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《兵工学报(火化工分册)》 1997-01
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The Effect of Composite Propellant Thermal Decomposition Characteristics on it's Fracture Property

Peng Wangda Wong Wujun Cao chuanxin Zhang Ren (National University of Defense Technology,Changsha 410073)  
The effect of AP/HTPB Composite propellant thermal decomposition characteristics on initial change rate of fracture property during aging has been studied in this paper.The results show that initial change rate of fracture energy is inversely proportional to initial decomposition temperature,high temperature decomposition peak temperature and decomposition reaction activation energy at high and low temperature,but it is directly proportional to high and low temperature reaction rate constant.The linear regression accuracy of all these corresponding relation exceeds 0.98.
【CateGory Index】: V512.3
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【Citations】
Chinese Journal Full-text Database 1 Hits
1 Peng Wangda Zhang Ren ZhuHui Zhu Huitian Duli (National Univesity of Defense Technology,Changsha,Hunan 410073);Investigation on AP/HTPB Propellant Fracure Energies[J];固体火箭技术;1993-04
【Co-citations】
Chinese Journal Full-text Database 1 Hits
1 Peng Wangda Wong Wujun Cao chuanxin Zhang Ren (National University of Defense Technology,Changsha 410073);The Effect of Composite Propellant Thermal Decomposition Characteristics on it's Fracture Property[J];兵工学报(火化工分册);1997-01
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