کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
649085 884642 2009 5 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Simulation of a LHP-based thermal control system under orbital environment
موضوعات مرتبط
مهندسی و علوم پایه مهندسی شیمی جریان سیال و فرایندهای انتقال
پیش نمایش صفحه اول مقاله
Simulation of a LHP-based thermal control system under orbital environment
چکیده انگلیسی

In this paper, a thermal control system, using loop heat pipe as basic heat transfer elements, was designed for Alpha Magnetic Spectrometer. A system level model, which is integrated with the International Space Station model, was built, optimized and used to analyze several typical cases representing the orbital environment, to understand the operation of the LHP-based thermal control system during the mission time. The LHP system was proved to be able to maintain the Cryocooler within the required temperature range in most cases, while under some worst cold environments, the bypass valve needs to be activated.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Applied Thermal Engineering - Volume 29, Issue 13, September 2009, Pages 2726–2730
نویسندگان
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