LEADER 01884nam  2200505 a 450 
001 9910701853303321
005 20120622101917.0
035   $a(CKB)5470000002421575
035   $a(OCoLC)796083014
035   $a(EXLCZ)995470000002421575
100   $a20120622d2011      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications$b[electronic resource] /$fA.T. Nettles
210  1$aHuntsville, Ala. :$cNational Aeronautics and Space Administration, Marshall Space Flight Center,$d[2011]
215   $a1 online resource (vii, 39 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2011-216477
300   $aTitle from title screen (viewed on June 22, 2012).
300   $a"December 2011."
320   $aIncludes bibliographical references (page 39).
606   $aCompressive strength$2nasat
606   $aImpact strength$2nasat
606   $aHoneycomb structures$2nasat
606   $aLaunch vehicles$2nasat
606   $aDamage$2nasat
606   $aTolerances (mechanics)$2nasat
606   $aResidual strength$2nasat
615  7$aCompressive strength.
615  7$aImpact strength.
615  7$aHoneycomb structures.
615  7$aLaunch vehicles.
615  7$aDamage.
615  7$aTolerances (mechanics)
615  7$aResidual strength.
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   $a9910701853303321
996   $aA damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications$93492436
997   $aUNINA