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The Effect of Aluminum and Ammonium Perchlorate Content on Temperature Sensitivity, Mechanical Properties and Performance of HTPB Propellants

机译：高氯酸盐含量对HTPB推进剂温度敏感性，力学性能和性能的影响

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F. Nihal TUuml; ZUuml; N;
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年度 2007
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1. The Effect of Aluminum and Ammonium Perchlorate Content on Temperature Sensitivity, Mechanical Properties and Performance of HTPB Propellants [J] . F. Nihal Tuezuen Transactions of the Japan society for aeronautical and space sciences . 2007,第169期

机译：铝和高氯酸铵含量对HTPB推进剂的温度敏感性，力学性能和性能的影响
2. Effect of Coating of Ammonium Perchlorate with Fluorocarbon on Ballistic and Sensitivity Properties of AP/A1/HTPB Propellant [J] . S. Nandagopal, M. Mehilal, M. A. Tapaswi Propellants, Explosives, Pyrotechnics . 2009,第6期

机译：高氯酸铵涂氟碳对AP / A1 / HTPB推进剂弹道和敏感性的影响
3. Effects of Aluminum and Temperature on the Tensile Mechanical Properties of Lithium‐Perchlorate/Polyvinyl Alcohol‐Based Electrically Controlled Solid Propellants [J] . He Zhicheng, Xia Zhixun, Hu Jianxin, Propellants, Explosives, Pyrotechnics . 2020,第3期

机译：铝和温度对高氯酸锂/聚乙烯醇基电控固体推进剂的抗拉机械性能的影响
4. Investigation of the ballistic and thermomechanical performances of a composite propellant at base of porous ammonium perchlorate [C] . A. MEZROUA, K. KIMECHE, Y. D. TRACHE International Annual Conference of ICT . 2015

机译：高氯酸铵碱基碱基复合推进剂的弹道和热机械性能研究
5. Drop-weight impact initiation of ammonium perchlorate composite solid rocket propellants [D] . Baker, Patrick John 1994

机译：高氯酸铵复合固体火箭推进剂的落锤冲击引发
6. Dynamic Mechanical Response and Damage Mechanism of HTPB Propellant under Impact Loading [O] . Hengning Zhang, Meng Liu, Yinggang Miao, 2020

机译：冲击载荷下HTPB推进剂的动态机械响应及损伤机制
7. Compressive mechanical properties of HTPB propellant at low temperatures and high strain rates [O] . Xiangdong Chen, Jianwei Lai, Xin-long Chang, 2017

机译：HTpB推进剂在低温和高应变速率下的压缩力学性能
8. Thermal Decomposition Characteristics of Orthorhombic Ammonium Perchlorate (o-AP)211 and an 0-AP/HTPB-Based Propellant [R] . Behrens, Minier 1999

机译：正交高氯酸铵（o-ap）211和0-ap / HTpB基推进剂的热分解特性

The Effect of Aluminum and Ammonium Perchlorate Content on Temperature Sensitivity, Mechanical Properties and Performance of HTPB Propellants

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