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100   $a20100916d2006      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA comparison of coolant options for Brayton power conversion heat rejection systems$b[electronic resource] /$fJohn 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, 2006
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2006]
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA TM- ;$v2006-214121
300   $aTitle from title screen (viewed on Sept. 16, 2010).
300   $a"February 2006."
320   $aIncludes bibliographical references (page 14).
410  0$aNASA technical memorandum ;$v214121.
606   $aBrayton cycle$2nasat
606   $aHeat pipes$2nasat
606   $aNuclear electric propulsion$2nasat
606   $aCoolants$2nasat
606   $aDesign analysis$2nasat
606   $aFluid pressure$2nasat
606   $aHigh pressure$2nasat
615  7$aBrayton cycle.
615  7$aHeat pipes.
615  7$aNuclear electric propulsion.
615  7$aCoolants.
615  7$aDesign analysis.
615  7$aFluid pressure.
615  7$aHigh pressure.
700   $aSiamidis$b John$01389259
701   $aMason$b Lee S$01386997
712 02$aNASA Glenn Research Center.
712 12$aSpace Technology & Applications International Forum$f(2006 :$eAlbuquerque, N.M.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697257403321
996   $aA comparison of coolant options for Brayton power conversion heat rejection systems$93517066
997   $aUNINA