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Differences of thermal decomposition behaviors and combustion properties between CL-20-based propellants and HMX-based solid propellants
Authors:Zhou  Shuiping  Zhou  Xiaoyang  Tang  Gen  Guo  Xiang  Pang  Aimin
Affiliation:1.Science and Technology on Aerospace Chemical Power Laboratory, Hubei Institute of Aerospace Chemical Technology, Xiangyang, 441003, China
;2.The Fourth Academy of China Aerospace Science and Technology Corporation, Xi’an, 710025, China
;
Abstract:Journal of Thermal Analysis and Calorimetry - Differences of thermal decomposition characteristics and combustion properties between CL-20-based propellants and HMX-based propellants were...
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