| タイトル | International Space Station Electrodynamic Tether Reboost Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19980223479 |
| 著者（英） | Herrmann, M.; Johnson, L. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1998-07-01 |
| 言語 | eng |
| 内容記述 | The International Space Station (ISS) will require periodic reboost due to atmospheric aerodynamic drag. This is nominally achieved through the use of thruster firings by the attached Progress M spacecraft. Many Progress flights to the ISS are required annually. Electrodynamic tethers provide an attractive alternative in that they can provide periodic reboost or continuous drag cancellation using no consumables, propellant, nor conventional propulsion elements. The system could also serve as an emergency backup reboost system used only in the event resupply and reboost are delayed for some reason. |
| NASA分類 | Astronautics (General) |
| レポートNO | NAS 1.15:208538
M-886
NASA/TM-1998-208538 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/228226 |
