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Thermal architecture for the SPIDER flight cryostat Amiri, Mandana; Burger, Bryce; Halpern, Mark; Hasselfield, Matthew
Abstract
We describe the cryogenic system for SPIDER, a balloon-borne microwave polarimeter that will map 8% of the sky with degree-scale angular resolution. The system consists of a 1284 L liquid helium cryostat and a 16 L capillary-filled superfluid helium tank, which provide base operating temperatures of 4 K and 1.5 K, respectively. Closed-cycle 3He adsorption refrigerators supply sub-Kelvin cooling power to multiple focal planes, which are housed in monochromatic telescope inserts. The main helium tank is suspended inside the vacuum vessel with thermally insulating fiberglass flexures, and shielded from thermal radiation by a combination of two vapor cooled shields and multi-layer insulation. This system allows for an extremely low instrumental background and a hold time in excess of 25 days. The total mass of the cryogenic system, including cryogens, is approximately 1000 kg. This enables conventional long duration balloon flights. We will discuss the design, thermal analysis, and qualification of the cryogenic system Copyright 2010 Society of Photo-Optical Instrumentation Engineers. One print or electronic copy may be made for personal use only. Systematic reproduction and distribution, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper are prohibited.
Item Metadata
Title |
Thermal architecture for the SPIDER flight cryostat
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Creator | |
Publisher |
Society of Photo-Optical Instrumentation Engineers (SPIE)
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Date Issued |
2010
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Description |
We describe the cryogenic system for SPIDER, a balloon-borne microwave polarimeter that will map 8% of the sky with
degree-scale angular resolution. The system consists of a 1284 L liquid helium cryostat and a 16 L capillary-filled
superfluid helium tank, which provide base operating temperatures of 4 K and 1.5 K, respectively. Closed-cycle 3He
adsorption refrigerators supply sub-Kelvin cooling power to multiple focal planes, which are housed in monochromatic
telescope inserts. The main helium tank is suspended inside the vacuum vessel with thermally insulating fiberglass
flexures, and shielded from thermal radiation by a combination of two vapor cooled shields and multi-layer insulation.
This system allows for an extremely low instrumental background and a hold time in excess of 25 days. The total mass
of the cryogenic system, including cryogens, is approximately 1000 kg. This enables conventional long duration balloon
flights. We will discuss the design, thermal analysis, and qualification of the cryogenic system
Copyright 2010 Society of Photo-Optical Instrumentation Engineers.
One print or electronic copy may be made for personal use only. Systematic reproduction and distribution,
duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper are prohibited.
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Genre | |
Type | |
Language |
eng
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Date Available |
2011-09-12
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Provider |
Vancouver : University of British Columbia Library
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Rights |
Attribution-NonCommercial-NoDerivatives 4.0 International
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DOI |
10.14288/1.0107569
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URI | |
Affiliation | |
Citation |
Gudmundsson, Jon E.; Ade, Peter A. R.; Amiri, Mandana; Benton, Steven J.; Bihary, Richard; Bock, James J.; Bond, J. Richard; Bonetti, Joseph A.; Bryan, Sean A.; Burger, Bryce; Chiang, H. Cynthia; Contaldi, Carlo R.; Crill, Brendan P.; Dore, Olivier; Farhang, Marzieh; Filippini, Jeffrey P.; Fissel, Laura M.; Gandilo, Natalie N.; Golwala, Sunil R.; Halpern, Mark; Hasselfield, Matthew; Hilton, Gene C.; Holmes, Warren; Hristov, Viktor V.; Irwin, Kent D.; Jones, William C; Kuo, Chao Lin; MacTavish, Carrie J.; Mason, Peter V.; Montory, Thomas E.; Morford, Tracy A.; Netterfield, C. Barth; O'Dea, Daniel T.; Rahlin, Alexandra S.; Reintsema, Carl D.; Ruhl, John E.; Runyan, Marcus C.; Schenker, Matthew A.; Shariff, Jamil A.; Soler, Juan Diego; Trangsrud, Amy R.; Tucker, Carole E.; Tucker, Rebecca S.; Turner, Anthony D. Thermal architecture for the SPIDER flight cryostat. Millimeter, Submillimeter, and Far-Infrared Detectors and Instrumentation for Astronomy V, edited by Holland, Wayne S.; Jonas Zmuidzinas, Proceedings of SPIE Volume 7741, 77411M, 2010.
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Publisher DOI |
10.1117/12.857925
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Peer Review Status |
Reviewed
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Scholarly Level |
Faculty
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Copyright Holder |
Halpern, Mark
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Rights URI | |
Aggregated Source Repository |
DSpace
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Item Media
Item Citations and Data
Rights
Attribution-NonCommercial-NoDerivatives 4.0 International