LEADER 01721oam  2200445 a 450 
001 9910701805703321
005 20120628114316.0
035   $a(CKB)5470000002422056
035   $a(OCoLC)796997295
035   $a(EXLCZ)995470000002422056
100   $a20120628d1986      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aSpace Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis$b[electronic resource] $efinal report
210  1$aHuntsville, Ala. :$cSRS Technologies, Systems Technology Division ;$aMarshall Space Flight Center, Ala. :$cMaterials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center,$d[1986]
215   $a1 online resource (v, 52 pages) $cillustrations
225 1 $a[NASA contractor report] ;$v178746
300   $aTitle from title screen (viewed on June 28, 2012).
300   $a"January 6, 1986."
517   $aSpace Shuttle main engine 
606   $aComputerized simulation$2nasat
606   $aLiquid oxygen$2nasat
606   $aSpace Shuttle Main Engine$2nasat
606   $aTurbine pumps$2nasat
615  7$aComputerized simulation.
615  7$aLiquid oxygen.
615  7$aSpace Shuttle Main Engine.
615  7$aTurbine pumps.
712 02$aSRS Technologies.$bSystems Technology Division.
712 02$aGeorge C. Marshall Space Flight Center.$bMaterials and Processes Laboratory.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701805703321
996   $aSpace Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis$93526363
997   $aUNINA