@article{oai:jaxa.repo.nii.ac.jp:00032091,
 author = {平尾, 邦雄 and 小山, 孝一郎 and HIRAO, Kunio and OYAMA, Kohichiro},
 issue = {4},
 journal = {東京大学宇宙航空研究所報告},
 month = {Oct},
 note = {計測器をできるだけ小型に,より精度のよい回路に改良することは,飛しょう体搭載の場合には特に考えねばならないし,また,テレメータにより送信されてきた信号を,できるだけすみやかに,処理できるような回路構成を行なうことも必要である.本論文では,従来の電子温度測定器を上述の要求をみたすように改良した結果を報告する., One of the methods of electron temperature measurements as an application of resonance probe theory has been presented by one of the authors. However, on account of a single probe, detected signal includes V^^→×B^^→ voltage induced by geomagnetic field and rocket velocity as well as other noise. In order to get rid of the effects of geomagnetic field and rocket velocity and random noise, an improved type of electron temperature probe is tested. At the same time, the instrument was made smaller to some extent., 資料番号: SA0125196000},
 pages = {495--505},
 title = {電子温度測定器の改良,小型化について},
 volume = {5},
 year = {1969}
}