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科研机构

北京航空航天大学 [6]

清华大学 [4]

数学与系统科学研究院 [2]

西安交通大学 [1]

福建物质结构研究所 [1]

大连化学物理研究所 [1]

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期刊论文 [12]

会议论文 [7]

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物理化学 [1]

物理有机化学 [1]

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浏览/检索结果: 共19条，第1-10条

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	The influence of inner material with different average thermal conductivity on the performance of whole insulation system for liquid hydrogen on orbit storage 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 18, 页码: 10913-10923 作者: Wang, Ping; Ji, Lun; Yuan, Jing; An, Zhenguo; Yan, Kaiqi 收藏 \| 浏览/下载：110/0 \| 提交时间：2021/04/26 Passive insulation system Inner material Multilayer insulation Thermal insulation performance Liquid hydrogen on orbit storage
	Modeling and optimization of composite thermal insulation system with HGMs and VDMLI for liquid hydrogen on orbit storage 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 11, 页码: 7088-7097 作者: Wang, Ping; Ji, Lun; Yuan, Jing; An, Zhenguo; Yan, Kaiqi 收藏 \| 浏览/下载：17/0 \| 提交时间：2020/05/24 Liquid hydrogen on orbit storage Hollow glass microspheres Variable density multilayer insulation Optimal configuration Thermal insulation performance
	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
	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
	Effects of deformation on the burning behavior of solid propellants 期刊论文 INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS, 2017, 卷号: 9, 期号: 2 作者: Wang, B.; Peng, H.; Chen, Y. X. 收藏 \| 浏览/下载：2/0 \| 提交时间：2019/12/05 Burning rate strain binder fraction tensile strength composite
	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
	Theoretical study of thermite reaction enthalpy for metal composite oxides of ferrite series 期刊论文 Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2016, 卷号: 39, 期号: [db:dc_citation_issue] 作者: Wang, Meng-Jie; Chang, Chun-Ran; Xu, Kang-Zhen; Ma, Hai-Xia; Zhao, Feng-Qi 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/02 Density functional theory DFT Metal composite oxides Quantum chemistry Thermite reaction

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