| 注册
首页|期刊导航|固体火箭技术|NEPE推进剂/衬层界面形成机理的分子动力学模拟

NEPE推进剂/衬层界面形成机理的分子动力学模拟

桑丽鹏 冀金成 李慧 杨根 范家珂 武祎晨 叶理欣 朱卫华 陶博文

固体火箭技术2024,Vol.47Issue(6):815-823,9.
固体火箭技术2024,Vol.47Issue(6):815-823,9.DOI:10.7673/j.issn.1006-2793.2024.06.008

NEPE推进剂/衬层界面形成机理的分子动力学模拟

Molecular dynamics simulations on the formation mechanisms of NEPE propellant/liner interface

桑丽鹏 1冀金成 2李慧 2杨根 3范家珂 2武祎晨 3叶理欣 2朱卫华 2陶博文1

作者信息

  • 1. 航天化学能源全国重点实验室,襄阳 441003||湖北航天化学技术研究所,襄阳 441003
  • 2. 南京理工大学 化学与化工学院,南京 210094
  • 3. 湖北航天化学技术研究所,襄阳 441003
  • 折叠

摘要

Abstract

To study the formation mechanisms of NEPE propellant/liner interface,molecular dynamics was used to simulate the formation process of propellant/liner(PEG/N-100/NA/TPB and HTPB/LAP/2,4-TDI/TPB)interface.The results show that the molecules in the NEPE propellant can aggregate and then partly undergo curing reactions.Afterwards,the NEPE propellant system will slowly approach the liner and permeate into it.Then the network structure in the system has been formed by cross-linking curing reactions.Finally the NEPE propellant/liner interface was produced.PEG and NA in the NEPE propellant can not only react with the—NCO groups of N-100,but also react with the—NCO groups on the surface of the liner.Among the five possible interfacial reac-tions,the interfacial PEG/2,4-TDI/TPB reaction has the largest reaction rate constant,followed by the NA/N-100/TPB reactions in the NEPE propellant,and then the interfacial NA/2,4-TDI/TPB reactions,and the PEG/N-100/TPB reactions in the NEPE propel-lant and the interfacial HTPB/N-100/TPB reactions has the smallest rate constant,whose reaction rate constants are comparable.The distribution of the active groups in different regions between the NEPE propellant/liner interface is uneven.

关键词

NEPE推进剂/衬层界面/分子动力学/形成机理/固化反应/反应速率常数

Key words

NEPE propellant/liner interface/molecular dynamics/formation mechanism/curing reaction/reaction rate constant

分类

航空航天

引用本文复制引用

桑丽鹏,冀金成,李慧,杨根,范家珂,武祎晨,叶理欣,朱卫华,陶博文..NEPE推进剂/衬层界面形成机理的分子动力学模拟[J].固体火箭技术,2024,47(6):815-823,9.

基金项目

国家自然基金面上项目(22175059). (22175059)

固体火箭技术

OA北大核心CSTPCD

1006-2793

访问量0
|
下载量0
段落导航相关论文