CN204612600U - A kind of guided missile protective device - Google Patents
A kind of guided missile protective device Download PDFInfo
- Publication number
- CN204612600U CN204612600U CN201520281662.0U CN201520281662U CN204612600U CN 204612600 U CN204612600 U CN 204612600U CN 201520281662 U CN201520281662 U CN 201520281662U CN 204612600 U CN204612600 U CN 204612600U
- Authority
- CN
- China
- Prior art keywords
- guided missile
- missile
- daughter
- carrier
- protective device
- 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.)
- Expired - Fee Related
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A kind of guided missile protective device; comprise guided missile carrier (1) and be arranged on the multistage propulsion system (2) below guided missile carrier (1); described guided missile carrier (1) is provided with guided missile (3); it is characterized in that: described guided missile carrier (1) is provided with at least one daughter missile (4) for preventing anti-guided missile from attacking; described daughter missile (4) is evenly distributed on the periphery of guided missile (3); the number of described daughter missile (4) is four, and described multistage propulsion system is that Pyatyi promotes.The arranging of daughter missile of guided missile protective device of the present utility model can effectively prevent antimissile attack, reduces economic loss.
Description
Technical field
The utility model relates to protective device, specifically refers to a kind of guided missile protective device.
Background technology
There is vast territory in China, the vast people masses, in increasingly competitive international big environment, strengthening China defense force and be important.In the prior art, before MISSILE LAUNCHING to aerial arrival destination, guided missile is all faced with the threat of being shot down by anti-guided missile, and because guided missile is expensive, in the stroke of guided missile, contingency is shot down and can be caused huge economic loss and miss one's aim.
Utility model content
The technical problems to be solved in the utility model overcomes above technological deficiency, provides a kind of guided missile that prevents to be shot down possible a kind of guided missile protective device by anti-guided missile in stroke.
For solving the problems of the technologies described above; the technical scheme that the utility model provides is: a kind of guided missile protective device; comprise guided missile carrier and be arranged on the multistage propulsion system below guided missile carrier; described guided missile carrier is provided with guided missile; described guided missile carrier is provided with at least one daughter missile for preventing anti-guided missile from attacking, and described daughter missile is evenly distributed on the periphery of guided missile.
The utility model advantage is compared with prior art: the arranging of daughter missile of guided missile protective device of the present utility model can effectively prevent antimissile attack, reduces economic loss.
As improvement, the number of described daughter missile is four, can effectively prevent antimissile attack like this.
As improvement, described multistage propulsion system is that Pyatyi promotes, and this kind of structure pushes effective.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of guided missile protective device of the utility model top view.
Fig. 2 is the structural representation of a kind of guided missile protective device of the utility model front view.
As shown in the figure: 1, guided missile carrier, 2, multistage propulsion system, 3, guided missile, 4, daughter missile.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
By reference to the accompanying drawings; a kind of guided missile protective device; the multistage propulsion system 2 comprising guided missile carrier 1 and be arranged on below guided missile carrier 1; described guided missile carrier 1 is provided with guided missile 3; described guided missile carrier 1 is provided with at least one daughter missile 4 for preventing anti-guided missile from attacking, and described daughter missile 4 is evenly distributed on the periphery of guided missile 3.
The number of described daughter missile is four.
Described multistage propulsion system is that Pyatyi promotes.
Operation principle of the present utility model: guided missile is in running, when the detector of radar or guided missile detect anti-guided missile interception or threatened in free-running operation target time, automatically firing order is assigned to the daughter missile of its year, (also can by ground remote control), daughter missile launches goal from guided missile carrier, in the running of this daughter missile, daughter missile uses Automatic-searching aiming means automatically to march on towards target until hit, and the remaining daughter missile be present on guided missile carrier can with main missile target, the attack effect that this kind of mode produces is better.
Be described the utility model and embodiment thereof above, this description does not have restricted, and shown in accompanying drawing is also one of embodiment of the present utility model, and actual structure is not limited thereto.If generally speaking those of ordinary skill in the art enlightens by it, when not departing from the utility model and creating aim, design the frame mode similar to this technical scheme and embodiment without creationary, protection domain of the present utility model all should be belonged to.
Claims (3)
1. a guided missile protective device; comprise guided missile carrier (1) and be arranged on the multistage propulsion system (2) below guided missile carrier (1); described guided missile carrier (1) is provided with guided missile (3); it is characterized in that: described guided missile carrier (1) is provided with at least one daughter missile (4) for preventing anti-guided missile from attacking, and described daughter missile (4) is evenly distributed on the periphery of guided missile (3).
2. a kind of guided missile protective device according to claim 1, is characterized in that: the number of described daughter missile (4) is four.
3. a kind of guided missile protective device according to claim 1, is characterized in that: described multistage propulsion system is that Pyatyi promotes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520281662.0U CN204612600U (en) | 2015-05-04 | 2015-05-04 | A kind of guided missile protective device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520281662.0U CN204612600U (en) | 2015-05-04 | 2015-05-04 | A kind of guided missile protective device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN204612600U true CN204612600U (en) | 2015-09-02 |
Family
ID=53965153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201520281662.0U Expired - Fee Related CN204612600U (en) | 2015-05-04 | 2015-05-04 | A kind of guided missile protective device |
Country Status (1)
Country | Link |
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CN (1) | CN204612600U (en) |
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2015
- 2015-05-04 CN CN201520281662.0U patent/CN204612600U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150902 Termination date: 20180504 |