Zobrazeno 1 - 10
of 52
pro vyhledávání: '"Bijiao He"'
Publikováno v:
ACS Omega, Vol 5, Iss 41, Pp 26673-26681 (2020)
Externí odkaz:
https://doaj.org/article/6aa10b5b6c0a445095ff7bc6f93ccee2
Publikováno v:
Machine Learning: Science and Technology, Vol 4, Iss 4, p 045015 (2023)
The Vlasov–Poisson equation is one of the most fundamental models in plasma physics. It has been widely used in areas such as confined plasmas in thermonuclear research and space plasmas in planetary magnetospheres. In this study, we explore the fe
Externí odkaz:
https://doaj.org/article/51e75bc7bb9b498bbe3ad45a16c16aec
Publikováno v:
Aerospace, Vol 9, Iss 11, p 706 (2022)
Chemical and electrical thrusters are generally utilized to control the attitude and orbit of spacecraft in aerospace. When they are firing, the exhaust expands into the vacuum environment, known as the vacuum plume. The plume flow can collide with s
Externí odkaz:
https://doaj.org/article/6aaae434b0b4487dbfda80ee89780d7d
Publikováno v:
AIP Advances, Vol 8, Iss 8, Pp 085027-085027-12 (2018)
A momentum flux measuring instrument (MFMI), which ranges from 1 mN∼300 N, is designed to measure the parameters related to the momentum flux of exhaust plume of attitude and orbit control thrusters covered electric and chemical thrusters. A MFMI w
Externí odkaz:
https://doaj.org/article/e65f37a7a52d493094e21b7bdfd87559
Publikováno v:
Nanoscale; 5/14/2024, Vol. 16 Issue 18, p9123-9135, 13p
Publikováno v:
International Journal of Mechanical Sciences. 245:108088
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::499c84912d521b72dd5db318803c8a60
https://doi.org/10.1016/j.ijmecsci.2022.108088
https://doi.org/10.1016/j.ijmecsci.2022.108088
Publikováno v:
Acta Astronautica. 179:581-593
Electrospray thrusters with small size, high precision specific impulse, low power consumption are the most recommended propulsive equipments for micro-nano satellites. Molecular dynamics simulation is able to be used to predict the fundamental physi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98b459a3b38ac6b2aeca28f65ef52857
https://doi.org/10.1016/j.actaastro.2020.11.018
https://doi.org/10.1016/j.actaastro.2020.11.018
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:1158-1169
Effects from ion thruster plume have long raised concerns. However, little work has systematically analyzed the influencing parameters in the ion thruster plume simulation. This paper analyzes LIPS 200 ion thruster plume simulations about the influen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd63962812211e6c8de77213788b8a74
https://doi.org/10.1177/0954410020967220
https://doi.org/10.1177/0954410020967220
Publikováno v:
ACS Omega, Vol 5, Iss 41, Pp 26673-26681 (2020)
The low-pressure gas in the vacuum plume produced by the chemical thrusters contaminates the spacecraft when adsorbed on the low-temperature surface. To provide theoretical support for further research on gaseous plume pollutants, the adsorption isot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3f29322ba290744994fb00add8827a0c
https://doi.org/10.1021/acsomega.0c03538
https://doi.org/10.1021/acsomega.0c03538
Publikováno v:
SSRN Electronic Journal.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c805e11eb502f45dba54426a432e2683
https://doi.org/10.2139/ssrn.4196489
https://doi.org/10.2139/ssrn.4196489