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芳族降速剂对HMX-CMDB推进剂燃烧性能的影响

巩如楠 程国荣 赵卓安 陈松 刘所恩 廉建彪 张兵 陈锦芳 刘晓璐

含能材料2026,Vol.34Issue(6):691-698,8.
含能材料2026,Vol.34Issue(6):691-698,8.DOI:10.11943/CJEM2026005

芳族降速剂对HMX-CMDB推进剂燃烧性能的影响

Effect of Aromatic Burning Rate Inhibitor on the Combustion Performance of HMX-CMDB Propellants

巩如楠 1程国荣 2赵卓安 3陈松 2刘所恩 2廉建彪 2张兵 2陈锦芳 2刘晓璐2

作者信息

  • 1. 山西北方兴安化学工业有限公司,山西 太原 030008||大连理工大学力学与航空航天学院,辽宁 大连 116024
  • 2. 山西北方兴安化学工业有限公司,山西 太原 030008
  • 3. 中国科学院上海有机化学研究所,上海 200032
  • 折叠

摘要

Abstract

In order to explore the effect of aromatic compounds on the combustion performance of CMDB propellant,2,2'-(pro-pane-1,1-diyl)bis(4-(tert-butyl)phenol)(PDBP)was used to prepare HMX-CMDB propellant,and the combustion performance of HMX-CMDB propellants with different PDBP contents was studied using the target line method.The results showed that with the increase of PDBP content,the burning rate and pressure index of HMX-CMDB propellant significantly decreased.For HMX-CMDB propellant containing 7%PDBP,the burning rate at 16 MPa decreased to 8.55 mm·s-1,and the pressure index de-creased to 0.217.Compared with the sucrose octaacetate(SOA),HMX-CMDB propellant containing the same mass of PDBP ex-hibited almost unchanged burning rate in the low-pressure region(8-10 MPa),a further reduced burning rate in the high-pressure region(12-16 MPa),resulting in a lower pressure index.In addition,after replacing SOA with 1%PDBP,the det-onation heat of HMX-CMDB propellant was reduced by only 20 kJ·kg-1.Based on chemical structure analysis,the mechanism of PDBP's burning rate inhibition effect is as follows:the aromatic molecule decompose to form protons and structurally stable radi-cal molecules with conjugated π bonds,and the active protons can react with the active radicals released from the decomposi-tion of energetic molecules in the HMX-CMDB propellant,forming stable structures that mitigate the autocatalytic effect of free radicals,thereby reducing the burning rate.

关键词

芳族降速剂/HMX-CMDB推进剂/燃烧性能/降速机理

Key words

aromatic burning rate inhibitor/HMX-CMDB propellant/combustion performance/burning rate inhibition mechanism

分类

军事科技

引用本文复制引用

巩如楠,程国荣,赵卓安,陈松,刘所恩,廉建彪,张兵,陈锦芳,刘晓璐..芳族降速剂对HMX-CMDB推进剂燃烧性能的影响[J].含能材料,2026,34(6):691-698,8.

含能材料

1006-9941

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