کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1507283 993901 2015 12 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
The thermal design, characterization, and performance of the Spider long-duration balloon cryostat
ترجمه فارسی عنوان
طراحی حرارتی، مشخصات و عملکرد کریستت بالون بلند مدت عنکبوتی
کلمات کلیدی
ابزار دقیق، پس زمینه مایکروویو کیهانی، بار مصرف استراتوسفری، کریواستات،
موضوعات مرتبط
مهندسی و علوم پایه مهندسی مواد مواد الکترونیکی، نوری و مغناطیسی
چکیده انگلیسی
We describe the Spider flight cryostat, which is designed to cool six millimeter-wavelength telescopes during an Antarctic long-duration balloon flight. The cryostat, one of the largest to have flown on a stratospheric payload, uses liquid 4He to deliver cooling power to stages at 4.2 and 1.6 K. Stainless steel capillaries facilitate a high flow impedance connection between the main liquid helium tank and a smaller superfluid tank, allowing the latter to operate at 1.6 K as long as there is liquid in the 4.2 K main tank. Each telescope houses a closed cycle 3He adsorption refrigerator that further cools the focal planes down to 300 mK. Liquid helium vapor from the main tank is routed through heat exchangers that cool radiation shields, providing negative thermal feedback. The system performed successfully during a 17 day flight in the 2014-2015 Antarctic summer. The cryostat had a total hold time of 16.8 days, with 15.9 days occurring during flight.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Cryogenics - Volume 72, Part 1, December 2015, Pages 65-76
نویسندگان
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