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北京航空航天大学 [15]

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清华大学 [5]

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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：111/0 \| 提交时间：2021/04/26 Passive insulation system Inner material Multilayer insulation Thermal insulation performance Liquid hydrogen on orbit storage
	Heat Transfer Behaviors on Combinational Insulation of Spray-On Foam and Variable Density Multilayer for Cryogenic Propellant Tanks 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 4 作者: Chen, Shuping; Jin, Shufeng; Liu, Dan; Yao, Shuting; Wang, Lihong 收藏 \| 浏览/下载：6/0 \| 提交时间：2019/11/15 Cryogenics Enthalpy Heat conduction Heat flux Heat resistance Multilayers Propellants Space research Spacecraft propulsion Boundary temperature Cryogenic propellant tanks Heat transfer behavior Heat transfer calculations Long duration missions Multi-layer insulation Solid heat conductions Spray on foam insulation
	Oxidation of Catocene in AP/Catocene Mixture at Low Temperature 期刊论文 PROPELLANTS EXPLOSIVES PYROTECHNICS, 2019, 卷号: 44, 期号: 4, 页码: 513-518 作者: Jiang, Ben-Z.; Wang, Ting-P. 收藏 \| 浏览/下载：19/0 \| 提交时间：2019/06/20 AP Catocene Oxidation Products Oxidation mechanism
	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
	金属配位自燃离子液体的合成及表征学位论文 : 中国科学院研究生院, 2018 作者: 章泽筠收藏 \| 浏览/下载：73/0 \| 提交时间：2019/03/29 推进剂,自燃离子液体,点火延迟时间,过渡金属
	Active Vibration Control of Flexible Satellites Using Solid Propellant Microthruster Array 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 31 作者: Yang, Bo; Fan, Zichen; Miao, Jun; Long, Jun; Liu, Xuhui 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/30 Actuators Asymptotic stability Digital control systems Discrete time control systems Equations of state Flexible structures Piezoelectric actuators Propellants Riccati equations Solid propellants Spacecraft propulsion Uncertainty analysis Active vibration controls Flexible satellites Global asymptotic stability Low-frequency vibration Monte Carlo approach Saturation problems State-dependent Riccati equation Switching strategies Controllers
	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
	A high-precision attitude coordinated control method using MEMS thruster for pico- and nano-satellite [一种皮纳卫星MEMS固体微推力器阵列联合姿态控制的高精度方法] 期刊论文 Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2018, 卷号: 44, 页码: 1378-1386 作者: Yang, B.; Li, J. 收藏 \| 浏览/下载：2/0 \| 提交时间：2019/12/30 Actuators Attitude control Costs Flywheels Global optimization Nanosatellites Numerical methods Sliding mode control Solid propellants Spacecraft propulsion Wheels Allocation matrices Attitude stability Co-ordinated control High-precision Lyapunov stability Microthruster Optimal switching Terminal sliding mode Monte Carlo methods

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