@inproceedings{oai:jaxa.repo.nii.ac.jp:00005322,
 author = {西山, 和孝 and Nishiyama, Kazutaka},
 book = {宇宙航空研究開発機構特別資料: 大電力化/モジュール化電気推進に関する研究会, JAXA Special Publication},
 month = {Feb},
 note = {大電力化/モジュール化電気推進に関する研究会(2008年10月21日. 東京国際フォーラム). 主催: 宇宙航空研究開発機構. 後援: 無人宇宙実験システム研究開発機構., In order to advance the technology of electron cyclotron resonance (ECR) microwave discharge ion thrusters known as the 'mu' family, we have been developing a 20-cm diameter thruster mu 20 after successful development and flight experiences of an asteroid explorer 'Hayabusa' employing four 10-cm diameter thrusters mu 10. In contrast to the mu 10 whose ion beam current was saturated to 150 mA at higher microwave powers than 30 W, the mu 20 can generate 500 mA ion beam current with 100 W microwave power and 1100 - 1300 V acceleration voltage, yielding beam ion production cost (discharge power per unit beam current) of 200 W/A and thrust of 27 mN thanks to enlargement of the discharge chamber and moderate plasma density below cutoff. The mu 20 will be applied to deep space missions with larger delta-v and more massive spacecraft than Hayabusa., 形態: カラー図版あり, 資料番号: AA0064241005, レポート番号: JAXA-SP-08-013},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {20cmマイクロ波放電式イオンエンジン},
 volume = {JAXA-SP-08-013},
 year = {2009}
}