CN101554923A - Airplane missile defense system - Google Patents
Airplane missile defense system Download PDFInfo
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- CN101554923A CN101554923A CNA2008101626021A CN200810162602A CN101554923A CN 101554923 A CN101554923 A CN 101554923A CN A2008101626021 A CNA2008101626021 A CN A2008101626021A CN 200810162602 A CN200810162602 A CN 200810162602A CN 101554923 A CN101554923 A CN 101554923A
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- missile
- airplane
- guided missile
- defense system
- gun
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Abstract
The invention relates to an airplane missile defense system for smashing missiles or enemy planes striking at the rear part of an airplane. The airplane missile defense system comprises a rear view radar, a special backward aerogun and a special missile. The rear view radar is used for observing, targeting an object at the rear of the airplane and directing the missile. Radar guidance is unnecessary if infrared guidance is used for a homing missile. The aerogun is used for launching the missile in a pipe, solving zero-crossing velocity when the missile is launched backwards; causing the missile to complete the process of zero-crossing velocity in a gun bore to travel forward after the missile is out of the gun bore, and ensuring the stability of missile flight. The rear part of the missile is made into a gun shell form so as to be suitable for aerogun launch. When the airplane is chased by the enemy plane or stricken by the missile, the distance is so near that a short-distance micro-missile can be adopted, thus solving the problem that the existing air-to-air missile can not be launched backwards, greatly lowering the technical difficulty of over-the-shoulder launch and improving airplane survivability in wars.
Description
Technical field
The present invention is a kind of can adopting an effective measure when aircraft suffers that guided missile or enemy plane are attacked, and smashes and attacks guided missile or enemy plane, guarantees inherently safe, improves the airplane missile defense system of aircraft survivability.After this system of aircraft equipment, can increase substantially battlefield survival, capture the battlefield mastery of the air, thereby capture the final victory of war.
Background technology
As everyone knows, modern war is no matter still carry out on the ocean on land, and mastery of the air is to obtain the key factor of war victory.And denial of the air will test the attack how aircraft is defeated enemy plane and how to be prevented air defence missile in air battle.Just can my army's aircraft accusing each other with enemy plane and opposing under the strike of air defence missile and survive.At present, along with improving constantly of aeroplane performance, the method that gun and antiaircraft gun hit aircraft lost efficacy substantially, and hitting aircraft with guided missile is current basic means, guided missile is in the process of hitting aircraft, and final stage adopts active radar target seeker or the autonomous target of attack of infrared seeker substantially.Because air speed is fast, guided missile one launch plane has changed original position, and therefore, guided missile all is to pursue and attack at the aircraft rear.In case the aircraft rear is suffered to attack and can only be broken away from by speed and motor-driven, and is not only very passive, and the success ratio of breaking away from is very little.If directly target enforcement is rearward attacked, destroy the target of coming to attack, the viability of aircraft will improve greatly.
The fire control attack pattern of target is called shoulder emission more behind the aircraft attack tail, and takeing on emission more is exactly a kind of new attack mode, and promptly this machine utilizes the airborne fire control system control machine to carry air-to-air missile and attacks the enemy plane of this machine in hot pursuit or the attack pattern of guided missile.The shoulder emission is that guided missile is launched forward more, aloft turn, and the target of going to attack the rear then, because when preceding penetrating, guided missile has been crossed this machine wing this " shoulder ".Russia, the U.S. and China are all in research at present.The afterbody of Muscovite Soviet Union-35 aircraft has a very big tail cone, and the inside is equipped with small-sized backsight radar, can attack backward by navigate missile.Except that Muscovite Soviet Union-35 can accomplish to launch a guided missile backward, the ability that other aircrafts are not all launched a guided missile backward.As if the retroeflection research of long distance bullet is mainly done by the U.S. and China, but all do not have what breakthrough.
The guided missile of penetrating ability after having is middle apart from the combined guidance air-to-air missile, this guided missile both can as middle the same apart from the combined guidance air-to-air missile, the fwd target is attacked in the flight that goes ahead, can penetrate the target of attacking the rear again in the past, because this specific character makes this bullet need adopt three sections guidances, just section is a program segment; The stage casing is an instruction+inertial navigation section; Latter end is a powered-flight phase.Just the section guided missile is by predetermined instruction flight; The stage casing guided missile receives the instruction of carrier aircraft, changes to finish " shoulder more "; The latter end guided missile adopts active radar target seeker or infrared seeker, autonomous target of attack, and carrier aircraft can break away from this moment fully.
Concerning fire control system, before MISSILE LAUNCHING, be required to be its bookbinding data, and carry out the inertial navigation butt joint; The first period of guided missile is very short, and fire control system and guided missile do not have interconnection of signals; Before the midcourse guidance penetrated be difficulty the most, thereby to handle carrier aircraft, make the forward direction radar-tracked missile so that for it transmits target information, help it to finish " shoulder more ", if this missile attack is failed, also be unfavorable for the existence of carrier aircraft.Simultaneously the information of the detection of a target is also taken into account to target detector in the back, so that lose objects not.
The guided missile of penetrating ability after having generally is the infrared close combat air to air missile of low coverage with thrust vectoring control, this guided missile both can as the low coverage infra-red missile the same, bullet is placed forward on launcher, launch the target of going to attack the place ahead forward, can also on launcher, place forward by bullet, launcher changes 180 ° and launches the target (need to adopt the thrust vectoring control technology, this bullet is when the speed zero passage, and its lift is provided by thrust vectoring) of going to attack the rear backward.The infra-red missile that similar emission is general is such, and after the MISSILE LAUNCHING, carrier aircraft can break away from.This specific character requires very high to launcher, equipment and system's control are quite complicated, and operation easier is bigger.
The difficult point of the maximum of penetrating after the realization be after penetrate in the process, guided missile has speed to diminish gradually earlier, zero passage becomes big process more gradually, is called for short speed zero passage process.In this process, the lift of guided missile diminishes earlier gradually, becomes big more gradually, and guided missile just must fall after emission like this, thereby may produce harmful effect to the attack of guided missile.And the more important thing is, the balance of general guided missile is handled by rudder face, in speed zero passage process, power and moment that the guided missile rudder face is handled also have an elder generation to diminish gradually, become big process more gradually, like this, guided missile will be unstable, if the carrier aircraft flow field is to the influence of guided missile when considering MISSILE LAUNCHING, guided missile has been controlled with regard to more difficult.So traditional guided missile is penetrated after can not or being difficult to carry out, the guided missile of penetrating ability after having must have the thrust vectoring control ability, simultaneously in order to make the very fast past of speed zero passage process, also needs to install booster rocket additional to guided missile.This shows that the guided missile of penetrating ability after having is very big with now general guided missile difference, increased guided missile cost and carrier aircraft load greatly.After penetrate except with preceding penetrate the same the needs the backsight radar sensor, also need to rotate launcher and accessory equipment thereof, so higher to the carrier aircraft requirements on hardware equipment.
In sum, at present in the world except that Muscovite Soviet Union-35 can accomplish to launch a guided missile backward, the ability that other aircrafts are not all launched a guided missile backward.And-35 employed R-73 of Russia Soviet Union are a kind of emission forms of takeing on more, can't accomplish directly to launch backward.Guided missile will be launched more shoulder forward and turns again backward, the technical requirements height, and difficulty is big, and the reaction time is long, operating difficulties, and also cost height, carrier aircraft load are greatly.Therefore, people expect to occur the airplane missile defense system that a kind of cost is low, in light weight, simple to operate, shoot straight, and with raising battlefield survival rate, even create a kind of aircraft that can't shoot down, and capture the battlefield mastery of the air.
Summary of the invention
The present invention will utilize prior art to set up a kind of brand new airplane missile defense system.When aircraft runs into missile attack or enemy plane and pursues and attacks, directly launch a guided missile backward, destroy enemy missile or enemy plane, increase substantially the opportunity of combat viability, capture the battlefield mastery of the air.
Airplane missile defense system of the present invention is characterized in that: it comprises a backsight radar, behind the purpose made to gun and guided missile.The backsight radar is target, the navigate missile that is used for finding, locking the aircraft rear.Its effect is with existing the same with forward-looking radar.Because long-range and over the horizon is attacked and is served as by forward-looking radar and commander's machine, thus with short-range micro radar escapable cost, alleviate carrier aircraft and load, as use the infrared guidance homing missile, then can be without radar guidance.The effect of gun is to make guided missile emission in pipe, solves guided missile and launches speed per hour backward and spend zero problem, makes guided missile finish speed zero passage process in bore, promptly flies forward after going out thorax, guarantees the stability of missile flight.Boattail is made the shell form, to adapt to the gun emission.When aircraft suffer that enemy plane catches up with or during missile attack distance all very near, guided missile can adopt the short range micro missile.
Beneficial effect of the present invention: airplane missile defense system of the present invention is an airplane missile defense system of being built by prior art, can improve the opportunity of combat survival rate, captures the battlefield mastery of the air.Launch a guided missile to compare with existing shoulder more and have the following advantages: 1. volume is little, in light weight.Native system only needs short range radar and micro missile, can do volume very for a short time, can significantly alleviate the carrier aircraft load, strengthens the manoevreability of aircraft.2. cost is low.Native system all is a prior art, only need carry out the small number of devices repacking, and existing weaponry and equipment is reequiped a little and can be used, so the technological development cost is extremely low.3. simple to operate.Because the shoulder emission needs to adopt three sections guidances more, just section is a program segment; The stage casing is an instruction+inertial navigation section; Latter end is a powered-flight phase.Just the section guided missile is by predetermined instruction flight; The stage casing guided missile receives the instruction of carrier aircraft, changes to finish " shoulder more "; The latter end guided missile adopts active radar target seeker or infrared seeker, autonomous target of attack.This system can accomplish " no matter emission back " fully, operates very simple.4. speed of response is fast.This system obtains the information of target by the back to target detector, boosted missile launch area when target enters after, and when penetrating launching condition after satisfying, guided missile is promptly prepared emission, do not need into to get over the shoulder process, be directly to launch backward, so speed of response is fast.5. shoot straight.Back boosted missile is not only aimed at and is attacked directly emission backward of guided missile, and guided missile goes out to play the effect that discharges jamming bomb behind the thorax simultaneously, and making both sides' guided missile is target with the other side mutually, and the junction requirement that has wing-rooms on either side of a one-story house to prefer can significantly improve the hit rate of guided missile.
Description of drawings
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The specific embodiment
Airplane missile defense system of the present invention.Be to adorn a backsight radar at the aircraft rear portion, behind the purpose made to gun.The backsight radar is target, the navigate missile that is used for finding, locking the aircraft rear.As use the infrared guidance homing missile, then can be without radar guidance, no matter adopt the method for emission back.The effect of the gun in the present embodiment is to make guided missile emission in pipe, and the speed zero passage problem when solving guided missile and launching backward makes guided missile finish speed zero passage process in bore, promptly flies forward after going out thorax, guarantees the stability of missile flight.Boattail in the present embodiment is made the shell form, to adapt to the gun emission.Because of aircraft suffer that enemy plane catches up with or during missile attack distance all very near, guided missile can adopt the short range micro missile.Can not launch problem backward thereby solved existing air-to-air missile, reduce the technical risk of shoulder emission more greatly, improve the viability of aircraft in war.
Claims (4)
1, a kind of airplane missile defense system is characterized in that: it comprises a backsight radar, a gun of launching backward, and bullet shells is a kind of guided missile.
2, airplane missile defense system according to claim 1 is characterized in that: said backsight radar is target, the navigate missile that is used for observing, locking the aircraft rear.
3, airplane missile defense system according to claim 1, it is characterized in that: the said gun of emission backward is to be used for launching a guided missile, make guided missile emission in pipe, speed zero passage problem when the solution guided missile is launched backward, make guided missile in bore, finish speed zero passage process, promptly fly forward after going out thorax, guarantee the stability of missile flight.
4, airplane missile defense system according to claim 1 is characterized in that: said bullet shells is a kind of guided missile, and boattail is made the shell form, to adapt to the gun emission.When aircraft suffer that enemy plane catches up with or during missile attack distance all very near, guided missile can adopt the short range micro missile.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101626021A CN101554923A (en) | 2008-12-04 | 2008-12-04 | Airplane missile defense system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2008101626021A CN101554923A (en) | 2008-12-04 | 2008-12-04 | Airplane missile defense system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101554923A true CN101554923A (en) | 2009-10-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2008101626021A Pending CN101554923A (en) | 2008-12-04 | 2008-12-04 | Airplane missile defense system |
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| CN (1) | CN101554923A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104667539A (en) * | 2015-02-21 | 2015-06-03 | 佛山市三水区希望火炬教育科技有限公司 | Special aircraft capable of lunching aluminum paper to replace jamming bomb for teenager national defense scientific literacy education and training |
| CN105217037A (en) * | 2015-10-08 | 2016-01-06 | 山东中泰新能源集团有限公司 | A kind of fighter plane of 360 ° of transmitting cruise missiles |
| CN105318792A (en) * | 2014-08-01 | 2016-02-10 | 王正铉 | Device for launching guided missile reversed with flight path of aircraft to conduct offence and defense |
| CN105740136A (en) * | 2014-12-09 | 2016-07-06 | 上海新跃仪表厂 | Infrared seeker flight program testing assessment method |
| CN107943075A (en) * | 2017-11-22 | 2018-04-20 | 何振平 | It is a kind of that the method that yawing breaks away from attack is penetrated using big gun |
| CN112124595A (en) * | 2020-08-27 | 2020-12-25 | 彩虹无人机科技有限公司 | Locking device for unmanned aerial vehicle launching device |
-
2008
- 2008-12-04 CN CNA2008101626021A patent/CN101554923A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105318792A (en) * | 2014-08-01 | 2016-02-10 | 王正铉 | Device for launching guided missile reversed with flight path of aircraft to conduct offence and defense |
| CN105740136A (en) * | 2014-12-09 | 2016-07-06 | 上海新跃仪表厂 | Infrared seeker flight program testing assessment method |
| CN105740136B (en) * | 2014-12-09 | 2018-07-20 | 上海新跃仪表厂 | A kind of method of infrared seeker mission program test assessment |
| CN104667539A (en) * | 2015-02-21 | 2015-06-03 | 佛山市三水区希望火炬教育科技有限公司 | Special aircraft capable of lunching aluminum paper to replace jamming bomb for teenager national defense scientific literacy education and training |
| CN105217037A (en) * | 2015-10-08 | 2016-01-06 | 山东中泰新能源集团有限公司 | A kind of fighter plane of 360 ° of transmitting cruise missiles |
| CN107943075A (en) * | 2017-11-22 | 2018-04-20 | 何振平 | It is a kind of that the method that yawing breaks away from attack is penetrated using big gun |
| CN112124595A (en) * | 2020-08-27 | 2020-12-25 | 彩虹无人机科技有限公司 | Locking device for unmanned aerial vehicle launching device |
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Open date: 20091014 |