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    Chapter

    Performance Testing of a Lightweight, High Efficiency Cooler

    A lightweight, high efficiency cryocooler has been tested. The design operating point of the cooler is 10 W at 95 K with a rejection temperature of 300 K, and the goal is a 10 yr operating lifetime. The cooler...

    L. J Salerno, P Kittel, B. P. M Helvensteijn, A Kashani in Cryocoolers 12 (2003)

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    Chapter

    Cryocoolers for Human and Robotic Missions to Mars

    Future missions to Mars will make use of a number of different cryocoolers. These cryocoolers will be used to liquefy and preserve propellants and for transporting liquid hydrogen feed stock. The earliest miss...

    P. Kittel, L.J. Salerno, D.W. Plachta in Cryocoolers 10 (2002)

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    Chapter

    Terrestrial Applications of Zero-Boil-Off Cryogen Storage

    Storing cryogenic propellants with zero boil off (ZBO) using a combination of active (cryocoolers) and passive technologies has recently received a great deal of attention for longterm space missions. This pap...

    L. J. Salerno, J. Gaby, R. Johnson, P. Kittel, E. D. Marquardt in Cryocoolers 11 (2002)

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    Chapter

    Measuring Thermal Conductivity of Insulators at Cryogenic Temperatures

    Traditionally, launch vehicles have consisted of a structure containing the vehicle engines, propellant tanks, and electronics. NASA’s next generation of space transportation vehicles is planned to utilize the...

    B. P. M. Helvensteijn, L. J. Salerno, P. R. Roach… in Advances in Cryogenic Engineering (2000)