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Flight Performance of the AKARI Cryogenic System

机译:AKARI低温系统的飞行性能

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WedescribetheflightperformanceofthecryogenicsystemoftheinfraredastronomicalsatelliteAKARI,whichwassuccessfullylaunchedon2006February21(UT).AKARIcarriesa68.5cmtelescopetogetherwithtwofocal-planeinstruments,InfraredCamerasandFarInfraredSurveyor,allofwhicharecooleddowntocryogenictemperaturetoachievesuperiorsensitivity.AKARIhasauniquecryogenicsystem,whichconsistsofcryogen(liquidhelium)andmechanicalcoolers(2-stageStirlingcoolers).Withthehelpofmechanicalcoolers,179L(26.0kg)ofsuper-fluidliquidheliumcankeeptheinstrumentscryogenicallycooledformorethan500days.Theon-orbitperformanceoftheAKARIcryogenicsisconsistentwiththedesignandapre-flighttest,andtheboil-offgasflowrateisassmallas0.32mgs$$^{-1}$$.WeobservedanincreaseinthemajoraxisoftheAKARIorbit,whichcanbeexplainedbythrustduetothethermalpressureofventedheliumgas.
机译:WedescribetheflightperformanceofthecryogenicsystemoftheinfraredastronomicalsatelliteAKARI,whichwassuccessfullylaunchedon2006February21(UT).AKARIcarriesa68.5cmtelescopetogetherwithtwofocal-planeinstruments,InfraredCamerasandFarInfraredSurveyor,allofwhicharecooleddowntocryogenictemperaturetoachievesuperiorsensitivity.AKARIhasauniquecryogenicsystem,whichconsistsofcryogen(liquidhelium)andmechanicalcoolers(2- stageStirlingcoolers).Withthehelpofmechanicalcoolers,179L(26.0公斤)ofsuper-fluidliquidheliumcankeeptheinstrumentscryogenicallycooledformorethan500days.Theon-orbitperformanceoftheAKARIcryogenicsisconsistentwiththedesignandapre-flighttest,andtheboil-offgasflowrateisassmallas0 .32mgs $$ ^ {-1} $$。我们观察到AKARI轨道的长轴上的增加,这可以通过通入氦气的热压来解释。

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