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CEC-ICMC 2017 - Abstracts, Timetable and Presentations

9–13 Jul 2017
Monona Terrace Community and Convention Center
US/Central timezone

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Session

C4OrD - Aerospace Cryocoolers II

C4OrD
13 Jul 2017, 09:30
Monona Terrace Community and Convention Center

Monona Terrace Community and Convention Center

Madison, Wisconsin USA

Conveners

C4OrD - Aerospace Cryocoolers II

  • Peter Shirron (NASA / GSFC)
  • Ted Conrad (Raytheon Space and Airborne Systems)

Presentation materials

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  1. 539. MIRI Cooler Subsystem Test Facility Design and Performance
    Bradley Moore (JPL/Caltech)
    13/07/2017, 10:00
    Contributed Oral Presentation

    The Cryocooler for the Mid Infrared Instrument (MIRI) on the James Webb Space Telescope (JWST) provides cooling at 6.2K on the instrument interface. The system design has been incrementally documented in previous publications and has components that traverse three primary thermal regions on JWST: Region 1, approximated by 40K; Region 2, approximated by 100K; and Region 3, which is at the...

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  2. 454. Ball Aerospace Scalable Configurable Cryocooler Electronics (SCCE)
    Eric Marquardt (Ball Aerospace)
    13/07/2017, 10:15
    Contributed Oral Presentation

    Perceiving a need for space-qualified tactical cryocoolers suitable for shorter, higher risk-tolerant missions, Ball established a new approach to cryocooler electronics. An entirely new architecture, rooted in past experience and optimized with today’s technology, was developed that could be scaled to different power needs and could be configured for different missions or coolers as...

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  3. 4. Characterization Testing of Lockheed Martin High-Power Micro Pulse Tube Cryocooler
    Ian McKinley (Jet Propulsion Laboratory)
    13/07/2017, 10:30
    Contributed Oral Presentation

    This paper describes the thermal performance, exported vibration, and magnetics testing and results of a Lockheed Martin high-power micro pulse tube cryocooler. The thermal performance of the microcooler was measured in vacuum for heat reject temperatures between 200 and 300 K. The cooler was driven with a Chroma 61602 AC power source for input powers ranging from 10 to 60 W and drive...

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  4. 405. Advances in single- and multi-stage Stirling-type pulse tube cryocoolers for space applications in NLIP/SITP/CAS
    Prof. Haizheng Dang (National Laboratory for Infrared Physics, Shanghai Institute of Technical Physics, Chinese Academy of Sci)
    13/07/2017, 10:45
    Contributed Oral Presentation

    This paper presents a review of recent advances in single- and multi-stage Stirling-type pulse tube cryocoolers (SPTCs) for space applications in National Laboratory for Infrared Physics, Shanghai Institute of Technical Physics, Chinese Academy of Sciences (NLIP/SITP/CAS).
    A variety of single-stage SPTCs covering 25–150 K become mature, in which several mid-sized ones operating in 80–110 K...

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  5. 61. Status of Pulse Tube Cryocooler Development at SITP, CAS
    Dr ankuo zhang (Shanghai Institute of Technical Physics, Chinese Academy of Sciences)
    13/07/2017, 11:00
    Contributed Oral Presentation

    The development of pulse tube cryocoolers (PTCs) at Shanghai Institute of Technical Physics, Chinese Academy of Sciences (SITP, CAS) is presented. These PTCs can provide cooling power from mW to tens of watts over a range of temperatures from 20 K to 170 K, which can be used to cool varieties of detectors in space applications, such as quantum interference device, radiometer, ocean color...

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