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035   $a(OCoLC)761231836
035   $a(EXLCZ)995470000002507673
100   $a20111115j196809    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDescriptions and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnel /$fby Kenneth Sutton
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dSeptember 1968.
215   $a1 online resource (67 pages) $cillustrations
225 1 $aNASA technical note ;$vTN D-4750
300   $a"September 1968."
320   $aIncludes bibliographical references (pages 18-19).
606   $aNozzles$xTesting
606   $aMach number$xTesting
606   $aHeat resistant materials$xTesting
606   $aHeat resistant materials$xTesting$2fast
606   $aNozzles$xTesting$2fast
615  0$aNozzles$xTesting.
615  0$aMach number$xTesting.
615  0$aHeat resistant materials$xTesting.
615  7$aHeat resistant materials$xTesting.
615  7$aNozzles$xTesting.
700   $aSutton$b Kenneth$01403502
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910715033303321
996   $aDescriptions and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnel$93476358
997   $aUNINA