@article{oai:jaxa.repo.nii.ac.jp:00032588,
 author = {バンクス, P.M. and ウィリアムソン, P.R. and 小山, 孝一郎 and BANKS, P.M. and Williamson, P.R. and OYAMA, K.I},
 issue = {4_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Nov},
 note = {プラズマ物理,宇宙空間物理において多くの興味ある実験を重力勾配を利用してShuttle上空10 km～30 kmに位置させたSubsatelliteによってなす事ができる.この実験に含まれる三つの主な物理的過程はSubsatelliteにおける電子の捕集,Tetherが地球磁場を切る事によって生じる電磁波動の励起,および電子銃によるオービタからの電子の放出である.ここでは,Subsatelliteおよびオービタとまわりの電離層プラズマとの境界に存在する多くの電気的なプロセスに重点をおいて,Shuttle Electrodynamic Tether SystemとよばれるこのSystemについて述べる., Many novel electrodynamic and space plasma physics experiments can be done from the space shuttle using a gravity gradient stabilized sub-satellite tethered 10 to 30 Km above the Orbiter via a long, conducting wire. The three principal physical processes involved include electron collection at the sub-satellite, the generation of a Large emf through the orbital motion of the wire across geomagnetic field lines, and the active ejection of electrons from the Orbiter by means of an electron emitter. This system, called the Shuttle Electrodynamic Tether System (SETS), is described in this paper with emphasis on the many electrical processes acting, including those present at the sub-satellite and Orbiter interfaces with the ambient ionosphere plasma. An electrical circuit analogy is presented with discussion of several possible operating modes., 資料番号: SA0125914000},
 pages = {1237--1253},
 title = {<論文>Shuttle Electrodynamic Tether System(SETS)の電気的特性について},
 volume = {16},
 year = {1980}
}