Performance degradation of space Stirling cryocoolers due to gas contamination

With extensive application of infrared detective techniques, Stirling cryocoolers, used as an active cooling source, have been developed vigorously in China. After the cooler's cooling performance can satisfy the mission's request, its reliability level is crucial for its application. Among all the possible failure mechanisms, gas contamination has been found to be the most notorious cause of cooler's performance degradation by failure analyses. To analyze the characteristic of gas contamination, some experiments were designed and carried out to quantitatively analyze the relationship between failure and performance. Combined with the test results and the outgassing characteristic of non-metal materials in the cryocooler, a degradation model of cooling performance was given by T(t)=T0+A[1-exp(-t/B)] under some assumptions, where t is the running time, T is the Kelvin cooling temperature, and T0, A, B are model parameters, which can be given by the least square method. Here T0 is the fitting initial cooling temperature, A is the maximum range of performance degradation, and B is the time dependent constant of degradation. But the model parameters vary when a cryocooler is running at different cooling temperature ranges, or it is treated by different cleaning process. In order to verify the applicability of the degradation model, data fit analysis on eight groups of cooler's lifetime test was carried out. The final work indicated this model fit well with the performance degradation of space Stirling cryocoolers due to gas contamination and this model could be used to predict or evaluation the cooler's lifetime. Gaseous contamination will not arouse severe performance degradation until the contaminants accumulate to a certain amount, but it could be fatal when it works. So it is more serious to the coolers whose lifetime is more than 10,000 h. The measures taken to control or minimize its damage were discussed as well. To the long-life cryocooler, internal materials must be baked and organic/epoxy materials should be used as few as possible. Further more, pipeline for filling working fluid must have purifying facilities.

[1]  Jean-Yves Martin,et al.  Update on lifetime tests results and analysis carried out on Thales Cryogenics integral coolers (RM family) , 2003, SPIE Optics + Photonics.

[2]  J.,et al.  Gas Contamination Effects on Pulse Tube Performance , 2001 .

[3]  Jean-Yves Martin 10-year update of Stirling cryogenic coolers in France , 2000, SPIE Optics + Photonics.

[4]  T. Benschop,et al.  Development of the LSF95xx 2nd generation flexure bearing coolers , 2005, SPIE Defense + Commercial Sensing.

[5]  D. T. Kuo,et al.  Cryocooler contamination study , 2000 .

[6]  Alexander Veprik,et al.  Life test result of Ricor K529N 1watt linear cryocooler , 2007, SPIE Defense + Commercial Sensing.

[7]  Philippe Tribolet,et al.  Reliability optimization for IR detectors with compact cryo-coolers , 2005, SPIE Defense + Commercial Sensing.

[8]  B. J. Tomlinson,et al.  The Development of a 10 K Closed Cycle Stirling Cooler for Space Use , 2002 .

[9]  D. T. Kuo,et al.  CMCEC Life Test Results and Related Issues , 2003 .

[10]  D. T. Kuo,et al.  Cryocooler Contamination Study: Temperature Dependence of Outgassing , 2002 .

[11]  G. R. Pruitt,et al.  Methods for Accelerated Life Evaluation of Long‐Life Cryocoolers , 2004 .

[12]  D. S. Glaister,et al.  An Overview of the Performance and Maturity of Long Life Cryocoolers for Space Applications , 2002 .

[13]  D. S. Glaister,et al.  Space Cryocooler Contamination Lessons Learned and Recommended Control Procedures , 2002 .

[14]  B. G. Jones Development for Space Use of BAe’s Improved Single-Stage Stirling Cycle Cooler for Applications in the Range 50–80 K , 1995 .