CN103712524A - Combined type air-defense equipment - Google Patents

Combined type air-defense equipment Download PDF

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Publication number
CN103712524A
CN103712524A CN201310743312.7A CN201310743312A CN103712524A CN 103712524 A CN103712524 A CN 103712524A CN 201310743312 A CN201310743312 A CN 201310743312A CN 103712524 A CN103712524 A CN 103712524A
Authority
CN
China
Prior art keywords
fuse
defense equipment
low coverage
flyer
guided missile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201310743312.7A
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Chinese (zh)
Inventor
杨贻方
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd
Original Assignee
Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd filed Critical Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd
Priority to CN201310743312.7A priority Critical patent/CN103712524A/en
Publication of CN103712524A publication Critical patent/CN103712524A/en
Pending legal-status Critical Current

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Abstract

The invention provides combined type air-defense equipment. The equipment is characterized in that a container is divided into two segments, one segment is divided into 6*10 small cells, a short-distance fuse guided missile driven by a rocket and a punching engine is perpendicularly arranged in each cell, three folding wing small-scale helicopters are arranged in the other segment, an ultra-clear camera shooting processor and a Beidou signal processor are arranged on each helicopter, in the process of running, when the helicopters fly to the 15km high altitude, the helicopters conduct image scanning on the area with the width of 15km and the length of 100km, and conduct comparison on images according to the scanning frequency of 10-20 times per second, the difference is rapidly analyzed from the images, a flying object which moves at the speed of 100-2000m/s is judged, the flying three-dimensional area of the flying object is calculated according to the interception time, the short-distance fuse guided missiles are guided to be launched and enter the area in advance to conduct backward flying, the flying object is impacted and detonated to be blown up in a short-distance mode, therefore, a low-altitude target can be exposed out, effect intercepting can be achieved, and the equipment is used for intercepting cruise missiles, low-altitude penetration planes and the like.

Description

Combined air defense
Affiliated technical field
The present invention relates to a kind of emptying device, a kind of especially combined air defense equipment.
Background technology
Cruise missile and aircraft can utilize landform low-level penetration at present.Cruise missile has multiple advantage:
First, its volume is little, lightweight, is convenient to various platforms and carries.Naval's nuclear powered attack submarines can vertically carry 12 pieces, and can approach the coastal transmitting of enemy, thereby can hit the important military-political targets of 1300~2500 kilometers of its depths.The general every warship of surface ship can be taken 8~32 pieces, adopts after MK-41 launching tower, and a warship can be taken more than 100 pieces, because it can be at water surface Mobile launch, so be difficult for being detected.The amount of carrying of bomber is increasing, and B-52G can bring up to 20 pieces by 12 pieces after improving, and B-1B can take 30 pieces, and the DC-10 after repacking can take 50~60 pieces, and " Boeing-747 " after repacking can be taken 70~90 pieces.Ground-launched " battleax " guided missile is contained on motor-driven transportation-perpendicular-emission-type car, and each vehicle-mounted 4 pieces, 4 chassis Wei Yige batteries, can launch 16 pieces of guided missiles.The heavy equipment of missile firing battery can be by transporter air transports such as C-130 or C-5 to forward position or launching site.
Secondly, its far firing range, flying height is low, attacks sudden large.Tomahawk cruise missile range reaches 2500 kilometers farthest, and the shortest is 450 kilometers, all at enemy's fire net, launch outward, so flat pad is difficult to be found by the other side.Guided missile is 7~15 meters of sea flying heights, smooth land is below 50 meters, mountain area and hilly country are below 100 meters, substantially be continuous change of flight height with the fluctuating of landform, and this is highly all within the other side radar shadown, so be also difficult to the other side's discovery, very easily cause the emergentness of attack.In addition, guided missile is taked after effective stealthy measure, and its radar area is only 0.02~0.1 square metre, is equivalent to the albedo of a little sea-gull.A new generation's cruise missile only has an aiming pip of needle point size on radar screen, and visible being difficult to surveyed.
The 3rd, its accuracy at target is high, and lethality is strong.The cruise missile that range is 2500~3000 kilometers, hits error and is not more than 60 meters, and what precision was good reaches 10~30 meters, substantially has the ability of getting shape hard goal ready.The cruise missile of taking conventional warhead can destroy firm ground target, also can kill and wound and destroy area target with shrapnel.Take the cruise missile of 200,000 TNT equivalent nuclear warheads because accuracy at target is high, general higher 3~4 times than the fighting efficiency of ballistic missile.Cruise missile is because the flight time is long, and speed is low, and flying height is again just within small arms fire net, so subject to very much the volley of the non-guidance conventional Weapons such as bullet, in the Gulf War, having 3 pieces of " battleax " guided missiles is exactly by Iraq, to be smashed like this.
Circulation guided missile has Mobile launch like this, the strong advantage of survival ability.Cruise missile volume is little, lightweight, plays Ji collapsible, is convenient to various motor platforms (ground sea base and space base) transmitting, thereby has improved mobility and the survival ability of armament systems.Target property is not obvious, and penetration ability is strong.Cruise missile transmitting time has certain wake flame infra-red radiation, but in low latitude and the time very short, be difficult to carry out transmitter section detection.At cruise section, it is with subsonic flight, and Aerodynamic Heating is not serious, so infrared signature is not obvious.Because size is little and carried out stealthy processing, make radar scattering characteristic also not obvious again.In addition it carries out flight altitude control, utilizes terrain and its features to carry out hidden flight, thereby implement cruise section interception, also will be very difficult.Adopt combination (compound) aiming means, trajectory is unfixing.Cruise missile adopts the combined guidance modes such as inertial navigation, terrain contour matching guidance, GPS guidance and image matching guidance conventionally.Accuracy at target reaches 10-30m, thereby can attack selectively the target of high value.And can realize hidden flight, the flight of detouring, effectively target of attack.Flying speed is slow.Cruise missile is with subsonic flight, if supposition latter end 10km just finds cruise missile, implementing Terminal Phase Intercept also had three, 40 seconds.
General so anti-ballistic air defence system just cannot effectively be tackled.
summary of the invention
For the problems referred to above, the object of the present invention is to provide a kind of air defense equipment of effective interception.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of combined air defense equipment, it is characterized in that container lattice to become two sections, one section is divided into 6 * 10 little lattice, every lattice vertically pack one piece of low coverage fuse guided missile being driven by rocket and punching engine into, another section packs 3 small-sized helicopters of flap into, on each helicopter, be provided with super clear shooting processor and Big Dipper signal processor, during operation, helicopter flies to 15km high-altitude, picture scanning is carried out in the region of the wide long 100km of 15km, scan frequency contrast picture according to 10-20 time per second, therefrom express analysis goes out difference, judge the flyer that 100~2000 meter per seconds move, and calculate according to commit time the 3D region that this flyer of guided missile flies, guiding low coverage fuse MISSILE LAUNCHING enters the reverse flight in region in advance, clash into and low coverage ignition demolition flyer.
Beneficial effect of the present invention is: according to adopting high-altitude to overlook contrast picture, low target can be come out, effectively tackle.
The specific embodiment
In concrete enforcement, there is a lot of enforcement and optimize details:
Prioritization scheme one, low coverage fuse guided missile with 2-6 times of velocity of sound and 15~45 degree underriding angles to the reverse flight of flyer, tackle.
Prioritization scheme two, the bullet of low coverage fuse guided missile includes 3-15 kilogram of high explosive.
Prioritization scheme three arranges 2 groups and effectively defends in the wide region of war of every 100km, and sets up second guard wire, and interception firing order is by referring to war confirmation.
Combined air defense equipment of the present invention, can be for interception cruise missile, low-level penetrator.

Claims (4)

1. a combined air defense equipment, it is characterized in that container lattice to become two sections, one section is divided into 6 * 10 little lattice, every lattice vertically pack one piece of low coverage fuse guided missile being driven by rocket and punching engine into, another section packs 3 small-sized helicopters of flap into, on each helicopter, be provided with super clear shooting processor and Big Dipper signal processor, during operation, helicopter flies to 15km high-altitude, picture scanning is carried out in the region of the wide long 100km of 15km, scan frequency contrast picture according to 10-20 time per second, therefrom express analysis goes out difference, judge the flyer that 100~2000 meter per seconds move, and calculate according to commit time the 3D region that this flyer of guided missile flies, guiding low coverage fuse MISSILE LAUNCHING enters the reverse flight in region in advance, clash into and low coverage ignition demolition flyer.
2. combined air defense equipment according to claim 1, it is characterized in that low coverage fuse guided missile with the underriding angles of 2-6 times of velocity of sound and 15~45 degree to the reverse flight of flyer, tackle.
3. combined air defense equipment according to claim 1, is characterized in that the bullet of low coverage fuse guided missile includes 3-15 kilogram of high explosive.
4. combined air defense equipment according to claim 1, is characterized in that in the wide region of war of every 100km, arranging 2 groups effectively defends, and sets up second guard wire, and interception firing order is by referring to war confirmation.
CN201310743312.7A 2013-12-30 2013-12-30 Combined type air-defense equipment Pending CN103712524A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310743312.7A CN103712524A (en) 2013-12-30 2013-12-30 Combined type air-defense equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310743312.7A CN103712524A (en) 2013-12-30 2013-12-30 Combined type air-defense equipment

Publications (1)

Publication Number Publication Date
CN103712524A true CN103712524A (en) 2014-04-09

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310743312.7A Pending CN103712524A (en) 2013-12-30 2013-12-30 Combined type air-defense equipment

Country Status (1)

Country Link
CN (1) CN103712524A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105466286A (en) * 2014-09-28 2016-04-06 周妍 All-movable medium-range and short-range missile launching box
CN112461059A (en) * 2020-10-30 2021-03-09 彩虹无人机科技有限公司 Image-seeking guided missile ground launching method
CN113959269A (en) * 2021-11-17 2022-01-21 航天科工微电子***研究院有限公司 Grid empennage kinetic energy interceptor for intensive formation

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105466286A (en) * 2014-09-28 2016-04-06 周妍 All-movable medium-range and short-range missile launching box
CN112461059A (en) * 2020-10-30 2021-03-09 彩虹无人机科技有限公司 Image-seeking guided missile ground launching method
CN113959269A (en) * 2021-11-17 2022-01-21 航天科工微电子***研究院有限公司 Grid empennage kinetic energy interceptor for intensive formation

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Application publication date: 20140409