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NASA-TN-D-3095

Experimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absolute

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:50:29Z
date available2017-09-04T15:50:29Z
date copyright01/01/1966
date issued1966
identifier otherQHBBFEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/53550
description abstractCryogenic para hydrogen heat transfer data at near critical pressures and temperatures for advanced propulsion system coolant.
languageEnglish
titleNASA-TN-D-3095num
titleExperimental heat-transfer results for cryogenic hydrogen flowing in tubes at subcritical and supercritical pressures to 800 pounds per square inch absoluteen
typestandard
page142
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1966
contenttypefulltext
subject keywordsCOOLANTS
subject keywordsCRITICAL PRESSURE
subject keywordsCRITICAL TEMPERATURE
subject keywordsCRYOGENIC FLUID
subject keywordsCRYOGENIC FLUIDS
subject keywordsCRYOGENICS
subject keywordsHEAT TRANSFER
subject keywordsHIGH PRESSURE
subject keywordsHYDROGEN
subject keywordsNUSSELT NUMBER
subject keywordsPARA HYDROGEN
subject keywordsPROPULSION
subject keywordsPROPULSION SYSTEM
subject keywordsSUPERCRITICAL PRESSURES


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