Large-caliber supersonic target projectile for testing or training

A supersonic, large-caliber technology, applied in the field of simulated target missiles for testing or training, can solve the problem of low speed, difficulty in meeting the requirements of similarity, economy and repeatability of simulated targets for testing or training, and inability to simulate the speed of cruise missiles characteristics, etc., to achieve the effects of good ballistic repeatability, increased thrust, and stable flight attitude

Inactive Publication Date: 2013-09-18
THE THIRD ENG CORPS RES INST OF THE HEADQUARTERS OF GENERAL STAFF PLA
View PDF7 Cites 6 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] The aircraft model substitution method is cheap, reusable, and can better simulate the geometric characteristics of cruise missiles, but its disadvantage is that the speed is too low to simulate the speed characteristics of cruise missiles;
[0011] In summary, the existing alternative target methods are difficult to meet the requirements of test or training for the similarity, economy and repeatability of simulated targets

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Large-caliber supersonic target projectile for testing or training
  • Large-caliber supersonic target projectile for testing or training
  • Large-caliber supersonic target projectile for testing or training

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0028] In order to make it easier for those skilled in the art to understand and implement the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0029] figure 1 Shown is the schematic diagram of the structure of the target projectile of the present invention, which is a 252mm caliber supersonic target projectile propelled by a rocket engine. Thread connection is adopted between the engine and the target warhead. When the temperature is 20°C, the thrust of the rocket engine is 187.5kN, the structural length of the target warhead is not less than 2m, and the mass is 45.5kg.

[0030] figure 2 It is a structural schematic diagram of a rocket engine, which mainly includes a combustion chamber, a nozzle and fins 3 . The front end of the combustion chamber is threadedly connected with the target warhead, and the rear end is connected with the nozzle, and the outer circumfere...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

PropertyMeasurementUnit
Thicknessaaaaaaaaaa
Login to view more

Abstract

The invention relates to a large-caliber supersonic target projectile for testing or training. The large-caliber supersonic target projectile comprises a rocket engine and a target projectile, wherein the rocket engine comprises a combustion chamber, a jet tube and a plurality of fins; the front end of the combustion chamber is connected with the target projectile, and the back end of the combustion chamber is connected with the jet tube; the fins are distributed on the outer circumference of the jet tube; the target projectile comprises a shell, a counterweight body and a counterweight ring; the shell has a hollow structure; the counterweight body is embedded and fixed at the inner front end of the shell; and the counterweight ring is arranged on the middle part of the shell, and is fixed by using a preset separation blade. According to the large-aperture supersonic target projectile, on one hand, the gunpowder loading structure and gunpowder loading scheme of the rocket engine are improved, so that the thrust force of the engine is increased; on the other hand, the weight of a head structure is reduced, so that a high launching speed is achieved for the complete projectile; and target characteristics such as geometry, speed, infrared rays, radar reflecting area and the like at the final flying stage of a cruise missile can be well simulated, so that the requirements of testing or training on the similarity, economy and repeatability of a simulated target are met.

Description

technical field [0001] The invention relates to a beacon for radar performance debugging and detection, in particular to a large-diameter supersonic target missile capable of simulating the characteristics of cruise missile-related targets, and belongs to the technical field of simulated target missiles for testing or training. Background technique [0002] At present, the targets used in domestic and foreign interception cruise missile training and joint debugging tests of ultra-short-range anti-missile weapon systems generally adopt the following methods: [0003] 1. Aircraft release method [0004] This is a traditional method for testing precision-guided weapons, which is characterized by strong intuition, but also has many shortcomings, such as: high cost; difficult to control the flight trajectory and landing point; high requirements for the test field area; The scope of application is limited and the risk is high. [0005] 2. Rocket Prying [0006] Build a special ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): F42B8/24
Inventor 周长省高超徐流恩易治任辉启伍俊韩彧林加剑穆朝民
Owner THE THIRD ENG CORPS RES INST OF THE HEADQUARTERS OF GENERAL STAFF PLA
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products