CN203561295U - Simulated rocket projectile for emplacement reconnaissance radar training - Google Patents
Simulated rocket projectile for emplacement reconnaissance radar training Download PDFInfo
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- CN203561295U CN203561295U CN201320835970.4U CN201320835970U CN203561295U CN 203561295 U CN203561295 U CN 203561295U CN 201320835970 U CN201320835970 U CN 201320835970U CN 203561295 U CN203561295 U CN 203561295U
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- projectile
- igniter
- projectile body
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Abstract
A simulated rocket projectile for emplacement reconnaissance radar training comprises a projectile body, a rocket engine, an igniter and an empennage. The simulated rocket projectile is characterized in that a shell of the projectile body is composed of a curing agent added unsaturated polyester inner layer, a glass fiber middle layer and a tinfoil silkscreen fabric outer layer. A tinfoil silkscreen fabric reflection layer is attached to the outer surface of the empennage, a canopy chamber and a canopy opening device are arranged on the upper portion of an inner cavity of the projectile body, an ignition contact is arranged in the middle of the projectile body and connected with the igniter at the bottom of a propellant chamber of the projectile body through a control line, and a smoke generator connected with the igniter is further arranged in the projectile body. The simulated rocket projectile is large in electromagnetic wave reflection section and convenient for radar recognition and detection, different trajectory targets can be vividly simulated in terms of the launching speed, the launching angle and the radar section, damages to the projectile can be alleviated while damages to ground targets can be avoided by combination of the simulated rocket projectile and a parachuting device, recovery of the projectile body is facilitated, and a ballistic trajectory can be clearly observed by the aid of the smoke generator. Moreover, the projectile body is simple in structure, and manufacturing cost is greatly saved.
Description
Technical field
The utility model relates to a kind of training simulated rocket bullet, particularly a kind of simulated rocket bullet that is suitable for simulating Ballistic Target in artillery location radar training.
Background technology
Firing position reconnaissance and calibration radar is used for scouting position, enemy gun emplacement, can scout, identify and calculate forming the target of trajectory, main by the initial velocity of investigation Ballistic Target, calculate to check the quality of radar performance, therefore,, if peacetime training does not have Ballistic Target, radar just can not be followed the tracks of reckoning, radar station cannot be scouted school and penetrate training, also cannot verify the quality of radar performance.
At present, organize Gun Position Radar station to scout school and penetrate operation, mainly in conjunction with ball firing, carry out training, the shortcoming of existence is to rely on the Ballistic Target of live shell to carry out artillery location radar training, and tissue training's cost is high, training time is short, not only tissue training but also participate in manoeuvre, both easily clash, and affect training effect, and existing simulated rocket bullet manufacture cost high, transmitting initial velocity low, radar reflection cross section does not reach reflecting effect.
Summary of the invention
The purpose of this utility model is to provide a kind of artillery location radar training simulated rocket bullet, overcome that live shell tissue training chance is few, cost is high, guarantee is complicated, and existing simulated rocket bullet is manufactured the technical problem that the low and radar reflection cross section of cost high emission initial velocity does not reach reflecting effect, this artillery location radar training is high with simulated rocket bullet launch velocity, firing angle is adjustable, radar reflection cross section is large, and be convenient to observe ballistic trajectory and reclaim body, body structure is simple, it is low to manufacture cost.
The technical scheme that the utility model adopts is: comprise body, rocket engine, igniter and empennage, it is characterized in that: body shell is comprised of the unsaturated polyester (UP) internal layer, glass fibre intermediate layer and the tinfoil paper screen cloth skin that are added with curing agent, empennage appearance is posted tinfoil paper screen cloth reflecting layer, body inner chamber top arranges canopy storehouse and parachute opener, body middle part arranges contactless ignition, the igniter that connects bottom, body propellant powder storehouse by control line, also arranges the smoke generator being connected with igniter in body.
Body head arranges smoke-dispelling hole.
The good effect the utlity model has is: this simulated rocket bullet is large to electromagnetic reflecting section, be convenient to radar recognition detection, at emission rate and the different Ballistic Target of simulation true to nature of energy on radar cross section, in conjunction with parachuting device, can alleviate body landing damage and avoid injury on a surface target, being convenient to observe ballistic trajectory and reclaiming body; Can clear observation ballistic trajectory in conjunction with smoke generator, and body structure is simple, has greatly saved and has manufactured cost.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is further described.
Fig. 1 is a kind of structural representation of the present utility model.
Fig. 2 is the section enlarged diagram of the A-A of Fig. 1.
The specific embodiment
According to Fig. 1～2, describe concrete structure of the present utility model and use procedure in detail.
This artillery location radar training comprises body, rocket engine, igniter 10 and empennage 8 with simulated rocket bullet, body shell is comprised of outer 91 trilaminate materials of the unsaturated polyester (UP) internal layer 13, glass fibre intermediate layer 12 and the tinfoil paper screen cloth that are added with curing agent, this trilaminate material is to utilize mold die, and one cast is made.Empennage 8 appearances are posted tinfoil paper screen cloth reflecting layer 92, and such structure increases radar reflection cross section, and rocket projectile body projectile initial velocity is high simultaneously, the requirement to initial velocity while being applicable to radar-reconnaissance.Body inner chamber top arranges canopy storehouse 4 and parachute opener 3, and parachute is installed in canopy storehouse 4, and this parachute assembly is to utilize prior art.Rocket engine is to provide the power section of full bullet, identical with existing rocket engine, propellant powder storehouse 6 and jet pipe 7, consists of.Contactless ignition 5 is arranged on body middle part, connects the igniter 10 of 6 bottoms, propellant powder storehouse by the control line 11 in body.Body inner chamber top is also provided with smoke generator 2, by time-delay mechanism, is connected with igniter, and smoke generator produces smog and distributes by the smoke-dispelling hole 1 on bullet.
Use procedure: this imitating shell is by launcher and the transmitting of IGNITION CONTROL box.Igniter on body is by control line 11 propellant powder in ignition engine under the function of current, and gun propellant combustion also sprays flame gas from jet pipe, promotes imitating shell and arrives predetermined height.The time-delay mechanism connecting by igniter is controlled the fumicants of lighting smoke generator inside, fumicants is sowed outside body by smoke-dispelling hole after being lighted, forming smog track is convenient to observe, fumicants burning finishes rear canopy storehouse and starts action by parachute opener, canopy is opened, and the landing of the residual body of the imitating shell that plays, under the effect that lifts of hanging umbrella, the remains such as this imitating shell housing slowly land to be less than the speed of 8m/s.Parachuting device is for full bullet provides safe system, for ground staff provides safeguard safely.
The utility model is by practical application, and result shows to provide the Ballistic Target of artillery location radar training need, and its emission rate and radar cross section all meet radar identification, tracer request.The body that this imitating shell adopts metal tinfoil paper screen cloth to make, has realized body to electromagnetic reflection, and body reflecting section is large, is convenient to radar recognition detection.This imitating shell can be simulated different Ballistic Targets, comprise the Ballistic Targets such as mortar projectile, pomegranate shell, rocket projectile, training is penetrated in the scouting and the school that meet artillery location radar, check radar computer is to the reckoning of Ballistic Target and disposal ability, can also check the technical performance of phased array system artillery location radar, find in time the fault that radar exists.
Claims (2)
1. an artillery location radar is trained and is used simulated rocket bullet, comprise body, rocket engine, igniter and empennage, it is characterized in that: body shell is comprised of the unsaturated polyester (UP) internal layer, glass fibre intermediate layer and the tinfoil paper screen cloth skin that are added with curing agent, empennage appearance is posted tinfoil paper screen cloth reflecting layer, body inner chamber top arranges canopy storehouse and parachute opener, body middle part arranges contactless ignition, the igniter that connects bottom, body propellant powder storehouse by control line, also arranges the smoke generator being connected with igniter in body.
2. simulated rocket bullet is used in artillery location radar training according to claim 1, it is characterized in that: body head arranges loose mouth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320835970.4U CN203561295U (en) | 2013-12-18 | 2013-12-18 | Simulated rocket projectile for emplacement reconnaissance radar training |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320835970.4U CN203561295U (en) | 2013-12-18 | 2013-12-18 | Simulated rocket projectile for emplacement reconnaissance radar training |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203561295U true CN203561295U (en) | 2014-04-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320835970.4U Expired - Fee Related CN203561295U (en) | 2013-12-18 | 2013-12-18 | Simulated rocket projectile for emplacement reconnaissance radar training |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203561295U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104596361A (en) * | 2014-10-20 | 2015-05-06 | 中国运载火箭技术研究院 | Launcher sublevel recovery method |
| CN108107076A (en) * | 2017-12-19 | 2018-06-01 | 中国舰船研究设计中心 | A kind of ammunition Hot disaster measurement model for full size fire test |
| CN110440829A (en) * | 2019-08-19 | 2019-11-12 | 哈尔滨工业大学 | A kind of inertia device high overload test device and method |
-
2013
- 2013-12-18 CN CN201320835970.4U patent/CN203561295U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104596361A (en) * | 2014-10-20 | 2015-05-06 | 中国运载火箭技术研究院 | Launcher sublevel recovery method |
| CN104596361B (en) * | 2014-10-20 | 2016-03-30 | 中国运载火箭技术研究院 | The sub-level recovery method of a kind of carrier rocket |
| CN108107076A (en) * | 2017-12-19 | 2018-06-01 | 中国舰船研究设计中心 | A kind of ammunition Hot disaster measurement model for full size fire test |
| CN110440829A (en) * | 2019-08-19 | 2019-11-12 | 哈尔滨工业大学 | A kind of inertia device high overload test device and method |
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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: 20140423 Termination date: 20211218 |