| タイトル | Spacecraft design optimization using Taguchi analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920004647 |
| 著者（英） | Unal, Resit |
| 著者所属（英） | Old Dominion Univ. |
| 発行日 | 1991-09-01 |
| 言語 | eng |
| 内容記述 | The quality engineering methods of Dr. Genichi Taguchi, employing design of experiments, are important statistical tools for designing high quality systems at reduced cost. The Taguchi method was utilized to study several simultaneous parameter level variations of a lunar aerobrake structure to arrive at the lightest weight configuration. Finite element analysis was used to analyze the unique experimental aerobrake configurations selected by Taguchi method. Important design parameters affecting weight and global buckling were identified and the lowest weight design configuration was selected. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 92N13865 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/129532 |
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