Titlebook: Cryocoolers 13; Ronald G. Ross Conference proceedings 2005 Springer-Verlag US 2005 X-ray.development.modeling

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Lockheed Martin Two-Stage Pulse Tube Cryocooler for GIFTSripple suppression and vibration cancellation. The design is a “split” system in which the compressor and cold head are separated by a transfer line..The approach allows on orbit adjustment of the relative cooling loads and temperatures of the two stages..The controller provides precise temperature

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Ball Aerospace 4–10 K Space Cryocoolersatures down to 10 K, Ball has developed long life Stirling cycle cryocoolers. For temperatures to 4 K and below, Ball has developed a hybrid Stirling/J-T (Joule-Thomson) cooler. The hybrid cooler has been verified in test to 3.5 K on a Ball program and a 6 K Development Model is in development on th

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Status of Pulse Tube Cryocooler Development at Sunpowerd Space Flight Center. The first Phase II development effort between November 1999 and November 2001 established that a single-stage pulse tube driven by Sunpower’s manufactured linear compressor technology achieves efficient performance and promises to reach mass production costs similar to Sunpowe

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Development of a Small-Scale Collins-Type 10 K Cryocooler for Space Applicationsature levels ranging from 10K to 95K. A multi-stage 10K cryocooler is under development that applies microelectronic sophistication to achieve high efficiency in a reliable, compact design. The cryocooler is based upon a novel modification of the Collins cycle, a cycle commonly used in many high-eff