LEADER 01769oam  2200517I  450 
001 9910714088803321
005 20201211102929.0
035   $a(CKB)5470000002506781
035   $a(OCoLC)761231417
035   $a(EXLCZ)995470000002506781
100   $a20111115j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMechanical behavior of boron-epoxy and glass-epoxy filament-wound cylinders under various loads /$fby Harvey W. Herring, Robert M. Baucom, and Richard A. Pride
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (65 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-5050
300   $a"March 1969."
320   $aIncludes bibliographical references (pages 20-21).
606   $aCylinders$xTesting
606   $aFibrous composites$xTesting
606   $aCylinders$xTesting$2fast
606   $aFibrous composites$xTesting$2fast
615  0$aCylinders$xTesting.
615  0$aFibrous composites$xTesting.
615  7$aCylinders$xTesting.
615  7$aFibrous composites$xTesting.
700   $aHerring$b Harvey W.$01419398
702   $aBaucom$b Robert M.
702   $aPride$b Richard A.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714088803321
996   $aMechanical behavior of boron-epoxy and glass-epoxy filament-wound cylinders under various loads$93533702
997   $aUNINA