LEADER 01763nam  2200493Ia 450 
001 9910701159503321
005 20111128132053.0
035   $a(CKB)5470000002415452
035   $a(OCoLC)763287352
035   $a(EXLCZ)995470000002415452
100   $a20111128d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEdgewise compression testing of STIPS-0 (Structurally Integrated Thermal Protection System)$b[electronic resource] /$fAmy R. Brewer
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (iv, 42 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2011-217161
300   $aTitle from title screen (viewed on Nov. 28, 2011).
300   $a"July 2011."
320   $aIncludes bibliographical references. (page 26)
517   $aEdgewise compression testing of STIPS-0 
606   $aCompression tests$2nasat
606   $aMechanical properties$2nasat
606   $aThermal protection$2nasat
606   $aLoads (forces)$2nasat
606   $aAerospace engineering$2nasat
606   $aNondestructive tests$2nasat
615  7$aCompression tests.
615  7$aMechanical properties.
615  7$aThermal protection.
615  7$aLoads (forces)
615  7$aAerospace engineering.
615  7$aNondestructive tests.
700   $aBrewer$b Amy R$01403522
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701159503321
996   $aEdgewise compression testing of STIPS-0 (Structurally Integrated Thermal Protection System)$93476408
997   $aUNINA