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[期刊论文] 作者:Peng Zheng,Haibin Tang,Botong, 来源:黑龙江科技学院学报 年份:2019
为探究吕家坨井田地质构造格局,根据钻孔勘探资料,采用分形理论和趋势面分析方法,研究了井田7...
[期刊论文] 作者:Zun ZHANG,Zhe ZHANG,Haibin TANG,Jiting OUYANG, 来源:等离子体科学和技术(英文版) 年份:2021
The characteristics of electrons play a dominant role in determining the ionization and acceleration processes of plasmas.Compared with electrostatic diagnostic...
[期刊论文] 作者:Haibin TANG,Daren YU,Haixing WANG,Weizong WANG, 来源:等离子体科学和技术(英文版) 年份:2021
The development of electric propulsion has taken decades and in fact,began flight testing as early as the 1960s.However,it was initially slow to develop as an alternative to chemical propulsion systems due to the lack of available on-board ......
[期刊论文] 作者:Guangchuan ZHANG,Junxue REN,Wei LIANG,Ning OUYANG,Chao LU,Haibin TANG, 来源:中国航空学报(英文版) 年份:2020
The coupling region of a Hall thruster with a hollow cathode is the region between the cathode and the thruster plume. The characteristics of plasma in that reg...
[期刊论文] 作者:Yifeng FU,Cheng ZHOU,Peng WU,Zhongkai ZHANG,Zun ZHANG,Haibin TANG, 来源:等离子体科学和技术(英文版) 年份:2021
In this work,a zero-dimensional plasma model for self-field magnetoplasmadynamic thrusters(SF-MPDTs) is proposed,which is based on the ion-number balance equation and energy balance equation,and can calculate the average electron temperatur......
[期刊论文] 作者:Peng WU,Yibai WANG,Yong LI,Baojun WANG,Kaiyu ZHANG,Haibin TANG,Jinbin CAO, 来源:等离子体科学和技术(英文版) 年份:2004
Erosion can influence cathode life,and is thus considered to be one of the main factors limiting the application of applied-field magnetoplasmadynamic thrusters...
[期刊论文] 作者:Wei Jinju,Deng Zhanyun,Huang Chenghua,Huang Weihua,Yan Meixin,Liu Haibin,Tang Hongqin,, 来源:Plant Diseases and Pests 年份:2013
[Objective] The purpose was to understand species and occurrence status of major fugal diseases in sugarcane cultivation areas of Guangxi in China, so as to pro...
[期刊论文] 作者:Zhongkai ZHANG,Guanrong HANG,Jiayun QI,Zun ZHANG,Zhe ZHANG,Jiubin LIU,Wenjiang YANG,Haibin TANG, 来源:等离子体科学和技术(英文版) 年份:2021
In this work,a force measurement system is proposed to measure the thrust of plasma micro-thruster with thrust magnitude ranging from sub-micro-Newtons to hundreds micro-Newtons.The thrust measurement system uses an elastic torsional pendul......
[期刊论文] 作者:Fawzi DERKAOUI,Zhaoxin LIU,Wenjiang YANG,Yu QIN,Kunlong WU,Peng ZHAO,Juzhuang YAN,Junxue REN,Haibin TANG, 来源:等离子体科学和技术(英文版) 年份:2021
A high temperature superconducting (HTS) magnetically levitated testbed has been developed for the steady thrust measurement of miniature ion electrospray thruster.The structure of the testbed mainly consists of an HTS composite bearing,a m......
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