固体火箭技术2016，Vol.39Issue(1)：78-82,5.DOI:10.7673/j.issn.1006-2793.2016.01.014
改性双基推进剂的热安全性研究
Thermal safety analysis of CMDB propellant
陈晨 1路桂娥 2江劲勇 3葛强 4王韶光 3贾昊楠4
作者信息
- 1. 中国白城兵器试验中心，白城 137001
- 2. 军械工程学院，石家庄 050000
- 3. 军械工程学院，石家庄 050000
- 4. 军械技术研究所，石家庄 050000
- 折叠
摘要
Abstract
To evaluate thermal safety of a CMDB propellant effectively,the thermal decomposition and self-ignition procedure of GHT propellant were studied by a differential scanning calorimetry ( DSC) and a set-up of thermal self-ignition. Curves of thermal decomposition at different rate,time to self-ignition and curves of thermal self-ignition of GHT propellant at different aging time were obtained respectively.By calculating and analyzing the data,thermal decomposition kinetics parameters,thermal safety parameters and self ignition parameters.The studies have revealed that,increasing environment temperature and time of storage make thermal safety of GHT propellant worse.关键词
改性双基推进剂/GHT推进剂/热安全性/热分解/热自燃Key words
CMDB/GHT propellant/thermal safety/thermal decomposition/thermal self-ignition分类
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陈晨,路桂娥,江劲勇,葛强,王韶光,贾昊楠..改性双基推进剂的热安全性研究[J].固体火箭技术,2016,39(1):78-82,5.
