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《JOurnal of Solid Rocket Technology》 1993-04
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Investigation on AP/HTPB Propellant Fracure Energies

Peng Wangda Zhang Ren ZhuHui Zhu Huitian Duli (National Univesity of Defense Technology,Changsha,Hunan 410073)  
The paper addresses effects of tempreature change,type and content of additivesect.on fracture energies of AP/HTPB Solid propellant.The experimental results provesthat the fracture energies of propellants decrease with the increasing temperature and bord-ing agent can enhance fracture energies of propellant.When adhesion exponent is close toone,propellants show the highest fracture energies.
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【References】
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];;1997-01
【Co-references】
Chinese Journal Full-text Database 1 Hits
1 Zhang Ren; Li Jianhua; Weng Wujun (Department of Material Science and Applied Chemistry,National Univesity of Defence Technology, Changsha, 410073);DEVELOPMENT OF FERROCENE BURNING RATE CATALYSTS[J];JOURNAL OF PROPULSION TECHNOLOGY;1994-03
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