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| Study of General Rule of Thermal Stability of HTPB Propellant |
| Received:October 08, 2010 Revised:June 15, 2011 |
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| DOI： |
| KeyWord:HTPB propellant thermal stability aging rule |
| Author | Institution |
| YANG Wan-jun |
1. No.59 Research Institute of China Ordnance Industry， Chongqing ， China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection， Chongqing ， China |
| WEI Xiao-qin |
1. No.59 Research Institute of China Ordnance Industry， Chongqing ， China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection， Chongqing ， China |
| HUANG Wen-ming |
1. No.59 Research Institute of China Ordnance Industry， Chongqing ， China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection， Chongqing ， China |
| YU Shu-hua |
1. No.59 Research Institute of China Ordnance Industry， Chongqing ， China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection， Chongqing ， China |
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| Abstract: |
| The general rule of thermal stability of HTPB propellants with 4 different ingredients was studied through thermal ageing test in different temperature by using degreasing method. It was concluded that HTPB propellants of different ingredients have similar characteristic decomposing rule and thermal stability rule. The purpose was to provide reference for pre-evaluating storage performance of HTPB propellant. |
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