02244nam 2200565I 450 991070733340332120160726113057.0(CKB)5470000002464186(OCoLC)953997252(EXLCZ)99547000000246418620160726j199610 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThermal control subsystem design for the avionics of a space station payload /Matthew E. MoranCleveland, Ohio :National National Aeronautics and Space Administration, Lewis Research Center,October 1996.1 online resource (15 pages) illustrationsNASA technical memorandum ;107334Title from title screen (viewed July 26, 2016)."October 1996"--Report documentation page."Prepared for the Intemational Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996.""Performing organization: National National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (page 15).Space Shuttle payloadsnasatTemperature controlnasatCoolingnasatControl systems designnasatElectronic controlnasatAvionicsnasatThermal analysisnasatDesign analysisnasatSpace Shuttle payloads.Temperature control.Cooling.Control systems design.Electronic control.Avionics.Thermal analysis.Design analysis.Moran Matthew E.1395983Lewis Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910707333403321Thermal control subsystem design for the avionics of a space station payload3455325UNINA