LEADER 02443oam  2200673   450 
001 9910717246603321
005 20220323085940.0
035   $a(CKB)5470000002529761
035   $a(OCoLC)1305016322
035   $a(EXLCZ)995470000002529761
100   $a20220323d1989      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSpace shuttle main engine structural analysis and data reduction/evaluation$hVolume 2$iHigh pressure oxidizer turbo-pump turbine end bearing analysis $efinal report /$fby Gregory A. Sisk
210  1$aHuntsville, AL :$cLockheed Missiles & Space Company, Huntsville Engineering Center,$d1989.
215   $a1 online resource (approximately 85 pages) $cillustrations
225 1 $a[NASA contractor report] ;$vNASA-CR-183664
300   $a"April 1989."
300   $a"LMSC-HEC TR F268584-II."
320   $aIncludes bibliographical reference (page 6).
517   $aSpace shuttle main engine structural analysis and data reduction/evaluation 
606   $aData reduction
606   $aFinite element method
606   $aSpace shuttles$xPropulsion systems
606   $aStructural analysis (Engineering)
606   $aTurbine pumps
606   $aSynthetic training devices
606   $aSpacecraft propulsion$2nasat
606   $aComputerized simulation$2nasat
606   $aData reduction$2nasat
606   $aFinite element method$2nasat
606   $aSpace Shuttle Main Engine$2nasat
606   $aStructural analysis$2nasat
606   $aTurbine pumps$2nasat
615  0$aData reduction.
615  0$aFinite element method.
615  0$aSpace shuttles$xPropulsion systems.
615  0$aStructural analysis (Engineering)
615  0$aTurbine pumps.
615  0$aSynthetic training devices.
615  7$aSpacecraft propulsion.
615  7$aComputerized simulation.
615  7$aData reduction.
615  7$aFinite element method.
615  7$aSpace Shuttle Main Engine.
615  7$aStructural analysis.
615  7$aTurbine pumps.
700   $aSisk$b Gregory A.$01403693
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910717246603321
996   $aSpace shuttle main engine structural analysis and data reduction$93476823
997   $aUNINA