日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
マイクロ波放電型イオンエンジンのビーム計測
佐鳥 新國中 均大滝 基之
著者情報
ジャーナル フリー

1998 年 46 巻 534 号 p. 406-412

詳細
抄録

Beam characteristics of a microwave discharge ion thruster were measured by several kinds of beam analyzers for the purpose of comparing its efficiencies with conventional DC discharge ion thrusters. Propellant utilization, ion cost, doubly charged ion fraction, and beam divergence were evaluated with throttling parameters, resulting in thrust efficiency of 64% when the microwave ion thruster was operated at the condition of mass flow rate of 1.6sccm, microwave power of 45W and acceleration voltage of 1.5kV.

著者関連情報
© The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top