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001 9910717163103321
005 20220218085610.0
035   $a(CKB)5470000002528584
035   $a(OCoLC)1293754032
035   $a(EXLCZ)995470000002528584
100   $a20220126j202201    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure /$fA.T. Nettles, W.E. Guin, and C.C. Wolfe
210  1$aHuntsville, Alabama :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$dJanuary 2022.
215   $a1 online resource (approximately 30 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v20210026811
300   $a"January 2022."
320   $aIncludes bibliographical references (page 17).
606   $aComposite materials$2nasat
606   $aSandwich structures$2nasat
606   $aCarbon fibers$2nasat
615  7$aComposite materials.
615  7$aSandwich structures.
615  7$aCarbon fibers.
700   $aNettles$b A. T$g(Alan T.),$01389578
702   $aGuin$b W. E.
702   $aWolfe$b C. C.
712 02$aGeorge C. Marshall Space Flight Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910717163103321
996   $aA quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure$93476814
997   $aUNINA