固体火箭技术2011，Vol.34Issue(4)：497-500,4.
含LLM-105的钝感微烟推进剂能量参数和燃烧特性
Energy parameters and combustion characteristics of insensitive and minimum smoke propellants containing LLM-105
赵凤起 1高红旭 1徐司雨 1仪建华 1裴庆 1郝海霞 1邢晓玲1
作者信息
摘要
Abstract
The compatibility of 2,6-Diamino-3,5-dinitropyrazine-l-oxide (LLM-105) with some main components of composite modified double base ( CMDB) propellant as well as the energy parameters and combustion characteristics of the insensitive and minimum smoke propellants containing LLM-105 were studied. The results show that the binary systems of LLM-105 with the main components of CMDB propellant have good compatibility. The theoretical specific impulse and heat of explosion at constant volume of the propellant decrease gradually by substituting RDX with LLM-105. The burning rates of propellant containing LLM-105 are relatively lower because of the subendothermic process of LLM-105. The combustion characteristics of the propellant can be adjusted by using some combustion catalysts.关键词
LLM-105/钝感/微烟推进剂/能量参数/燃烧性能Key words
LLM-105/insensitivity/minimum smoke propellant/energy parameters/combustion characteristics分类
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赵凤起,高红旭,徐司雨,仪建华,裴庆,郝海霞,邢晓玲..含LLM-105的钝感微烟推进剂能量参数和燃烧特性[J].固体火箭技术,2011,34(4):497-500,4.
