Description The spectrum of coverage of the volume includes aeroheating and thermal protection for high-velocity entry flight into the Earth's atmosphere (Space Shuttle), comet-like flight very close to the sun (Solar Starprobe), and entry into the gaseous envelope surrounding the planet Jupiter (Jupiter Galileo Probe).


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    Title :

    Development Of A Double-Wall Artery High-Capacity Heat Pipe


    Contributors:


    Publication date :

    1983-01-01




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English



    Development of a double-wall artery high capacity heat pipe

    PONNAPPAN, R. / MAHEFKEY, T. | AIAA | 1982


    Improved double-wall artery high capacity heat pipe

    PONNAPPAN, R. / BEAM, J. | AIAA | 1984


    Improved double-wall artery high-capacity heat pipe

    PONNAPPAN, R. / BEAM, J. E. / MAHEFKEY, T. | AIAA | 1985



    Analysis of evaporator critical heat flux in the double wall artery heat pipe

    PONNAPPAN, R. / RAMALINGAM, M. / JOHNSON, J. et al. | AIAA | 1988