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Multi-Stage Cryocooler for Space Applications

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Abstract

Ball has developed a two-stage Stirling cycle cooler for high reliability space applications. Our cooler provides in excess of 400 mW of lift at 30 K at the cold stage, and up to a watt at the mid stage, for 75 W of input power. We have incorporated novel sensors that allow monitoring of the piston gap clearance to ensure that it operates without contact. We have measured thermal performance, output vibration, EMI, and the effects of launch vibration.

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References

  1. Ross, R.G., Jr., “Requirements for long life mechanical cryocoolers for space applications,” Cryogenics, Vol. 31, (1990).

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  2. Radebaugh, Ray, “Measurement and Calculation of Regenerator Ineffectiveness for Temperatures of 5 to 40K,” WL-TR-92-3074, Wright-Patterson Air Force Base, Ohio 45433–6533, (1992).

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  3. Boyle, R., et. al., “Non-real time, feed forward vibration control system development and test results,” Proceedings of 7th International Cryocooler Conference, PL-CP-93-1001, Phillips Laboratory, Kirtland AFB, New Mexico 87117-5776, (1993), pp. 805.

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  4. Johnson, D.L., et. al., “Electromagnetic Compatibility Characterization of a BAe Stirling-Cycle Cryocooler for Space Applications,” Proc. Cryog. Eng. Conf., Huntsville, Alabama, ACE 37, (1991).

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© 1995 Springer Science+Business Media New York

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Carrington, H., Gully, W.J., Hubbard, M., Varner, C., Arter, P. (1995). Multi-Stage Cryocooler for Space Applications. In: Ross, R.G. (eds) Cryocoolers 8. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-9888-3_10

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  • DOI: https://doi.org/10.1007/978-1-4757-9888-3_10

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-9890-6

  • Online ISBN: 978-1-4757-9888-3

  • eBook Packages: Springer Book Archive

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