火炸药学报2025，Vol.48Issue(12)：1163-1167,5.DOI:10.14077/j.issn.1007-7812.202506013
低燃速HMX改性双基推进剂的燃烧性能
Study on the Combustion Performance of Low Burning Rate HMX Modified Double-base Propellants
摘要
Abstract
To meet the continuous development requirements of weapons and equipments,HMX-modified double-base propel-lants with low burning rate were developed to improve the endurance time and stealth penetration capability of missile engines.The"burning rate-target line method"was used to study the effects of triacetin(GTA),combustion catalytic system(organic combustion catalytic system Pb/Cu/CB,inorganic combustion catalytic system Pb/Cu/CB),and different combustion catalyst ratios on the combustion performance of HMX-based high solid content composite modified double-base propellant(HMX-CMDB)of screw extrusion process.The results indicate that GTA can effectively reduce the burning rate and pressure index of HMX-CMDB.The Pb/Cu/CB outperforms the Pb/Cu/CB in improving the combustion performance of low burning rate HMX-CMDB.When conbining GTA with Pb/Cu/CB,the burning rate of HMX-CMDB reaches 9.25mm/s at 10MPa,and the pres-sure index is 0.336 at 7-12MPa.The theoretical specific impulse calculated for the formulation is 247.13s,with a heat of explosion of 4 788J/g,meeting the technical specifications required for high-energy low-burning-rate propellants.关键词
物理化学/低燃速/HMX/改性双基推进剂/三乙酸甘油酯/压强指数/降速剂/燃速催化剂Key words
physical chemistry/low burning rate/HMX/modified double-base propellants/triacetin/pressure index/burning rate inhibitors/burning-rate catalyst分类
军事科技引用本文复制引用
陈黄,袁熙,张国辉,王康,赵美玲,张丽荣,陈松..低燃速HMX改性双基推进剂的燃烧性能[J].火炸药学报,2025,48(12):1163-1167,5.基金项目
火炸药基础产品创新科研项目 （）
