CN102087083A - Rope course type short-range missile intercepting device - Google Patents
Rope course type short-range missile intercepting device Download PDFInfo
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- CN102087083A CN102087083A CN2009101866119A CN200910186611A CN102087083A CN 102087083 A CN102087083 A CN 102087083A CN 2009101866119 A CN2009101866119 A CN 2009101866119A CN 200910186611 A CN200910186611 A CN 200910186611A CN 102087083 A CN102087083 A CN 102087083A
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Abstract
The invention discloses a rope course type short-range missile intercepting device. The device consists of a folded square net (1), rockets (2), canister launchers (3) and a net storage case (4). When the device is used, the four rockets are launched synchronously, drag a rope course at an external field angle and fly relative to an attacking missile; when the net is completely unfolded, the external field angle is corrected, and parallel flight is performed; when the net collides with the object, under the opposite dragging action of the object, the net pulls the rockets to approach to and collide with the object, and a warhead controlled by a proximity fuse is triggered to bomb the object, so that the aim of interception is fulfilled.
Description
Technical field: the apparatus and method of interception enemy missile in a kind of military affairs.
Background technology and summary of the invention: open drag parachute and police during according to aircraft landing and invent this device of design with the principle of netting seizure.Its structure is that one cross section is arranged is the tetragonal storage net cage of rescinded angle at a transmitter center, and four diagonal angles are provided with four rocket-launching batterys, launching tube shaft centre line and storage net cage shaft centre line from after an outer angle (5 °~10 °) of opening is arranged forward.One piece of pencil rocket is arranged in each launching tube.(mesh can't be passed just to institute's interception guided missile greatly as far as possible to store the square net that weaves with high strength cord of placing a folding compression in the net cage.Reduce volume to reduce after the rope consumption makes it folding as far as possible), the storage net cage respectively has elongated slot to communicate with the center line relevant position of launching tube, and four angles of square net are assembled into by two adjacent head ropes gathers rope and passes elongated slot and be attached near the rocket flight center of gravity the yarn ear.The rocket front portion is the warhead of highly sensitive acoustic fuse control.The rear portion is propellant powder and igniter.Form a blocking module by such nested structure, and by a plurality of such modules and search surveillance radar, tracking aiming radar, photodetection control device, electric and follower are combined into an interception fight yarn system and are installed to needed place.Its effect is to realize like this; Surveying discovery when surveillance radar has target to enter the effective range scope.By radar tracker control transmitter run-home and starting ignition device, four pieces of rocket synchronized transmissions are flown relatively with the square wire side target that certain outer subtended angle is folding in tow.And open square net rapidly, owing to the rope curbing function that is tethered on the rocket flight center of gravity, four pieces of outer subtended angles of rocket corrections change the parallel flight of trawlnet into after net opens fully.When net with after target contacts because of the impulsive force of target certainly greater than the towing tension of four pieces of rockets; and because the flexibility of netting has cushioned the impulsive force of target; so target drags netting and four pieces of rockets are done oppositely flight; the moving four pieces of rockets of guipure are drawn close or are collided to target in reverse flight course; so acoustic fuse causes the warhead blast with the target demolition, thereby reaches interception purposes.This just made in the past will be accurate to the interception that point-to-point interception changes over the face of certain area, and reliability is improved greatly.This method realizes that difficulty is also little, and cost is not high relatively yet, can be used for the ship that navigates, aircraft, and the defending missile of various military targets such as radar station is attacked.Even can develop into interception intercontinental missile and deep space satellite, and also can make rocket into anti-torpedo and submarine mine that small torpedo is used for submarine, development potentiality is arranged very much.
Description of drawings: Fig. 1, Fig. 2 are structural representation, and wherein Fig. 1 is that A is that B-B is to view to view, Fig. 2.
Fig. 3 to Fig. 6 is emission, intercept process schematic diagram.Wherein Fig. 3 is emission initial procedure schematic diagram,
Fig. 4, Fig. 5 are that net opens back flight schematic diagram fully.Fig. 5 is that the C of Fig. 4 is to view.
Fig. 6 is a net and mechanism schematic diagram after target contacts.
(1) folding square net, (2) rocket, (3), launching tube, (4) storage net cage, (5) long straight trough, (6) yarn ear, (7) thin control rope among Fig. 2, Fig. 3.
The specific embodiment: technology transfer is produced after producing typing for the organization development test of national military project research department, equips our troops.
Claims (1)
1. the scope of asking for protection is; In a square long case (4), place the square net (1) of a folding compression, the outside, four diagonal angles at case is provided with four rocket-launching batterys (3) after rescinded angle, in four pieces of pencil rockets (2) are arranged, rocket central axis and net cage central axis from after an outer angle of opening is arranged forward, and there is a long straight trough (5) to communicate, four angles of square net are assembled into by adjacent two head ropes gathers rope and passes on the attaching lug that elongated slot is attached to the rocket flight center of gravity, such device forms a transmitter module, and by a plurality of such modules and search surveillance radar, the tracking aiming radar, Electro-Optical Sensor Set, servo-actuated and electric part are combined into an intercepting system, when radar is found to have target to enter effective range, radar control system run-home emission also spreads a net rapidly, when net and its impulsive force after target contacts greater than the rocket towing tension, so target net with regard to traction and rocket is done oppositely flight, rocket affects down at nettle and draws close to target in reverse flight course, acoustic fuse is ignited warhead target is demolished, and reaches the purpose of interception.
Priority Applications (1)
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CN2009101866119A CN102087083A (en) | 2009-12-03 | 2009-12-03 | Rope course type short-range missile intercepting device |
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CN2009101866119A CN102087083A (en) | 2009-12-03 | 2009-12-03 | Rope course type short-range missile intercepting device |
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CN102087083A true CN102087083A (en) | 2011-06-08 |
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CN2009101866119A Pending CN102087083A (en) | 2009-12-03 | 2009-12-03 | Rope course type short-range missile intercepting device |
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Application publication date: 20110608 |