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001 9910699653603321
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035   $a(CKB)5470000002404400
035   $a(OCoLC)706732471
035   $a(EXLCZ)995470000002404400
100   $a20110310d2010      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSimplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware$b[electronic resource] /$fA.T. Nettles, A.J. Hodge, and J.R. Jackson
210  1$a[Huntsville], Ala. :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d[2010]
215   $a1 online resource (27 pages) $cillustrations
225 1 $aNASA/TP ;$v2010-216434
300   $aTitle from title screen (viewed on March 10, 2011).
300   $a"June 2010."
320   $aIncludes bibliographical references (pages 24-27).
410  0$aNASA technical paper ;$v216434.
606   $aComposite materials$2nasat
606   $aCompression loads$2nasat
606   $aDegradation$2nasat
606   $aDamage$2nasat
606   $aFatigue (materials)$2nasat
606   $aTolerances (mechanics)$2nasat
606   $aFailure$2nasat
615  7$aComposite materials.
615  7$aCompression loads.
615  7$aDegradation.
615  7$aDamage.
615  7$aFatigue (materials)
615  7$aTolerances (mechanics)
615  7$aFailure.
700   $aNettles$b A. T$g(Alan T.)$01389578
701   $aHodge$b A. J$01403595
701   $aJackson$b J. R$01403596
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699653603321
996   $aSimplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware$93476580
997   $aUNINA