Performance characteristics according to the radial position of gas distributor holes in a low-power cylindrical Hall thruster

2016 ◽  
Vol 23 (8) ◽  
pp. 083514 ◽  
Author(s):  
Yuanyuan Gao ◽  
Hui Liu ◽  
Peng Hu ◽  
Hongyan Huang ◽  
Daren Yu
2017 ◽  
Vol 24 (6) ◽  
pp. 063518 ◽  
Author(s):  
Yuanyuan Gao ◽  
Hui Liu ◽  
Peng Hu ◽  
Hongyan Huang ◽  
Daren Yu

1997 ◽  
Author(s):  
W. Hargus, Jr. ◽  
R. Cedolin ◽  
N. Meezan ◽  
M. Cappelli ◽  
W. Hargus, Jr. ◽  
...  

2021 ◽  
Vol 1754 (1) ◽  
pp. 012167
Author(s):  
JIA Hangyu ◽  
QU Chengzhi ◽  
JI Yuhui ◽  
ZHOU Guangrui ◽  
WU Suliang
Keyword(s):  

Author(s):  
Guangchuan ZHANG ◽  
Junxue REN ◽  
Wei LIANG ◽  
Ning OUYANG ◽  
Chao LU ◽  
...  

Vacuum ◽  
2013 ◽  
Vol 88 ◽  
pp. 63-69 ◽  
Author(s):  
Tomoyuki Ikeda ◽  
Kazuya Togawa ◽  
Hirokazu Tahara ◽  
Yosuke Watanabe

1999 ◽  
Vol 34 (11) ◽  
pp. 1446-1453 ◽  
Author(s):  
Jong-Woo Park ◽  
Yun-Gi Kim ◽  
Il-Kwon Kim ◽  
Kyu-Charn Park ◽  
Kyu-Chan Lee ◽  
...  

2014 ◽  
Vol 1016 ◽  
pp. 400-404
Author(s):  
Luciano Magno Fragola Barbosa ◽  
Paulo H. Iscold A. de Oliveira

This work presents a comparative study of aerodynamic and performance characteristics of relevant examples of low speed aircraft that have been built and flown between 1890 and 1990. As speed is related to aircraft mass and wing loading and power, the aircraft analyzed present low weight, low wing loading and low power. To generate this study a set of tools have been developed, which are specifically aimed to slow and light aircraft. One additional goal of the study is to obtain a consistent reference data basis - by using the developed tools to analyze existing aircraft - prior to use these tools in new designs with the features of low speed, low wing loading and low power.


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