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Engineering evaluation of SSME dynamic data from engine tests and SSV flightsAn engineering evaluation of dynamic data from SSME hot firing tests and SSV flights is summarized. The basic objective of the study is to provide analyses of vibration, strain and dynamic pressure measurements in support of MSFC performance and reliability improvement programs. A brief description of the SSME test program is given and a typical test evaluation cycle reviewed. Data banks generated to characterize SSME component dynamic characteristics are described and statistical analyses performed on these data base measurements are discussed. Analytical models applied to define the dynamic behavior of SSME components (such as turbopump bearing elements and the flight accelerometer safety cut-off system) are also summarized. Appendices are included to illustrate some typical tasks performed under this study.
Document ID
19860014170
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:178807
TR-64058-03
NASA-CR-178807
Report Number: NAS 1.26:178807
Report Number: TR-64058-03
Report Number: NASA-CR-178807
Accession Number
86N23641
Funding Number(s)
CONTRACT_GRANT: NAS8-33508
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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