LEADER 01879oam  2200493Ia 450 
001 9910701831203321
005 20120615125552.0
035   $a(CKB)5470000002421798
035   $a(OCoLC)795576092
035   $a(EXLCZ)995470000002421798
100   $a20120615d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSSME structural dynamic model development$b[electronic resource] $ephase II, final report /$fby M. J. Foley and V. L. Wilson
210  1$aHuntsville, AL :$cLockheed Missiles & Space Company, Inc, Huntsville Engineering Center :$cNational Aeronautics and Space Administration, George C. Marshall Space Flight Center,$d[1985]
215   $a1 online resource (v, 46 pages, 184 unnumbered pages) $cillustrations
225 1 $a[NASA contractor report] ;$v178708
225 1 $aLMSC-HEC TR ;$vF042668
300   $aTitle from title screen (viewed on June 15, 2012).
300   $a"1 November 1985."
320   $aIncludes bibliographical references (page 46).
517   $aSSME structural dynamic model development 
606   $aDynamic structural analysis$2nasat
606   $aFinite element method$2nasat
606   $aMathematical models$2nasat
606   $aSpace Shuttle Main Engine$2nasat
615  7$aDynamic structural analysis.
615  7$aFinite element method.
615  7$aMathematical models.
615  7$aSpace Shuttle Main Engine.
700   $aFoley$b M. J$01409233
701   $aWilson$b V. L$01409234
712 02$aHuntsville Research & Engineering Center.
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701831203321
996   $aSSME structural dynamic model development$93495106
997   $aUNINA