摘要
用高压DSC研究了高能改性双基推进剂AlRDXCMDB在2~6MPa下的热分解行为及其与相应压强下燃速的关系,结果表明,不同压强下燃速的增值与DSC上两峰温差(RDX分解峰温与双基粘合剂峰温之差)的增值有线性关系。
The thermal decomposition behavior of Al RDX CMDB propellant and the correlation between it and the burning rate were investigated by high pressure DSC at 2~6MPa.The results show that the increments of burning rate at various pressures are linear with the increments of the difference between RDX decomposition peak temperature and double base binder peak temperature.
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第3期35-39,共5页
Journal of Solid Rocket Technology
关键词
双基推进剂
差热分析
燃烧性能
高压热分解
Modified double base propellant Propellant combustion Differential thermal analysis