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Swift BAT Loop Heat Pipe Thermal System Characteristics and Ground/Flight Operation Procedure
Author(s) -
Michael K. Choi
Publication year - 2003
Publication title -
1st international energy conversion engineering conference (iecec)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2003-6077
Subject(s) - swift , heat pipe , loop (graph theory) , thermal , aerospace engineering , mechanics , computer science , control theory (sociology) , environmental science , physics , heat transfer , engineering , meteorology , mathematics , control (management) , combinatorics , artificial intelligence , programming language
The SWIFT Burst Alert Telesco pe (BAT) Detector Array has a total power dissipation of 208 W. To meet the stringent temperature gradient and thermal stability requirements in the normal operational mode, and heater power budget in both the normal operational and safehold modes, the Det ector Array is thermally well coupled to eight constant conductance heat pipes (CCHPs) embedded in the Detector Array Plate (DAP), and two loop heat pipes (LHPs) transport heat from the CCHPs to a radiator. The CCHPs have ammonia as the working fluid and the LHPs have propylene as the working fluid. Precision heater controllers, which have adjustable set points in flight, are used to control the LHP compensation chamber and Detector Array XA1 ASIC temperatures. The radiator has the AZ -Tek AZW -LA -II low -alpha white paint as the thermal coating and is located on the anti -sun side of the spacecraft. This paper presents the characteristics, ground operation and flight operation procedures of the LHP thermal system.

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