| タイトル | Dynamic analysis for shuttle design verification |
| 著者（英） | Rheinfurth, M. H.; Fralich, R. W.; Green, C. E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1972-07-01 |
| 言語 | eng |
| 内容記述 | Two approaches that are used for determining the modes and frequencies of space shuttle structures are discussed. The first method, direct numerical analysis, involves finite element mathematical modeling of the space shuttle structure in order to use computer programs for dynamic structural analysis. The second method utilizes modal-coupling techniques of experimental verification made by vibrating only spacecraft components and by deducing modes and frequencies of the complete vehicle from results obtained in the component tests. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 72N30874 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/533761 |
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