Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Zuo, Gu"'
Publikováno v:
Journal of Aerospace Technology and Management, Vol 13 (2021)
The design of the magnetic field is crucial to the performance of the hall thruster. This paper investigates the effects of magnetic field on the discharge characteristics of the low-power hall thruster in the method of combining simulation and exper
Externí odkaz:
https://doaj.org/article/62982154c1c2462ea4a1b2d3bf7aeccc
Autor:
Xinwei Chen, Jun Gao, Zuo Gu, Ning Guo, Shangmin Wang, Sanxiang Yang, Yifan Ma, Kai Shi, Hai Geng, Hong Zhang, Yanxu Pu
Publikováno v:
AIP Advances, Vol 11, Iss 11, Pp 115311-115311-10 (2021)
The Faraday probe and cylindrical Langmuir probe were used to characterize the downstream ion and electron spatial evolution of a 300 W class low-power Hall thruster. The time-averaged ion current density, electron energy probability function, plasma
Externí odkaz:
https://doaj.org/article/f54a5b782d5c42dea853981529fd96d3
Publikováno v:
Journal of Aerospace Technology and Management, Vol 13 (2021)
Lifetime is a main factor restraining the application of low-power Hall thruster. Magnetic shielding configuration is regarded as a promising method to prolong the lifespan of Hall thruster. Aiming to demonstrate the feasibility and effectiveness of
Externí odkaz:
https://doaj.org/article/26791fae927e4947a62c8be79e003679
Publikováno v:
Journal of Aerospace Technology and Management, Vol 13, Iss 1, Pp e4521-e4521 (2021)
Journal of Aerospace Technology and Management v.13 2021
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 13, Article number: e4521, Published: 26 NOV 2021
Journal of Aerospace Technology and Management v.13 2021
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 13, Article number: e4521, Published: 26 NOV 2021
The design of the magnetic field is crucial to the performance of the hall thruster. This paper investigates the effects of magnetic field on the discharge characteristics of the low-power hall thruster in the method of combining simulation and exper
Publikováno v:
In Chinese Journal of Aeronautics February 2010 23(1):15-21
Publikováno v:
Journal of Aerospace Technology and Management, Volume: 13, Article number: e2821, Published: 21 MAY 2021
Journal of Aerospace Technology and Management v.13 2021
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Vol 13, Iss 1, Pp e2821-e2821 (2021)
Journal of Aerospace Technology and Management v.13 2021
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Vol 13, Iss 1, Pp e2821-e2821 (2021)
Lifetime is a main factor restraining the application of low-power Hall thruster. Magnetic shielding configuration is regarded as a promising method to prolong the lifespan of Hall thruster. Aiming to demonstrate the feasibility and effectiveness of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::60f59dd4d512c9f6f24b31ac88c1949d
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100323&lng=en&tlng=en
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462021000100323&lng=en&tlng=en
Autor:
Xinwei CHEN, Bijiao HE, Zuo GU, Hai GENG, Ning GUO, Yong ZHAO, Kai SHI, Kai TIAN, Tao CHEN, Yifan MA
Publikováno v:
Plasma Science and Technology. 24:074003
The distribution of the thermal effects of the ion thruster plume are essential for estimating the influence of the thruster plume, improving the layout of the spacecraft, and for the thermal shielding of critical sensitive components. In order to ob
Publikováno v:
Plasma Science and Technology. 25:015504
Low-power Hall thruster (LHT) generally has poor discharge efficiency characteristics due to the large surface-to-volume ratio. Aiming to further refine and improve the performance of 300 W class LHT in terms of thrust and efficiency, and to obtain t
Autor:
Hong Zhang, Wang Shangmin, Sanxiang Yang, Guo Ning, Kai Shi, Hai Geng, Chen Xinwei, Jun Gao, Zuo Gu, Yifan Ma, Yanxu Pu
Publikováno v:
AIP Advances, Vol 11, Iss 11, Pp 115311-115311-10 (2021)
The Faraday probe and cylindrical Langmuir probe were used to characterize the downstream ion and electron spatial evolution of a 300 W class low-power Hall thruster. The time-averaged ion current density, electron energy probability function, plasma
Publikováno v:
Applied Mechanics and Materials. :1106-1114
Nowadays, health care management is driven by informationization and information technologies are widely used in various types of hospitals. Doctors and nurses are the direct users of information technologies for health care management (ITHCM), as we