CN103017611A - Arresting barrier technology of guided missile end barrier - Google Patents

Arresting barrier technology of guided missile end barrier Download PDF

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Publication number
CN103017611A
CN103017611A CN 201110290045 CN201110290045A CN103017611A CN 103017611 A CN103017611 A CN 103017611A CN 201110290045 CN201110290045 CN 201110290045 CN 201110290045 A CN201110290045 A CN 201110290045A CN 103017611 A CN103017611 A CN 103017611A
Authority
CN
China
Prior art keywords
guided missile
net
rocket projectile
missile
pulled
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
CN 201110290045
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Chinese (zh)
Inventor
冯晓雪
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN 201110290045 priority Critical patent/CN103017611A/en
Publication of CN103017611A publication Critical patent/CN103017611A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a controllable flying rocket projectile. A big net is made of high strength fibers; each mesh is larger than 2 cm; net lines are used as leads; four high explosive grenades are arranged per forty square centimeters; when a guided missile passes through the net, the four high explosive grenades detonate the guided missile; when the guided missile of an enemy attacks, a radar of a party opposite to the enemy finds out the guided missile, and the track of the guided missile is worked out through a computer; a net pack is pulled by the rocket projectile, and the net can be pulled open by four parachute packs under a pulling force of the rocket projectile; and the quicker the speed of the rocket projectile is, the larger the net is pulled open. A skynet is pulled in the sky to meet the incoming guided missile; and the skynet being 100 meters long and 100 meters wide can be pulled open by the controllable flying rocket projectile towards the track of the incoming guided missile, so as to meet the incoming guided missile, so that an airplane can escape along a reverse direction.

Description

Missiles ' terminal interception catch net technology
Technical field
The Interception Technology of missiles ' terminal.Present interception thinking with the missile intercept guided missile.Go intercept point to need pre-warning time with point, the radar that this time need to get well and the faster interceptor of flight.Developing better radar early warning system needs the technology of time and Geng Gao, if we exchange the time for the space, we tackle with face, and guided missile also can be with net interception. when aircraft by guided missile chase after can the sky fly the time.Saving somebody's life with catch net is the best way.When aircraft can intercept attack oneself guided missile the time with how it feels.
Background technology
The rocket projectile of controllable flight.With the large net that high strength fibre is made, mesh is 40 square centimeters of four high-explosive projectiles of lead-in wire greater than 2 centimetres of netting twines, and four bombs of periphery are ignited guided missile when guided missile is crossed net.The radar of oneself is found to calculate track by computer when enemy missile is attacked, and rocket projectile hauls the net bag, pulls open at off line available four the directed packs of the pulling force of rocket projectile.What the faster net of the speed of rocket projectile drew more opens.Pull open a large net on high and meet to attack guided missile.The rocket projectile of one piece of controllable flight pulls open one long 100 meters wide 100 meters sky net in face of the ballistic trajectory of attacking guided missile, meets to attack guided missile, and aircraft can be along runing away in the other direction.
Summary of the invention
When one airplane is locked by enemy plane or is locked by surface-to-air ballistic missile, MISSILE LAUNCHING is directed reach aircraft, rebecca finds that guided missile only has evasive maneuvering, break away from missile attack, at this moment automatic acquisition system is opened automatically, locking air-to-air missile or surface-to-air ballistic missile ballistic trajectory, calculate the ballistic trajectory of enemy missile by computer, pass to rocket projectile, rocket projectile hauls the net bag, pulls open at off line available four the directed packs of the pulling force of rocket projectile.What the faster net of the speed of rocket projectile drew more opens., rocket projectile pulls open one wide 100 meters high 100 meters large wire net from airplane tail group and is attacking on the missile trajectory.Tackle.This mesh of throwing the net is 40 square centimeters of four high-explosive projectiles of lead-in wire greater than 2 centimetres of netting twines.Four bombs of periphery are ignited guided missile when guided missile is crossed net.The reason of Here it is thatch and shield.Mao Buru keeps off thatch with shield with the thatch gear, and this is simple.This hold-up interception method not only can be used for aircraft can also be used for naval vessel tank and fixed target.The relative missile intercept guided missile of this method requires lowly to radar, requires also not high to the velocity accuracy of guided missile.Economical and practical.

Claims (1)

1. pull open on high a large net of hanging up full bomb with rocket projectile and tackle to attack guided missile.
CN 201110290045 2011-09-28 2011-09-28 Arresting barrier technology of guided missile end barrier Pending CN103017611A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110290045 CN103017611A (en) 2011-09-28 2011-09-28 Arresting barrier technology of guided missile end barrier

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110290045 CN103017611A (en) 2011-09-28 2011-09-28 Arresting barrier technology of guided missile end barrier

Publications (1)

Publication Number Publication Date
CN103017611A true CN103017611A (en) 2013-04-03

Family

ID=47966496

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110290045 Pending CN103017611A (en) 2011-09-28 2011-09-28 Arresting barrier technology of guided missile end barrier

Country Status (1)

Country Link
CN (1) CN103017611A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105258573A (en) * 2015-10-21 2016-01-20 李宏江 Air defense skynet
CN106403717A (en) * 2015-07-27 2017-02-15 郭三学 Boat blocking device
CN106959054A (en) * 2017-03-17 2017-07-18 江苏锐盾警用装备制造有限公司 A kind of unmanned plane catches blocking apparatus

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106403717A (en) * 2015-07-27 2017-02-15 郭三学 Boat blocking device
CN105258573A (en) * 2015-10-21 2016-01-20 李宏江 Air defense skynet
CN106959054A (en) * 2017-03-17 2017-07-18 江苏锐盾警用装备制造有限公司 A kind of unmanned plane catches blocking apparatus
CN106959054B (en) * 2017-03-17 2018-07-27 江苏锐盾警用装备制造有限公司 A kind of unmanned plane capture blocking apparatus

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PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130403