LEADER 01890nam  2200505   450 
001 9910702733803321
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035   $a(CKB)5470000002430863
035   $a(OCoLC)902679849
035   $a(EXLCZ)995470000002430863
100   $a20150203j201409    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites $ea protocol for producing void-free quality laminates /$fTan-Hung Hou
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dSeptember 2014.
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA/TM ;$v2014-218524
300   $aTitle from title screen (viewed Feb. 3, 2015).
300   $a"September 2014."
320   $aIncludes bibliographical references (pages 15-16).
517   $aCure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites 
606   $aResin matrix composites$2nasat
606   $aLaminates$2nasat
606   $aPressure distribution$2nasat
606   $aVoids$2nasat
606   $aMatrix materials$2nasat
606   $aPolyimides$2nasat
615  7$aResin matrix composites.
615  7$aLaminates.
615  7$aPressure distribution.
615  7$aVoids.
615  7$aMatrix materials.
615  7$aPolyimides.
700   $aHou$b T. H.$01393498
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702733803321
996   $aCure cycle design methodology for fabricating reactive resin matrix fiber reinforced composites$93449691
997   $aUNINA