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SSME structural dynamic model developmentA mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed emphasis on LOX and High Fuel Turbopumps is developed. The advantages of both complete engine dynamics, and high fidelity modeling are incorporated. Development of this model, some results, and projected applications are discussed.
Document ID
19840009219
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Foley, M. J. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Tilley, D. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Welch, C. T. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
LMSC-HREC-TR-D867307
NAS 1.26:170960
NASA-CR-170960
Report Number: LMSC-HREC-TR-D867307
Report Number: NAS 1.26:170960
Report Number: NASA-CR-170960
Accession Number
84N17287
Funding Number(s)
CONTRACT_GRANT: NAS8-34973
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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