Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
抄録（英）
In this study, by electromagnetic analysis we found that Non-50 Ω line, the impedance of which isn't 50 Ω , in the miniature microwave discharge ion thruster Ω 1 was the resonator and microwave power inside the thruster could be formulated using S-parameters of non-50 Ω line. Measuring microwave absorbance by plasma, this formulation was verified and the possibility of estimating microwave absorbance from the shape of the resonator without experiments was suggested.
内容記述
形態: カラー図版あり
形態: PDF
内容記述（英）
Physical characteristics: Original contains color illustrations
Physical characteristics: PDF
マイクロ波放電式小型イオンスラスタにおけるプラズマのマイクロ波吸収率の測定
61856147.pdf
(1.19MB)
