| タイトル | Magnetic suspension and balance system advanced study, phase 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910004150 |
| 著者（英） | Abdelsalam, M. K.; Eyssa, Y. M.; Mcintosh, G. E.; Boom, R. W. |
| 著者所属（英） | Madison Magnetics, Inc. |
| 発行日 | 1990-11-01 |
| 言語 | eng |
| 内容記述 | The design improvements for the system encompass 14 or 18 external superconductive coils mounted on a 8 x 8 foot wind tunnel, a superconductive model core magnet on a holmium mandrel to fit an F-16 model, model wings of permanent magnet material Nd2Fe14B, and fiber glass epoxy structure. The Magnetic Suspension and Balance System (MSBS) advanced design is confirmed by the successful construction and test of a full size superconductive model core solenoid with holmium mandrel. The solenoid is 75 cm long and 12.6 cm in diameter and produces 6.1 tesla for a hold time of 47 minutes. An integrated coil system design of a new compact configuration without specific coils for roll or pitch shows promise of simplicity; magnet reductions of 30 percent compared to the most recent 1985 design are possible. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 91N13463
NASA-CR-4327
NAS 1.26:4327 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/135239 |
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