| タイトル | Lessons Learned From CM-2 Modal Testing and Analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020062759 |
| 著者（英） | Otten, Kim D.; Carney, Kelly S.; McNelis, Mark E.; Goodnight, Thomas W. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2002-06-01 |
| 言語 | eng |
| 内容記述 | The Combustion Module-2 (CM-2) is a space experiment that launches on Shuttle mission STS-107 in the SPACEHAB Double Research Module. The CM-2 flight hardware is installed into SPACEHAB single and double racks. The CM-2 flight hardware was vibration tested in the launch configuration to characterize the structure's modal response. Cross-orthogonality between test and analysis mode shapes were used to assess model correlation. Lessons learned for pre-test planning and model verification are discussed. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | NAS 1.15:211692
E-13422
NASA/TM-2002-211692 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/63212 |
