DocumentCode :
426823
Title :
SWIFT burst alert telescope loop heat pipe thermal system characteristics and flight operation procedure
Author :
Choi, Michael K.
Author_Institution :
NASA Goddard Space Flight Center, Greenbelt, MD, USA
fYear :
2004
fDate :
29-31 July 2004
Firstpage :
357
Lastpage :
360
Abstract :
Loop heat pipe (LHP) startup procedure is required after the spacecraft checkout phase, which follows the launch, ascent and early orbit phase, and after a safehold mode. This procedure will be verified during the BAT (burst alert telescope) instrument thermal vacuum and thermal balance test. The startup procedure and the LHP components in the normal flight operation mode are discussed in detail. The BAT power convertor box is used to contain power switches for the TCS normal operation mode heaters. It is required to supply voltage to the electronic heater controllers to power heaters, and adjustable voltage signals to the heater controllers to change the temperature set points in flights. It is also required to supply voltage to the startup heaters of the LHP.
Keywords :
heat pipes; power convertors; power semiconductor switches; space vehicle electronics; telescopes; thermal analysis; SWIFT burst alert telescope; electronic heater controllers; flight operation procedure; loop heat pipe thermal system; power convertor box; power heaters; power switches; spacecraft; startup heaters; Aerospace electronics; Circuits; Costs; Detectors; Heat transfer; NASA; Telescopes; Temperature control; Voltage control; Waste heat;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 2002. IECEC '02. 2002 37th Intersociety
Print_ISBN :
0-7803-7296-4
Type :
conf
DOI :
10.1109/IECEC.2002.1392046
Filename :
1392046
Link To Document :
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