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Lessons Learned From CM-2 Modal Testing and Analysis

Author
Otten, Kim D.
Published
June 2002.
Physical Description
1 electronic document
Additional Creators
Carney, Kelly S., McNelis, Mark E., and Goodnight, Thomas W.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
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.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20020062759.
NAS 1.15:211692.
E-13422.
NASA/TM-2002-211692.
Ninth International Congress on Sound and Vibration; 8-11 Jul. 2002; Orlando, FL; United States.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15422128