The thermal design, characterization, and performance of the Spider long-duration balloon cryostat

•We describe the Spider flight cryostat.•We review the thermal design, characterization and performance of the cryostat.•The system performed successfully during a 17day flight in the 2014–2015 Antarctic summer. We describe the Spider flight cryostat, which is designed to cool six millimeter-wavelen...

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Veröffentlicht in:Cryogenics (Guildford) 2015-12, Vol.72, p.65-76
Hauptverfasser: Gudmundsson, J.E., Ade, P.A.R., Amiri, M., Benton, S.J., Bock, J.J., Bond, J.R., Bryan, S.A., Chiang, H.C., Contaldi, C.R., Crill, B.P., Dore, O., Filippini, J.P., Fraisse, A.A., Gambrel, A., Gandilo, N.N., Hasselfield, M., Halpern, M., Hilton, G., Holmes, W., Hristov, V.V., Irwin, K.D., Jones, W.C., Kermish, Z., MacTavish, C.J., Mason, P.V., Megerian, K., Moncelsi, L., Montroy, T.E., Morford, T.A., Nagy, J.M., Netterfield, C.B., Rahlin, A.S., Reintsema, C.D., Ruhl, J.E., Runyan, M.C., Shariff, J.A., Soler, J.D., Trangsrud, A., Tucker, C., Tucker, R.S., Turner, A.D., Wiebe, D.V., Young, E.
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Sprache:eng
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Zusammenfassung:•We describe the Spider flight cryostat.•We review the thermal design, characterization and performance of the cryostat.•The system performed successfully during a 17day flight in the 2014–2015 Antarctic summer. 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 1.6K. 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 1.6K as long as there is liquid in the 4.2K main tank. Each telescope houses a closed cycle 3He adsorption refrigerator that further cools the focal planes down to 300mK. 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 17day flight in the 2014–2015 Antarctic summer. The cryostat had a total hold time of 16.8days, with 15.9days occurring during flight.
ISSN:0011-2275
1879-2235
DOI:10.1016/j.cryogenics.2015.09.002