LEADER 02169nam  2200577Ia 450 
001 9910700761103321
005 20110802115112.0
035   $a(CKB)5470000002411395
035   $a(OCoLC)744420941
035   $a(EXLCZ)995470000002411395
100   $a20110802d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles$b[electronic resource] /$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[2011]
215   $a1 online resource (vii, 23 pages) $cillustrations
225 1 $aNASA/TP ;$v2011-216457
300   $aTitle from title screen (viewed on Aug. 2, 2011).
300   $a"February 2011."
320   $aIncludes bibliographical references (pages 22-23).
606   $aDamage assessment$2nasat
606   $aLaunch vehicles$2nasat
606   $aThermal protection$2nasat
606   $aSandwich structures$2nasat
606   $aResidual strength$2nasat
606   $aAres 1 launch vehicle$2nasat
606   $aComposite structures$2nasat
606   $aComposite materials$2nasat
606   $aImpact damage$2nasat
615  7$aDamage assessment.
615  7$aLaunch vehicles.
615  7$aThermal protection.
615  7$aSandwich structures.
615  7$aResidual strength.
615  7$aAres 1 launch vehicle.
615  7$aComposite structures.
615  7$aComposite materials.
615  7$aImpact damage.
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   $a9910700761103321
996   $aThe effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles$93551009
997   $aUNINA