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丙烯酸类聚合物对丁羟胶片补强/抑制AP热分解研究

黎超华 邓剑如 张习龙 张智威 徐然

固体火箭技术Issue(6):833-837,5.
固体火箭技术Issue(6):833-837,5.DOI:10.7673/j.issn.1006-2793.2014.06.018

丙烯酸类聚合物对丁羟胶片补强/抑制AP热分解研究

Research of the reinforcement of butyl hydroxy film and the inhibition of the thermal decomposition of AP based on acrylic polymer

黎超华 1邓剑如 1张习龙 1张智威 1徐然1

作者信息

  • 1. 湖南大学 化学化工学院,长沙 410082
  • 折叠

摘要

Abstract

Based on the high⁃strength,low burning rate performance requirements of hydroxy⁃terminated polybutadiene( HTPB) propellant,a new⁃style reinforced and low burning rate dual functional additives was designed and synthesized.Acrylic acid,hydroxy⁃ethyl acrylate,butyl acrylate and triethylamine were used as ingredients to synthesize a new type polyacrylic ester polymer.To prove the synthetic compounds were the designed target compounds,series of characterization were carried out for the structure. The syn⁃thetic target compounds were used to study the influence of additive on mechanical properties of the propellant substrate and the thermal decomposition of AP.The results show that the additives can obviously increase the crosslink density,which can significantly improve propellant substrate mechanical strength.The add of dual functional additives can make the high temperature stage decompo⁃sition of AP reach 380 ℃,which can obviously inhibit the thermal decomposition of AP,so as to reduce propellant burning rate.

关键词

丁羟推进剂/交联/降速/高强度/低燃速

Key words

HTPB propellant/crosslinking/reduce burning rate/high strength/low burning rate

分类

航空航天

引用本文复制引用

黎超华,邓剑如,张习龙,张智威,徐然..丙烯酸类聚合物对丁羟胶片补强/抑制AP热分解研究[J].固体火箭技术,2014,(6):833-837,5.

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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