LEADER 01586nam  2200457 a 450 
001 9910700382303321
005 20110825124449.0
035   $a(CKB)5470000002409161
035   $a(OCoLC)747836133
035   $a(EXLCZ)995470000002409161
100   $a20110825d2009      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications$b[electronic resource] /$fA.T. Nettles
210  1$a[Huntsville], Ala. :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d[2009]
215   $a1 online resource (vii, 23 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2009-215900
300   $aTitle from title screen (viewed on Aug. 25, 2011).
300   $a"June 2009."
320   $aIncludes bibliographical references (page 23).
606   $aEpoxy matrix composites$2nasat
606   $aTemperature effects$2nasat
606   $aCompressive strength$2nasat
606   $aLaunch vehicles$2nasat
606   $aSafety factors$2nasat
615  7$aEpoxy matrix composites.
615  7$aTemperature effects.
615  7$aCompressive strength.
615  7$aLaunch vehicles.
615  7$aSafety factors.
700   $aNettles$b A. T$g(Alan T.)$01389578
712 02$aGeorge C. Marshall Space Flight Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700382303321
996   $aHot$93490401
997   $aUNINA