LEADER 01946oam  2200529Ia 450 
001 9910696932803321
005 20230902161726.0
035   $a(CKB)5470000002383566
035   $a(OCoLC)690684961
035   $a(EXLCZ)995470000002383566
100   $a20101208d2009      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aImpact testing on reinforced carbon-carbon flat panels with BX-265 and PDL-1034 external tank foam for the Space Shuttle return to flight program$b[electronic resource] /$fMatthew E. Melis ... [and others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2009]
215   $a1 online resource (208 pages) $ccolor illustrations
225 1 $aNASA/TM- ;$v2009-213642/REV 1
300   $aTitle from title screen (viewed on Dec. 8, 2010).
300   $a"December 2009."
320   $aIncludes bibliographical references (pages 207-208)
410  0$aNASA technical memorandum ;$v213642.
606   $aCarbon-carbon composites$2nasat
606   $aDynamic models$2nasat
606   $aFoams$2nasat
606   $aImpact damage$2nasat
606   $aImpact tests$2nasat
606   $aColumbia (Orbiter)$2nasat
606   $aSpace shuttles$2nasat
615  7$aCarbon-carbon composites.
615  7$aDynamic models.
615  7$aFoams.
615  7$aImpact damage.
615  7$aImpact tests.
615  7$aColumbia (Orbiter)
615  7$aSpace shuttles.
701   $aMelis$b Matthew E$01401307
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910696932803321
996   $aImpact testing on reinforced carbon-carbon flat panels with BX-265 and PDL-1034 external tank foam for the Space Shuttle return to flight program$93469867
997   $aUNINA