| タイトル | Avoiding unrealistic overtest by notching the vibration test specification |
| 著者（英） | Hershfeld, D. J. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | The test specifications for spacecraft and components permit test levels to be reduced under a procedure commonly referred to as notching. A summary is provided of the steps required to comply with the notching criterion. Primary structural loads are discussed along with aspect of mathematical modelling of the spacecraft structure, a launch loads analysis, a vibration test loads analysis, and notching methods. It is shown that current, general vibration test specifications are capable of producing unrealistically high spacecraft structural loads. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74A36008 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/452009 |
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