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Thermodynamic Performance of the Ball Aerospace Multistage Stirling Cycle Mechanical Cooler

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Cryocoolers 12

Abstract

Ball Aerospace has been working on highly reliableStirling cycle multi-stage mechanical coolers for more than a decade. We have produced, characterized, and delivered one-, two-, and three-stage coolers on a number of programs. Currently we are developing a more producible two-stage cooler with twice the capacity that uses the same envelope. The tendency for larger coolers to be relatively efficient has been a benefit. We have incorporated changes to the motor to improve its electrical efficiency.

This paper discusses a full range of qualification testing on the mechanicalunit. We completed thermal characterization to the point of regenerator saturation. We measured vibration export on a 6-axis dynamometer, and carried out vibration testing to 17 Grms. As a result of the vibration tests, we have corrected a few mistakes we made in our zeal to be more producible.

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References

  1. General Environmental Verification Specification (GEVS) for STS and ELV Payloads, Subsystems, and Components, Revision A, Table 2.4-4, Goddard Space Flight Center.

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  2. Gully, W.J., et al., “Qualification Test Results for a Dual-Temperature Stirling Cryocooler,” Cryocoolers 10, Klewer Academic/Plenum Publishers, New York, (1999), pp. 59–65.

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© 2003 Kluwer Academic Publishers

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Gully, W.J., Glaister, D., Marquardt, E., Stack, R., Wright, G.P. (2003). Thermodynamic Performance of the Ball Aerospace Multistage Stirling Cycle Mechanical Cooler. In: Ross, R.G. (eds) Cryocoolers 12. Springer, Boston, MA. https://doi.org/10.1007/0-306-47919-2_7

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  • DOI: https://doi.org/10.1007/0-306-47919-2_7

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-0-306-47714-0

  • Online ISBN: 978-0-306-47919-9

  • eBook Packages: Springer Book Archive

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