Preparation method of ablation-resistant anti-scouring ethylene-propylene-diene monomer rubber heat insulating material

A technology of EPDM and thermal insulation materials, applied in the field of thermal insulation materials, can solve the problems of inconsiderate different characteristics of strategic and tactical solid rocket motors, backward design of artificial debonding layers of thermal insulation layers, etc., and achieve stable and effective thermal protection effects, Mitigates negative mass, low density effects

Inactive Publication Date: 2020-01-24
陕西逸丰品科航空科技有限公司
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

For example, in the early stage, the large solid rocket motors used in different types of strategic missiles and the small solid rocket motors used in tactical missiles in our country sometimes used the same insulation material formula (in some models in active service), and the difference between strategic and tactical solid rocket motors The characteristics are not well considered, and the design of the artificial debonding layer of the thermal insulation layer is relatively backward

Method used

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Embodiment Construction

[0027] In order to enable those skilled in the art to better understand that the technical solutions of the present invention can be implemented, the present invention will be further described below in conjunction with specific examples, but the given examples are only used as illustrations of the present invention, not as limitations of the present invention.

[0028] The requirements for the material of the thermal insulation layer of the rocket engine are low density, high tensile strength and elongation, low ablation rate, and low density, which means that under the same volume, the mass of the thermal insulation layer will be lighter, and the negative mass of the engine If it becomes smaller, the flight distance of the rocket engine will increase; the greater the tensile strength and elongation, the less likely the thermal insulation layer will change when the stress of the engine charge changes, and the more it can ensure the normal operation of the rocket engine; the abl...

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Abstract

The invention relates to a preparation method of an ablation-resistant anti-scouring ethylene-propylene-diene monomer rubber heat insulating material. The preparation method comprises the following steps: S1, adopting an ethylene-propylene-diene monomer rubber material as a matrix material, and adding an ablation-resistant auxiliary material, fibers, a softener, a reinforcing agent, a vulcanizingsystem and other preservatives into the matrix material; S2, carrying out plastication and mixing procedures, and formulating a basic formula meeting mechanical and ablation performance; S3, manufacturing small samples, mechanical test pieces and ablation test pieces, and detecting mechanical and ablation performance; S4, analyzing performance detection data on the basis of detection, and adjusting the proportion of the auxiliary materials; S5, adjusting the formula, and then preparing small samples; S6, preparing mechanical test pieces, ablation test pieces, heat-conducting test pieces and density test pieces, carrying out detection to obtain detection data, and finally detecting a final formula; and S7, preparing a novel material according to the final formula to obtain the heat insulating material. The heat insulating material provided by the invention has the advantages of low density, good anti-scouring and ablation-resistant performance, excellent bonding performance and excellent comprehensive performance.

Description

technical field [0001] The invention belongs to the technical field of thermal insulation materials, and in particular relates to a preparation method of an ablation-resistant and scour-resistant EPDM thermal insulation material. Background technique [0002] The primary function of the insulation layer is to insulate the solid rocket motor combustor casing to prevent the rocket motor casing from reaching temperatures that would endanger its structural integrity. In addition, the thermal insulation layer also plays a role in controlling the combustion surface of the solid propellant grain, buffering the transfer of shell strain to the solid propellant, preventing the migration of fluid chemical components in the rocket engine, preventing the combustion products from scouring the shell, and sealing the shell. , joints and accessories to prevent pressure loss and damage to it by thermal combustion products; guide combustion products to enter the nozzle in a laminar flow to the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C08L23/16C08L77/10C08K13/02C08K5/09C08K5/12C08K3/06C08K3/36C08K3/22
CPCC08L23/16C08L2205/16C08L2201/08C08K2003/2296C08L77/10C08K13/02C08K5/09C08K5/12C08K3/06C08K3/36C08K3/22
Inventor 路旭路逸宸苏媛
Owner 陕西逸丰品科航空科技有限公司
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