HTPB 推进剂粘结体系的热氧老化及防护研究
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:

武器装备预先研究项目基金(51328050101)


Study on Thermal-oxidative Aging and Protection of HTPB Propellant Binder System
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对海军战术导弹固体火箭发动机端羟基聚丁二烯(hydroxyl-terminated polybutadiene,HTPB)推进剂老 化问题,对HTPB 推进剂粘结体系的老化及防护进行探讨。对丁羟聚氨酯热氧老化机理及影响因素进行介绍,分别 从物理防护与防老剂的化学防护2 方面概述了HTPB 推进剂粘结体系的防护。从老化实验、仪器分析及分子模拟3 方面对老化及防护的研究方法进行了总结,并对分子模拟技术在HTPB 推进剂老化及防护研究的应用前景进行展望。 该研究对未来HTPB 推进剂的防老化及导弹贮存、使用性能的提高有一定指导意义。

    Abstract:

    Aiming at the aging problem of hydroxyl-terminated polybutadiene (HTPB) propellant in solid rocket engine of naval tactical missile, the aging and protection of HTPB propellant binder system were discussed. The thermal-oxidative aging mechanism and influencing factors of HTPB polyurethane were introduced, and the protection of HTPB propellant binder system was summarized from 2 aspects: physical protection and chemical protection of antioxidant. The research methods of aging and protection were summarized from 3 aspects: aging experiment, instrumental analysis and molecular simulation, and the application prospect of molecular simulation technology in the aging and protection of HTPB propellant was prospected. This study has a certain guiding significance for the future anti-aging of HTPB propellant and the improvement of missile storage and use performance.

    参考文献
    相似文献
    引证文献
引用本文

赖帅光. HTPB 推进剂粘结体系的热氧老化及防护研究[J].,2022,41(2).

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2021-10-09
  • 最后修改日期:2021-11-28
  • 录用日期:
  • 在线发布日期: 2022-05-07
  • 出版日期: