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Air Liquide space cryocooler systems.

Author(s) : TROLLIER T., TANCHON J., BUQUET J., et al.

Type of article: Article, Case study

Summary

After successful developments these last 3 years, AL/DTA is now in position to propose two pulse tube cryocooler systems for space applications in the 40-80 K temperature range. The two pulse tube cryocoolers are yet qualified against stringent thermal and mechanical environmental constraints. AL/DTA also develops associated Cooler Drive Electronic at QM level implementing launch locking and vibrations cancellation. This paper presents these complete cryocooler systems available for space applications. [Reprinted with permission from Elsevier. Copyright, 2008].

Details

  • Original title: Air Liquide space cryocooler systems.
  • Record ID : 2009-0990
  • Languages: English
  • Source: Cryogenics - vol. 48 - n. 5-6
  • Publication date: 2008/05

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