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100   $a20111115j196903    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCold performance evaluation of 4.97-inch radial-inflow turbine designed for single-shaft Brayton cycle space-power system /$fWilliam J. Nusbaum and Milton G. Kofskey
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dMarch 1969.
215   $a1 online resource (ii, 22 pages) $cillustrations
225 1 $aNASA technical note. ;$vTN D-5090
300   $a"March 1969."
320   $aIncludes bibliographical references (page 22).
606   $aTurbines$xAerodynamics
606   $aBrayton cycle
606   $aSpace vehicles$xAuxiliary power supply$xBrayton cycle
606   $aBrayton cycle$2fast
606   $aSpace vehicles$xAuxiliary power supply$xBrayton cycle$2fast
606   $aTurbines$xAerodynamics$2fast
615  0$aTurbines$xAerodynamics.
615  0$aBrayton cycle.
615  0$aSpace vehicles$xAuxiliary power supply$xBrayton cycle.
615  7$aBrayton cycle.
615  7$aSpace vehicles$xAuxiliary power supply$xBrayton cycle.
615  7$aTurbines$xAerodynamics.
700   $aNusbaum$b William J.$01413835
702   $aKofskey$b Milton G.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910714101003321
996   $aCold performance evaluation of 4.97-inch radial-inflow turbine designed for single-shaft Brayton cycle space-power system$93511253
997   $aUNINA