High current electron source capable of instant stable operation
Project/Area Number |
15H05558
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Research Category |
Grant-in-Aid for Young Scientists (A)
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Allocation Type | Single-year Grants |
Research Field |
Aerospace engineering
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Research Institution | University of Tsukuba |
Principal Investigator |
Yokota Shigeru 筑波大学, システム情報系, 准教授 (30545778)
|
Project Period (FY) |
2015-04-01 – 2018-03-31
|
Project Status |
Completed (Fiscal Year 2017)
|
Budget Amount *help |
¥19,240,000 (Direct Cost: ¥14,800,000、Indirect Cost: ¥4,440,000)
Fiscal Year 2017: ¥3,770,000 (Direct Cost: ¥2,900,000、Indirect Cost: ¥870,000)
Fiscal Year 2016: ¥5,850,000 (Direct Cost: ¥4,500,000、Indirect Cost: ¥1,350,000)
Fiscal Year 2015: ¥9,620,000 (Direct Cost: ¥7,400,000、Indirect Cost: ¥2,220,000)
|
Keywords | 宇宙推進 / 電気推進 / ホローカソード / 電子源 / 大電流電子源 |
Outline of Final Research Achievements |
A criterion to stabilize the operation of a hollow cathode for high power electric propulsion of space crafts is obtained. First, we found that the hollow cathode operation is unstable when the propellant flow rate is low and the electron extract current is high. Second, we observed the plasma in the hollow cathode using probes. As a result, we found that the forcible electron collection causes the unsteady operation. Finally, we developed a new hollow cathode under the stabilization criteria and demonstrated that the hollow cathode operation became stabilized instantly.
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Report
(4 results)
Research Products
(13 results)
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[Presentation] 100A Hollow Cathode2015
Author(s)
S. Yokota, K. Kojima, T. Kimura, H. Kataoka, A. Sasoh
Organizer
30th International Electric Propulsion Conference
Place of Presentation
神戸コンベンションセンター(兵庫県神戸市)
Year and Date
2015-07-06
Related Report
Int'l Joint Research