LEADER 02035nam  2200553Ia 450 
001 9910700760803321
005 20110823113036.0
035   $a(CKB)5470000002411398
035   $a(OCoLC)747568690
035   $a(EXLCZ)995470000002411398
100   $a20110823d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage$b[electronic resource] /$fA.J. Hodge, A.T. Nettles, and J.R. Jackson
210  1$a[Huntsville], Ala. :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d[2011]
215   $a1 online resource (viii, 23 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2011-216460
300   $aTitle from title screen (viewed on Aug. 22, 2011).
300   $a"March 2011."
320   $aIncludes bibliographical references (pages 22-23).
606   $aCompressive strength$2nasat
606   $aSandwich structures$2nasat
606   $aCarbon fibers$2nasat
606   $aImpact strength$2nasat
606   $aDamage$2nasat
606   $aEpoxy matrix composites$2nasat
606   $aLaminates$2nasat
606   $aFiber composites$2nasat
615  7$aCompressive strength.
615  7$aSandwich structures.
615  7$aCarbon fibers.
615  7$aImpact strength.
615  7$aDamage.
615  7$aEpoxy matrix composites.
615  7$aLaminates.
615  7$aFiber composites.
700   $aHodge$b A. J$01403595
701   $aNettles$b A. T$g(Alan T.)$01389578
701   $aJackson$b J. R$01403596
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700760803321
996   $aComparison of open-hole compression strength and compression after impact strength on carbon fiber$93498703
997   $aUNINA