Preparation method for active metal micro-projectile loading high explosive

A technology of active metal and high-energy explosives, applied in the fields of energetic materials, damage and ammunition engineering, can solve the problems of high pressure of ballistic calculation, low probability of successful interception, and difficulty in tracking, etc. powerful effect

Active Publication Date: 2019-10-22
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to propose a hypersonic aircraft loaded with high-energy explosives to solve the problems of extremely fast flight speed, extremely difficult to capture

Method used

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  • Preparation method for active metal micro-projectile loading high explosive
  • Preparation method for active metal micro-projectile loading high explosive
  • Preparation method for active metal micro-projectile loading high explosive

Examples

Experimental program
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Effect test

Embodiment 1

[0027] A preparation method of active metal micro-projectiles loaded with high-energy explosives, the specific steps are as follows:

[0028] (1) Weighing and powder mixing: the mass ratio of each component is: active metal / heavy metal / fluoropolymer = magnesium aluminum alloy / tungsten / polytetrafluoroethylene = 30 / 15 / 55, that is, weigh 15g of magnesium aluminum alloy powder , tungsten powder 7.5g, polytetrafluoroethylene powder 27.5g, placed in a planetary mixer and mixed for 20min, and mixed;

[0029] (2) Molding: put the above-mentioned uniformly mixed powder in a mold for compression, the pressure is 50MPa, the pressurization rate is 30N / s, the pressure holding time is 5min, the pressure release rate is 30N / s, and the mold is demoulded after the pressure release to obtain the molded part A;

[0030] (3) Sintering: Put the above-mentioned molded part A after demoulding in a sintering furnace for sintering. During the sintering process, an argon atmosphere is used. The...

Embodiment 2

[0035] A preparation method of active metal micro-projectiles loaded with high-energy explosives, the specific steps are as follows:

[0036] (1) Weighing and powder mixing: 50g per sample, the mass ratio of each component is: active metal / heavy metal / fluoropolymer=aluminum / tungsten-zirconium alloy / polytetrafluoroethylene=25 / 20 / 55, namely Take 12.5g of aluminum powder, 10g of tungsten-zirconium alloy powder, and 27.5g of polytetrafluoroethylene powder, mix them in a planetary mixer for 20 minutes, and mix well;

[0037] (2) Molding: put the above-mentioned uniformly mixed powder in a mold for compression, the pressure is 50MPa, the pressurization rate is 30N / s, the pressure holding time is 5min, the pressure release rate is 30N / s, and the mold is demoulded after the pressure release to obtain the molded part A;

[0038] (3) Sintering: Put the above-mentioned molded part A after demoulding in a sintering furnace for sintering. During the sintering process, an argon atmosphere i...

Embodiment 3

[0043] A preparation method of active metal micro-projectiles loaded with high-energy explosives, the specific steps are as follows:

[0044] (1) Weighing and powder mixing: 50g per sample each time, the mass ratio of each component is: active metal / heavy metal / fluoropolymer=magnesium / tungsten / fluororubber=25 / 15 / 60, that is, weigh 12.5 grams of magnesium powder g, 7.5g of tungsten powder, 30g of fluororubber powder, mixed in a planetary mixer for 30min, and mixed evenly;

[0045](2) Molding: put the above-mentioned uniformly mixed powder in a mold for compression, the pressure is 40MPa, the pressurization rate is 30N / s, the pressure holding time is 5min, the pressure release rate is 30N / s, and the mold is demoulded after the pressure release to obtain the molded part A;

[0046] (3) Sintering: Place the above-mentioned molded part A after demoulding in a sintering furnace for sintering. During the sintering process, an argon atmosphere is used. The sintering temperature is 360...

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Abstract

The invention relates to a preparation method for an active metal micro-projectile loading a high explosive and belongs to the field of energetic material, damage and ammunition engineering. The active metal micro-projectile loading a high explosive prepared by the preparation method combines advantages of the active metal energetic material and the high explosive: an active metal micro-projectileprojectile cloud is formed by the projectile, a trajectory of an incoming missile is roughly resolved to give a substantial flight path, and the explosive is scattered around important targets on thetrajectory or the protected important targets. For a hypersonic vehicle, the trajectory resolving and trajectory predicting and calculating pressure is reduced without capturing and tracking, so thatthe intercepting probability is improved. A shell of the micro-projectile is prepared by compounding the active meal and an adhesive. An inner charge is an existing high molecular bonding explosive or a casted mixed explosive which is sophisticated in technology. Generally, the micro-projectile is easily available in raw material, simple in process, low in cost, convenient to prepare on a large scale and feasible.

Description

technical field [0001] The invention relates to a method for preparing active metal micro-projectiles loaded with high-energy explosives, belonging to the fields of energetic materials, damage and ammunition engineering. Background technique [0002] The maximum speed of a hypersonic vehicle can reach more than 25 times the speed of sound, which cannot be captured by conventional military radar technology. The emergence of hypersonic aircraft will greatly change the existing air defense and anti-missile technology pattern, and even make the existing air defense and anti-missile system completely ineffective. Some important targets will be completely exposed to enemy firepower and subject to tactical or even strategic strikes . Traditional air defense and anti-missile technology focuses on tracking targets, calculating ballistics, and predicting rendezvous trajectories, and achieves the purpose of interception through the "scalpel" type of point-to-point precise collision or...

Claims

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Application Information

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IPC IPC(8): F42B33/02B22F1/00B22F3/02B22F3/10C22C21/00C22C23/00
CPCF42B33/0214B22F3/02B22F3/1007C22C21/00C22C23/00B22F1/10
Inventor 吕席卷束庆海马仙龙赵帅石艳松陈树森金韶华施瑞吴启才
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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