Experimental study on liquid oxygen chilldown in the horizontal pipe with an injector on the exit
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DOI: 10.1016/j.applthermaleng.2020.115212
Abstract: Abstract Components downstream of the pump in the cryogenic liquid rocket engine were simplified to a horizontal pipe upstream of an injector. Cryogenic chilldown was investigated experimentally in this pipe by constant flow rate of… read more here.
Keywords: experimental study; physical properties; properties fluid; injector ... See more keywords