A test system for testing the delay time of a fuze of a target of dynamic penetration intensity of a penetration bomb

Abstract

The present application relates to a kind of dynamic penetration strength target fuze delay detonation time test system of penetration bomb, belong to the field of fuze system.For including: fuze system, rocket sled body, target body, video system;Rocket sled body includes: rocket sled car, rocket sled track, stop block;Target body includes: target front marker, strength target, target rear marker;Rocket sled track upper left end is equipped with rocket sled car, the front end of rocket sled car is connected with fuze system, the right end of rocket sled track upper is fixed stop block, target front marker is arranged outside the right end of rocket sled track right side, with a certain distance from target front marker, strength target right side is equipped with target rear marker;Can effectively verify and measure the dynamic penetration thick scale strength target fuze delay detonation time under the guidance of penetration bomb cavity mode.

Description

Technical Field

[0001] This invention belongs to the field of war ignition systems, specifically relating to a test system for the delayed detonation time of a target fuse for dynamic penetration strength of a penetrating explosive projectile. Background Technology

[0002] The guided penetration detonation system consists of a penetrating warhead and a penetration fuse. It is typically launched from a rocket artillery system. After flying to the target area according to a predetermined control program, the guided penetration detonation warhead collides with the target. The penetrating warhead then penetrates the target body, and the penetration fuse detonates the warhead after a delay according to its pre-set operating mode, causing damage to the target.

[0003] The detonation system of a certain type of guided penetration explosive projectile employs a multi-mode adaptive setting. Depending on the target type, the detonation system's setting modes can be divided into cavity mode, layer-counting mode, and fixed-delay mode for other typical targets. Cavity mode is primarily used to strike targets with thick-scale high-strength protective armor, while layer-counting mode is mainly used to strike targets within specific floors of high-rise buildings. Other typical targets include fortifications, aircraft shelters, underground bunkers, bridges, airport runways, and railways. Taking striking a high-strength target as an example, the guided penetration explosive projectile is set to cavity mode by the ground-based rocket artillery fire control system. After launch, the fuze completes its release according to the operational sequence. Upon contact with the high-strength target, the collision overload triggers the fuze's timing to zero. The guided penetration explosive projectile penetrates the high-strength target, and the fuze's timing reaches zero. Then, unloading is determined based on the unloading threshold. After the unloading determination is valid, detonation occurs at the delay time corresponding to the basic timetable of the cavity mode, achieving detonation within a specific distance after penetrating the entire high-strength target, thus achieving the highly efficient destructive power of cavity mode.

[0004] The delayed detonation time of the fuze in a guided penetration-propellant warhead system determines whether the rocket can penetrate to the predetermined target location before detonating, maximizing the warhead's explosive power and achieving high-efficiency damage. Taking cavity mode as an example, when penetrating a thick-scale target, the delayed detonation time of the fuze directly affects whether the warhead has reliably penetrated the target by the time of detonation, with the explosion center at the predetermined location behind the target. Direct flight verification is costly, and testing methods are limited during flight verification. Without ground verification of the delayed detonation time of the fuze on a dynamic penetration-strength target, flight tests may result in an unreasonable determination of the delayed detonation time, potentially causing the warhead to detonate prematurely inside the target or beyond a certain distance behind the target, failing to achieve the warhead's optimal destructive power. Summary of the Invention

[0005] (a) Technical problems to be solved

[0006] The technical problem to be solved by this invention is to provide a test system for the delayed detonation time of a target fuze for the dynamic penetration strength of a guided explosive projectile, thereby solving the problem of the lack of ground testing methods for the delayed detonation time of the target fuze for the dynamic penetration strength of a guided explosive projectile.

[0007] (II) Technical Solution

[0008] To solve the above-mentioned technical problems, the present invention provides a test system for the delayed detonation time of a target fuse for dynamic penetration strength of a penetrating explosive projectile, comprising: a detonation system, a rocket skid, a target, and a video recording system;

[0009] The rocket sled body includes: a rocket sled vehicle, a rocket sled track, and stop blocks;

[0010] The target body includes: a target front marker, a strength target, and a target rear marker;

[0011] A rocket sled is provided on the upper left side of the rocket sled track. The front end of the rocket sled is connected to the warhead system. A stop block is fixed on the upper right side of the rocket sled track. A target front marker is set on the outside of the right side of the rocket sled track. The intensity target is set to the right of the target front marker and at a certain distance from the target front marker. A target rear marker is set to the right of the intensity target.

[0012] The video recording system includes three high-speed cameras and a high-speed video recording synchronous triggering system. The three high-speed cameras are referred to as the first high-speed camera, the second high-speed camera, and the third high-speed camera, respectively.

[0013] The center of the field of view of the first high-speed camera is directly facing the front surface of the high-intensity target to observe the motion state of the warhead system before it hits the target.

[0014] The center of the field of view of the second high-speed camera is directly facing the target surface behind the intensity target, and is used to observe the detonation position and time behind the target.

[0015] The third high-speed camera's field of view covers the area from the end of the rocket skid to the marker behind the intensity target, and is used to observe the entire process of the war-initiating system.

[0016] The high-speed video recording synchronous triggering system is used to record the zero point of the video using three high-speed cameras before the warhead system hits the target.

[0017] The testing process is as follows:

[0018] Before the test, the detonation system and rocket skid were assembled on site. The rocket skid was placed on the rocket skid track, the three high-speed cameras were reset, and the rocket skid engine was ignited. When the detonation system touched the target in front of the marker, the constraint between the rocket skid and the detonation system was released, the high-speed synchronous triggering system was activated, and the three high-speed cameras started timing to observe and record the detonation effect of the detonation system after hitting the target and passing through the target.

[0019] The warhead system includes: a warhead and a fuse;

[0020] The warhead is used to achieve dynamic penetration strength against the target under designed initial velocity conditions and to work with the fuse to complete delayed detonation.

[0021] The strength target is used to simulate the impact of a guided blasting projectile in cavitation mode on a thick-scale strength target protected by a target.

[0022] (III) Beneficial Effects

[0023] Compared with the prior art, the present invention has the following beneficial effects: it can effectively verify and measure the delayed detonation time of a guided penetrating thick-scale strength target fuze in cavitation mode. Attached Figure Description

[0024] Figure 1 This is a schematic diagram of the test system of the present invention. Detailed Implementation

[0025] To make the objectives, contents, and advantages of the present invention clearer, the specific embodiments of the present invention will be described in further detail below with reference to the accompanying drawings and examples.

[0026] Example 1

[0027] This embodiment provides a test system for the delayed detonation time of a target fuse for the dynamic penetration strength of a penetrating explosive projectile, including: a detonation system, a rocket skid, a target, and a video recording system;

[0028] The rocket sled body includes: a rocket sled, a rocket sled track, and stop blocks;

[0029] The target body includes: a target front marker, a strength target, and a target rear marker;

[0030] A rocket sled is provided on the upper left side of the rocket sled track. The front end of the rocket sled is connected to the warhead system. A stop block is fixed on the upper right side of the rocket sled track. A target front marker is set on the outside of the right side of the rocket sled track. The intensity target is set to the right of the target front marker and at a certain distance from the target front marker. A target rear marker is set to the right of the intensity target.

[0031] The video recording system includes three high-speed cameras and a high-speed video recording synchronous triggering system. The three high-speed cameras are referred to as the first high-speed camera, the second high-speed camera, and the third high-speed camera, respectively.

[0032] The center of the field of view of the first high-speed camera is directly facing the front surface of the high-intensity target to observe the motion state of the warhead system before it hits the target.

[0033] The center of the field of view of the second high-speed camera is directly facing the target surface behind the intensity target, and is used to observe the detonation position and time behind the target.

[0034] The third high-speed camera's field of view covers the area from the end of the rocket skid to the marker behind the intensity target, and is used to observe the entire process of the war-initiating system.

[0035] The high-speed video recording synchronous triggering system is used to record the zero point of video recording by three high-speed cameras before the warhead system hits the target.

[0036] The testing process is as follows:

[0037] Before the test, the detonation system and rocket skid were assembled on site. The rocket skid was placed on the rocket skid track, the three high-speed cameras were reset, and the rocket skid engine was ignited. When the detonation system touched the target in front of the marker, the constraint between the rocket skid and the detonation system was released, the high-speed synchronous triggering system was activated, and the three high-speed cameras started timing to observe and record the detonation effect of the detonation system after hitting the target and passing through the target.

[0038] The warhead system includes: a warhead and a fuse;

[0039] The warhead is used to achieve dynamic penetration strength against the target under designed initial velocity conditions and to work with the fuse to complete delayed detonation.

[0040] The strength target is used to simulate the impact of a guided blasting projectile in cavitation mode on a thick-scale strength target protected by a target.

[0041] The above description is only a preferred embodiment of the present invention. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present invention, and these improvements and modifications should also be considered within the scope of protection of the present invention.

Claims

1. A test system for the delayed detonation time of a target fuze for dynamic penetration strength of a penetrating explosive projectile, characterized in that, include: Tribulation system, rocket skid, target, video recording system; The rocket sled body includes: a rocket sled vehicle, a rocket sled track, and stop blocks; The target body includes: a target front marker, a strength target, and a target rear marker; A rocket sled is provided on the upper left side of the rocket sled track. The front end of the rocket sled is connected to the warhead system. A stop block is fixed on the upper right side of the rocket sled track. A target front marker is set on the outside of the right side of the rocket sled track. The intensity target is set to the right of the target front marker and at a certain distance from the target front marker. A target rear marker is set to the right of the intensity target. The video recording system includes three high-speed cameras and a high-speed video recording synchronous triggering system. The three high-speed cameras are referred to as the first high-speed camera, the second high-speed camera, and the third high-speed camera, respectively. The center of the field of view of the first high-speed camera is directly facing the front surface of the high-intensity target to observe the motion state of the warhead system before it hits the target. The center of the field of view of the second high-speed camera is directly facing the target surface behind the intensity target, and is used to observe the detonation position and time behind the target. The third high-speed camera's field of view covers the area from the end of the rocket skid to the marker behind the intensity target, and is used to observe the entire process of the war-initiating system. The high-speed video recording synchronous triggering system is used to record the zero point of the video using three high-speed cameras before the warhead system hits the target. The testing process is as follows: Before the test, the detonation system and rocket skid were assembled on site. The rocket skid was placed on the rocket skid track, the three high-speed cameras were reset, and the rocket skid engine was ignited. When the detonation system touched the target in front of the marker, the constraint between the rocket skid and the detonation system was released, the high-speed synchronous triggering system was activated, and the three high-speed cameras started timing to observe and record the detonation effect of the detonation system after hitting the target and passing through the target.

2. The dynamic penetration strength target fuze delayed detonation time testing system for penetrating explosive projectiles as described in claim 1, characterized in that, The warhead system includes: a warhead and a fuse; The warhead is used to achieve dynamic penetration strength against the target under designed initial velocity conditions and to work with the fuse to complete delayed detonation.

3. The dynamic penetration strength target fuze delayed detonation time testing system for penetration explosive projectiles as described in claim 1, characterized in that, The intensity target is used to simulate the impact of a guided high-explosive anti-tank (HEAT) projectile in cavitation mode on a thick-scale intensity target protected against a target.

Images