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035   $a(OCoLC)953997252
035   $a(EXLCZ)995470000002464186
100   $a20160726j199610    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aThermal control subsystem design for the avionics of a space station payload /$fMatthew E. Moran
210  1$aCleveland, Ohio :$cNational National Aeronautics and Space Administration, Lewis Research Center,$dOctober 1996.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107334
300   $aTitle from title screen (viewed July 26, 2016).
300   $a"October 1996"--Report documentation page.
300   $a"Prepared for the Intemational Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996."
300   $a"Performing organization: National National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 15).
606   $aSpace Shuttle payloads$2nasat
606   $aTemperature control$2nasat
606   $aCooling$2nasat
606   $aControl systems design$2nasat
606   $aElectronic control$2nasat
606   $aAvionics$2nasat
606   $aThermal analysis$2nasat
606   $aDesign analysis$2nasat
615  7$aSpace Shuttle payloads.
615  7$aTemperature control.
615  7$aCooling.
615  7$aControl systems design.
615  7$aElectronic control.
615  7$aAvionics.
615  7$aThermal analysis.
615  7$aDesign analysis.
700   $aMoran$b Matthew E.$01395983
712 02$aLewis Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707333403321
996   $aThermal control subsystem design for the avionics of a space station payload$93455325
997   $aUNINA