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Identification and characterization of structural nonlinearities in the Space Shuttle Main EngineStructural nonlinearities should be considered in the analysis and modeling of mechanical systems for accuracy in predicting dynamic behavior. Moreover, checks for nonlinearity should address the type and class of nonlinearity in the structure and identify the probable cause. A series of experimental modal survey tests were carried out to determine and characterize the structural nonlinearities of the Space Shuttle Main Engine main injector. Different excitation regimes at various amplitudes were utilized to induce vibration and strain, and acceleration measurements were taken at judiciously selected locations. The test results indicated that both stiffness and damping nonlinearities were present.
Document ID
19890040866
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Panossian, H. V.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SAE PAPER 881526
Report Number: SAE PAPER 881526
Accession Number
89A28237
Funding Number(s)
CONTRACT_GRANT: NAS8-40000
Distribution Limits
Public
Copyright
Other

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