02149nam 2200541Ia 450 991069725740332120230902161909.0(CKB)5470000002386348(OCoLC)664270412(EXLCZ)99547000000238634820100916d2006 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierA comparison of coolant options for Brayton power conversion heat rejection systems[electronic resource] /John Siamidis, Lee S. Mason ; prepared for the Space Technology and Applications International Forum (STAIF-2006) sponsored by the University of New Mexico's Institute for Space and Nuclear Power Studies (UNM-ISNPS) Albuquerque, New Mexico, February 12-16, 2006Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2006]1 online resource (15 pages) illustrationsNASA TM- ;2006-214121Title from title screen (viewed on Sept. 16, 2010)."February 2006."Includes bibliographical references (page 14).NASA technical memorandum ;214121.Brayton cyclenasatHeat pipesnasatNuclear electric propulsionnasatCoolantsnasatDesign analysisnasatFluid pressurenasatHigh pressurenasatBrayton cycle.Heat pipes.Nuclear electric propulsion.Coolants.Design analysis.Fluid pressure.High pressure.Siamidis John1389259Mason Lee S1386997NASA Glenn Research Center.Space Technology & Applications International Forum(2006 :Albuquerque, N.M.)GPOGPOBOOK9910697257403321A comparison of coolant options for Brayton power conversion heat rejection systems3517066UNINA