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.
Lessons Learned From CM-2 Modal Testing and Analysis
2002
12 pages
Report
Keine Angabe
Englisch
Lessons Learned From CM-2 Modal Testing and Analysis
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