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北京航空航天大学空间与环境学院导师教师师资介绍简介-汤海滨

本站小编 Free考研考试/2020-04-24

教授\博士生导师
电子邮箱:thb@buaa.edu.cn
办公地点:北航新主楼B座916
办公电话:**
空间等离子体电推进实验室:http://jlpp.buaa.edu.cn


基本情况
Beihang University Nov. 2001 – present
Professor, School of Space and Environment(Sep. 2017 – present)
Professor, School of Astronautics (Sep.2011 – Aug. 2017)
Associate Professor, School of Astronautics(Jul. 2004 – Aug. 2011)
Lecturer, School of Astronautics (Nov. 2003– Jun. 2004)
Postdoctoral, School of Astronautics (Nov.2001 – Oct. 2003)


研究方向
Electric (Plasma) propulsion,Micro-propulsion, Advanced Space Propulsion
Numerical modeling and Experiment on SpacePropulsion Systems
Plasma, Fluid, and Space Physics

科研课题
The National Natural Science Foundation
Projects of the National High TechnologyResearch and Development Program
The Fundamental Research Program
The State Key Lab Foundations and CNSA
Pre-research Projects

主讲课程
Advanced Technology of Measurement and Test(senior level)
Electric Propulsion and Plasmas Propulsion(graduate level)

近期学术著作及文章
1. Thomas M. York, Haibin Tang, Introduction to Plasmasand Plasma Dynamics, 2015, Published by Elsevier Inc
2. Zhe Zhang, Haibin Tang, Zun Zhang, Joseph Wang,and Shuai Cao, A retarding potential analyzer design for keV-level ion thrusterbeams, Review of Scientific Instruments, 87(12), 123510 (2016)
3. Zun Zhang, Haibin Tang, Junxue Ren, Zhe Zhangand Joseph Wang, Calibrating Ion Density Profile Measurements in Ion ThrusterBeam Plasma, Review of Scientific Instruments, 87(11),113502 (2016)
4. Zun Zhang, Haibin Tang, Mengdi Kong, Zhe Zhang,and Junxue Ren, Electron temperature measurement in Maxwellian non-isothermalbeam plasma of an ion thruster, Review of Scientific Instruments, 86(2), 023506(2015)
5. Hai-Bin Tang, Xin-Ai Zhang, Yu Liu, Hai-XingWang, Yi-Bai Wang, Numerical and Experimental Study of a 1‐kW Hydrazine Engineering DesignModel Arcjet Thruster, Journal of Aerospace Engineering, 27(1),2014, 16-25
6. Jiao Cheng, Hai-Bin Tang, and Thomas M. York, Energyconversion and transfer for plasmas in a magnetic expansion configuration, Physicsof Plasmas, 21(6),063501 (2014)
7. Min Li, Hai-Bin Tang, Jun-Xue Ren, and Thomas M.York, Modeling of plasma processes in the slowly diverging magnetic fields atthe exit of an applied-field magnetoplasmadynamic thruster, Physics of Plasmas20, 103502 (2013)
8. Hai-Bin Tang, Jiao Cheng, Chang Liu, and ThomasM. York, Study of applied magnetic field magnetoplasmadynamic thrusters withparticle-in-cell and Monte Carlo collision. II. Investigation of accelerationmechanisms, Physics of Plasmas 19, 073108 (2012)
9. Hai-Bin Tang, Jiao Cheng, Chang Liu, and ThomasM. York, Study of applied magnetic field magnetoplasmadynamic thrusters withparticle-in-cell code with Monte Carlo collision. I. Computation methods andphysical processes, Physics of Plasmas 19, 073107 (2012)
10. Hai-Bin Tang , Chao-Jin Qin, Yu Liu, “Characterization of the colloid thruster beams andplumes”, Journal ofAerosol Science.42(2011) 114-126
11. Tang H, Shi C, Zhang X, Zhang Z, Cheng J, Pulsed thrust measurementsusing electromagnetic calibration techniques, Review of ScientificInstruments, 82, 035118 (2011)
12. Tang HB, Zhang XA, Liu Y, Wang HX, Shi CB, Cai, B, ExperimentalStudy of Startup Characteristics and Performance of a Low-Power Arcjet, Journalof Propulsion and Power, 27(1), 2011, 218-226
13. Hai-bin Tang, Xin-ai Zhang, Yu Liu, Hai-xing Wang, Yan Shen,Performance and preliminary life test of a low power hydrazine engineeringdesign model arcjet, Aerospace Science and Technology, 15(7), 2011, 577–588


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