LEADER 01783nam 2200505I 450 001 9910709660303321 005 20180531140157.0 035 $a(CKB)5470000002471632 035 $a(OCoLC)1038072568 035 $a(EXLCZ)995470000002471632 100 $a20180531j198403 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEvaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems $eexecutive summary /$fT.J. Kramer, E.W. Brogren, and B.L. Siegel 210 1$aCleveland, Ohio :$cNASA Lewis Research Center,$dMarch 1984. 215 $a1 online resource (ix, 37 pages) $cillustrations 225 1 $aNASA/CR ;$v168321 300 $a"March 1984." 300 $a"BAC D 180-28274-1." 320 $aIncludes bibliographical references (page 37). 517 $aEvaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems 606 $aPropellant tanks$2nasat 606 $aChemical propulsion$2nasat 606 $aConvective heat transfer$2nasat 606 $aFoams$2nasat 606 $aCryogenic fluid storage$2nasat 615 7$aPropellant tanks. 615 7$aChemical propulsion. 615 7$aConvective heat transfer. 615 7$aFoams. 615 7$aCryogenic fluid storage. 700 $aKramer$b T. J.$01417240 702 $aBrogren$b E. W. 702 $aSiegel$b B. L. 712 02$aLewis Research Center, 712 02$aBoeing Aerospace Company. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910709660303321 996 $aEvaluation of propellant tank insulation concepts for low-thrust chemical propulsion systems$93524959 997 $aUNINA