| タイトル | Statistical determination of space shuttle component dynamic magnification factors |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730022110 |
| 著者（英） | Lehner, F. |
| 著者所属（英） | Boeing Co. |
| 発行日 | 1973-05-31 |
| 言語 | eng |
| 内容記述 | A method is presented of obtaining vibration design loads for components and brackets. Dynamic Magnification Factors from applicable Saturn/Apollo qualification, reliability, and vibroacoustic tests have been statistically formulated into design nomographs. These design nomographs have been developed for different component and bracket types, mounted on backup structure or rigidly mounted and excited by sinusoidal or random inputs. Typical nomographs are shown. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 73N30842
NASA-CR-124337
D5-17250 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/197885 |
