ShareDiaphragm Stirling cryocooler developments.
Author(s) : STACY W. D.
Type of article: Article
Summary
Three programmes are described, each leading to system or component test hardware: a 2-watt, 65 K single-stage Standard Spacecraft Cryocooler, a 300-milliwatt, 30 K two-stage cooler and a 200-milliwatt, 4-20 K single-stage cooler. Design features are described, and breadboard experimental data are presented.
Details
- Original title: Diaphragm Stirling cryocooler developments.
- Record ID : 1993-1805
- Languages: English
- Source: Cryogenics - vol. 32 - n. 2
- Publication date: 1992
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Advanced pulse tube cold head development.
- Author(s) : CHAN C. K., JACO C., NGUYEN T.
- Date : 1996/06/25
- Languages : English
- Source: Cryocoolers 9. Proceedings of the International Cryocooler Conference.
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Development of Stirling Cryocooler in space.
- Author(s) : FUKUDA T., TAKAGI M., TAKAKUSAGI T., FURUKAWA M., ISHII Y.
- Date : 1992
- Languages : Japanese
- Source: Cryogenics/ Cryog. Eng. - vol. 27 - n. 3
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Development and preflight qualification testing...
- Author(s) : JONES B. G., SCULL S. R.
- Date : 1992
- Languages : English
- Source: Cryogenics - vol. 32 - n. 10
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Development of two-stage small Stirling cycle c...
- Author(s) : KYOYA M., NARASAKI K., ITO K., NOMI K., MURAKAMI M., OKUDA H., MURAKAMI H., MATSUMOTO T., MATSUBARA Y.
- Date : 1994/05
- Languages : English
- Source: Cryogenics - vol. 34 - n. 5
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Development of advanced two-stage Stirling cryo...
- Author(s) : SATO Y., SUGITA H., KOMATSU K., et al.
- Date : 2009
- Languages : English
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