02443oam 2200673 450 991071724660332120220323085940.0(CKB)5470000002529761(OCoLC)1305016322(EXLCZ)99547000000252976120220323d1989 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSpace shuttle main engine structural analysis and data reduction/evaluationVolume 2High pressure oxidizer turbo-pump turbine end bearing analysis final report /by Gregory A. SiskHuntsville, AL :Lockheed Missiles & Space Company, Huntsville Engineering Center,1989.1 online resource (approximately 85 pages) illustrations[NASA contractor report] ;NASA-CR-183664"April 1989.""LMSC-HEC TR F268584-II."Includes bibliographical reference (page 6).Space shuttle main engine structural analysis and data reduction/evaluation Data reductionFinite element methodSpace shuttlesPropulsion systemsStructural analysis (Engineering)Turbine pumpsSynthetic training devicesSpacecraft propulsionnasatComputerized simulationnasatData reductionnasatFinite element methodnasatSpace Shuttle Main EnginenasatStructural analysisnasatTurbine pumpsnasatData reduction.Finite element method.Space shuttlesPropulsion systems.Structural analysis (Engineering)Turbine pumps.Synthetic training devices.Spacecraft propulsion.Computerized simulation.Data reduction.Finite element method.Space Shuttle Main Engine.Structural analysis.Turbine pumps.Sisk Gregory A.1403693George C. Marshall Space Flight Center,GPOGPOGPOBOOK9910717246603321Space shuttle main engine structural analysis and data reduction3476823UNINA