01983nam 2200553I 450 991070462900332120130705143034.0(CKB)5470000002443427(OCoLC)851800599(EXLCZ)99547000000244342720130705d2013 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierLarge-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept /R.H. Flachbart [and six others]Huntsville, Alabama :National Aeronautics and Space Administration, Marshall Space Flight Center,2013.1 online resource (vii, 43 pages) illustrations (some color)NASA/TP ;2013-217482Title from title screen (viewed on July 5, 2013)."April 2013."Includes bibliographical references (page 43).Upper stage rocket enginesnasatCryogenic fluidsnasatFluid managementnasatLiquid hydrogennasatFilm boilingnasatHeat transfernasatCryogenic coolingnasatPropellant tanksnasatFuel tank pressurizationnasatUpper stage rocket engines.Cryogenic fluids.Fluid management.Liquid hydrogen.Film boiling.Heat transfer.Cryogenic cooling.Propellant tanks.Fuel tank pressurization.Flachbart R. H.1418319George C. Marshall Space Flight Center,GPOGPOBOOK9910704629003321Large-scale liquid hydrogen tank rapid chill and fill testing for the advanced shuttle upper stage concept3529394UNINA