LEADER 01997nam  2200493I  450 
001 9910704182803321
005 20151119150312.0
035   $a(CKB)5470000002437833
035   $a(OCoLC)929987984
035   $a(EXLCZ)995470000002437833
100   $a20151119j198705    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTime-temperature-stress capabilities of composite materials for advanced supersonic technology application /$fJ.R. Kerr and J.F. Haskhs
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1987.
215   $a1 online resource (673 unnumbered pages) $cillustrations
225 1 $aNASA contractor report ;$v178272
300   $aTitle from title screen (viewed on Nov. 19, 2015).
300   $a"May 1987."
300   $a"Performing organization: Convair Division of General Dynamics Corporation, San Diego, California"--Technical report page.
320   $aIncludes bibliographical references (pages [652-655]).
606   $aAccelerated life tests$2nasat
606   $aAircraft construction materials$2nasat
606   $aSpacecraft construction materials$2nasat
606   $aTime temperature parameter$2nasat
606   $aFatigue (materials)$2nasat
615  7$aAccelerated life tests.
615  7$aAircraft construction materials.
615  7$aSpacecraft construction materials.
615  7$aTime temperature parameter.
615  7$aFatigue (materials)
700   $aKerr$b J. R.$01404112
702   $aHaskhs$b J. F.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704182803321
996   $aTime-temperature-stress capabilities of composite materials for advanced supersonic technology application$93478094
997   $aUNINA