10-18 | Diehl Defence GmbH & Co. KG | Method for migrating a missile in front of a interceptor missile |
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Application publication date: 20130508 |