Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Yohei Mito"'
Autor:
Hirokazu Tahara, Masato Nishida, Yohei Mito, Tomoyuki Ikeda, Tsuyoshi Kawamura, Taisuke Kagota
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The operational range of Hall thrusters will be hoped to be expanded for future orbital transfer vehicle and Mars exploration, i.e. for in-space propulsion. In this study, both smallsize 1-kW-class SPT and TAL Hall thrusters were operated with higher
Publikováno v:
2012 International Conference on Renewable Energy Research and Applications (ICRERA).
High-power and high-specific-impulse characteristics of Hall thrusters were experimentally studied. Input power and specific impulse reached above 5 kW and 3000 sec, respectively. As a result, the specific impulse and the thrust efficiency were 3202
Publikováno v:
2012 International Conference on Renewable Energy Research and Applications (ICRERA).
Development of Hall thrusters for nano, small and low-power satellites below 100W is expected. In lowering Hall thruster power, the cylindrical-type Hall thruster is more advantage than conventional coaxial-type Hall thrusters. In this study, a very
Publikováno v:
The Proceedings of Conference of Kansai Branch. :8-2