Identification and Characterization of Structural Nonlinearities in the Space Shuttle Main Engine
Date Published: 1988-10-01
Paper Number:881526
DOI: 10.4271/881526
Citation:
Panossian, H., "Identification and Characterization of Structural Nonlinearities in the Space Shuttle Main Engine," SAE Technical Paper 881526, 1988, doi:10.4271/881526.
Author(s):
H. V. Panossian - Rockwell International/Rocketdyne Division
Abstract:
Structural 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 (SSME) 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 non-linearities were present.
File Size: 374K
Product Status: In Stock
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