NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Lessons Learned From CM-2 Modal Testing and AnalysisThe 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.
Document ID
20020062759
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
McNelis, Mark E. (NASA Glenn Research Center Cleveland, OH United States)
Goodnight, Thomas W. (NASA Glenn Research Center Cleveland, OH United States)
Carney, Kelly S. (NASA Glenn Research Center Cleveland, OH United States)
Otten, Kim D. (Analex Corp. Brook Park, OH United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2002
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2002-211692
NAS 1.15:211692
E-13422
Meeting Information
Meeting: Ninth International Congress on Sound and Vibration
Location: Orlando, FL
Country: United States
Start Date: July 8, 2002
End Date: July 11, 2002
Sponsors: NASA Kennedy Space Center, International Inst. of Acoustics and Vibration, University of Central Florida
Funding Number(s)
PROJECT: RTOP 400-31-3A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available