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The Thermal Design, Characterization, and Performance of the SPIDER Long-Duration Balloon Cryostat

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arxiv 1506.06953 v2 pith:ZBXE5VFR submitted 2015-06-23 astro-ph.IM astro-ph.COphysics.ins-det

The Thermal Design, Characterization, and Performance of the SPIDER Long-Duration Balloon Cryostat

classification astro-ph.IM astro-ph.COphysics.ins-det
keywords cryostatflightliquidtankduringmainantarcticballoon
verification ladder T0 review T1 audit T2 compute T3 formal T4 reserved
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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 helium-4 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 helium-3 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.

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