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北京航空航天大学 [9]

清华大学 [5]

西安交通大学 [1]

上海有机化学研究所 [1]

武汉物理与数学研究所 [1]

山东大学 [1]

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期刊论文 [12]

会议论文 [7]

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金属有机化学 [1]

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浏览/检索结果: 共19条，第1-10条

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	Effects of Plasticizers, Antioxidants and Burning Rate Modifiers on Aging Performance of the HTPB/ HMDI Composite Solid Propellant 期刊论文 Hanneng Cailiao/Chinese Journal of Energetic Materials, 2019, 卷号: 27, 页码: 21-27 作者: Enew, A.M.; Abadir, E.; Elmarsafy, S.; Elsharkawy, K.K. 收藏 \| 浏览/下载：9/0 \| 提交时间：2019/12/30 Antioxidants Copper compounds HTPB propellants Iron oxides Plasticizers Polybutadienes Reinforced plastics Solvents Accelerated aging Aging performance Ballistic performance Burning rate modifier Composite solid propellant Diisocyanates Hydroxyl terminated polybutadienes P-phenylene diamines Composite propellants
	Improving the Mechanical Properties of Glycidyl Azide Polymeric Matrix Used in Composite Solid Rocket Propellant by Adding Advanced Cross-Linker 期刊论文 ZEITSCHRIFT FUR ANORGANISCHE UND ALLGEMEINE CHEMIE, 2019, 卷号: 645, 页码: 551-557 作者: Boshra, Islam K.; Elbeih, Ahmed; Mostafa, Hosam E. 收藏 \| 浏览/下载：2/0 \| 提交时间：2019/12/30 Glycidyl azide polymer (GAP) Hydroxyl terminated polybutadiene (HTPB) Cross-linker Mechanical properties
	Novel method for measuring primary and secondary smoke density of reduced HCl exhaust composite solid rocket propellant (CSRP) based on nitramine energetic material 期刊论文 SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2019, 卷号: 80, 页码: 121-129 作者: Abd Elall, Ali M.; Lin, Guo 收藏 \| 浏览/下载：5/0 \| 提交时间：2019/12/30 conventional scavenger non-chlorine and neutralized propellant smoke density
	Composite solid rocket propellant based on GAP polyurethane matrix with different plasticizers 会议论文 18th International Conference on Aerospace Sciences and Aviation Technology, ASAT 2019, Kobry Elkobbah, Cairo, Egypt, 2019-04-09 作者: Boshra, Islam K.; Elbeih, Ahmed; Mostafa, Hosam E. 收藏 \| 浏览/下载：2/0 \| 提交时间：2019/12/30
	Effects of magnesium-based hydrogen storage materials on the thermal decomposition, burning rate, and explosive heat of ammonium perchlorate-based composite solid propellant 期刊论文 Journal of Hazardous Materials, 2018, 卷号: 342, 页码: 477-481 作者: Liu, Leili; Li, Jie; Zhang, Lingyao; Tian, Siyu 收藏 \| 浏览/下载：4/0 \| 提交时间：2019/12/11
	Parameters affecting the erosive burning of solid rocket motor 会议论文 MATEC Web of Conferences, 2017-11-28 作者: Abdelaziz, A.; Guozhu, L.; Elsayed, A. 收藏 \| 浏览/下载：1/0 \| 提交时间：2019/12/30 Product design Propellants Rocket engines Rockets Burning rate Combustion phenomena Erosive burning High velocity Motor design Pressure-time curves Propellant surfaces Solid rocket motors Composite propellants
	Effect of bonding agent production materials on the mechanical properties of composite solid rocket propellant 会议论文 MATEC Web of Conferences 作者: Elall, A.M.A.; Lin, G. 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Adhesives Chlorine compounds Composite propellants Copper compounds Manufacture Rockets Solid propellants Strain Composite solid propellant Effect of solvents Environmental conditions Interfacial interaction Loading condition Polar solvents Properties of composites Solid particles Mechanical properties
	A Review on the Application and Usefulness of Metal Nanosized Particles in Solid Rocket Propellants 会议论文 2018 3rd International Conference on Smart and Sustainable Technologies, SpliTech 2018 作者: Ghedjatti, I.; Shiwei, Y.; Haixing, W. 收藏 \| 浏览/下载：5/0 \| 提交时间：2019/12/30 Composite propellants Decomposition Metals Nanomagnetics Nanostructured materials Pyrolysis Rockets Solid propellants Burning rate Catalytic properties Composite solid propellant Energetic nanomaterials Metal particle Micron-sized particles Performance enhancements Solid rocket propellant Nanocatalysts
	Study of cooldown thermal loading effect on the bore deformation of viscoelastic solid propellant grain 会议论文 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, 2017-07-10 作者: Adel, W.M.; Liang, G.-Z. 收藏 \| 浏览/下载：7/0 \| 提交时间：2019/12/30 Composite propellants Propellants Propulsion Rocket engines Solid propellants Strain Stress relaxation Testing Viscoelasticity Composite solid propellant Environmental temperature changes Experimental approaches Low firing temperature Nonlinear visco-elastic Nonlinear viscoelastic material Thermo-structural analysis Time-temperature superposition principles Finite element method
	Developing a viscoelastic relaxation model for AP-HTPB composite solid propellant based on experimental data 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, 2017-03-06 作者: Adel, W.M.; Liang, G.-Z. 收藏 \| 浏览/下载：1/0 \| 提交时间：2019/12/30 Composite propellants HTPB propellants Inorganic compounds Least squares approximations Polybutadienes Propellants Rocket engines Solid propellants Spacecraft Spacecraft propulsion Strain rate Stress relaxation Tensile testing Viscoelasticity 3D finite element model Composite solid propellant Hydroxyl terminated polybutadienes Stress relaxation data Stress relaxation tests Structural integrity analysis Time dependent behavior Viscoelastic relaxation Finite element method

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