LEADER 02058oam  2200577 a 450 
001 9910698094103321
005 20110908100545.0
035   $a(CKB)5470000002394058
035   $a(OCoLC)301229400$z(OCoLC)301238906
035   $a(EXLCZ)995470000002394058
100   $a20090202d1989      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue crack growth study of SCS?/Ti-15-3 composite$b[electronic resource] /$fPeter Kantzos and Jack Telesman
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration,$d[1989]
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v102332
300   $aTitle from title screen (viewed Jan. 29, 2009)
300   $a"August 1989."
300   $a"Performing organization, National Aeronautics and Space Administration, Lewis Research Center"--Rept. documentation p.
320   $aIncludes bibliographical references (page 6).
606   $aCoposite materials$2nasat
606   $aCrack propagation$2nasat
606   $aFatigue (materials)$2nasat
606   $aFracture mechanics$2nasat
606   $aMatrix materials$2nasat
606   $aSilicon carbides$2nasat
606   $aSpacecraft construction materials$2nasat
606   $aTitanium$2nasat
615  7$aCoposite materials.
615  7$aCrack propagation.
615  7$aFatigue (materials)
615  7$aFracture mechanics.
615  7$aMatrix materials.
615  7$aSilicon carbides.
615  7$aSpacecraft construction materials.
615  7$aTitanium.
700   $aKantzos$b Peter$01418610
701   $aTelesman$b Jack$01398014
712 02$aUnited States.$bNational Aeronautics and Space Administration.
712 02$aLewis Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910698094103321
996   $aFatigue crack growth study of SCS?$93532785
997   $aUNINA