Experimental Demonstration of Cryogenic Cooler Disturbance Attenuation Using the Non-Linear Passive Isolation System
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/56/3/56_T-12-26/_pdf
Reference12 articles.
1. 1) Ross, R. G.: Cryocooler Reliability and Redundancy Considerations for Long-life Space Missions, Cryocoolers 11, Kluwer Academic/Plenum Publishers, New York, 2001, pp. 637-648.
2. 2) Ross, R. G., Jr. and Johnson, D. L.: NASA's Advanced Cryocooler Technology Development Program, Advances in Cryogenic Engineering, Vol. 51, Am. Inst. of Physics, New York, 2006.
3. 3) Gilmore, D. G.: Spacecraft Thermal Control Hand Book, 2nd Edition, No. 87, AIAA, Reston, 1996.
4. 4) Werret, S. T.: Development of a Small Stirling Cycle Cooler for Space Flight Applications, Advances in Cryogenic Engineering, Vol. 31, Am. Inst. of Physics, New York, 1986.
5. 5) Radebaugh, R.: Pulse Tube Cryocoolers for Cooling Infrared Sensors, Proc. SPIE, Vol. 4130, 2000.
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1. Performance evaluation of spaceborne cryocooler micro-vibration isolation system employing pseudoelastic SMA mesh washer;Cryogenics;2015-04
2. Microvibration in spacecraft;Mechanical Engineering Reviews;2014
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