Development of Two-Stage Stirling Cooler for ASTRO-F

AIP Conference Proceedings

Volumn 710, Issue , 2004, Pages 1428-1435

  Narasaki, K ^a   Tsunematsu, S ^a   Ootsuka, K ^a   Kyoya, M ^a   Matsumoto, T ^b   Murakami, H ^b   Nakagawa, T ^b  

^a SUMITOMO HEAVY INDUSTRIES LTD   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BALL BEARINGS; COOLING SYSTEMS; CRYOGENICS; IODINE COMPOUNDS; LINEAR MOTORS; LIQUEFIED GASES; PISTONS; ROCKETS; SUPERFLUID HELIUM; TESTING; VACUUM TECHNOLOGY;

DRIVER ELECTRONICS; LINEAR BALL BEARING; PERFORMANCE TESTS; SUPERFLUID LIQUID HELIUM; SUPPORTING STRUCTURE; SUPPORTING SYSTEMS; THERMAL VACUUM TESTS; VERIFICATION TESTS;

ELECTRONIC COOLING;

EID: 36849091193     PISSN: 0094243X     EISSN: 15517616     Source Type: Conference Proceeding    
DOI: 10.1063/1.1774835     Document Type: Conference Paper

References (3)

1. M. Kyoya, K. Narasaki, K. Ito, K. Nomi, M. Murakami, H. Okuda, T. Matsumoto and Y. Matsubara "Development of Two-stage Small Stirling Cycle Cooler for Temperature below 20K, " Cryogenics, 34, pp.431-434, 1994.
2. H. Murakami, Japanese Infrared Survey Mission IRIS (ASTRO-F), Proceedings of SPIE, 3356, pp.471-477, 1998.
3. B.G. Jones and S.R. Scull, "Development and preflight qualification testing of a range of cryogenic coolers for applications from 20 K to 80 K, " Cryogenics, 32, pp.850-858, 1992.