In early nineties Mars was designated as the planet to be explored. The present results of Mars program include the following: Background of Mars program. Thermal control design for Martian spacecraft. Loop heat pipe for Lander and Rover. Test results. and LHP applications for future Martian Lander and Rover.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Loop Heat Pipe Applications for Thermal Control of Martian Landers/Rovers


    Contributors:
    G. Birur (author) / J. Rodriquez (author) / M. Nikitkin (author)

    Publication date :

    1999


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Loop Heat Pipe Applications for Thermal Control of Martian Landers/Rovers

    Birur, Gaj / Rodriquez, Jose / Nikitkin, Michael | NTRS | 1999


    Loop Heat Pipe Applications for Thermal Control of Martian Landers/Rovers

    Nikitkin, M. / Rodriguez, J. / Birur, G. | NTRS | 1999


    Loop Heat Pipe with Thermal Control Valve for Variable Thermal Conductance Link of Lunar Landers and Rovers

    Hartenstine, John / Anderson, William / Walker, Kara et al. | AIAA | 2011


    Thermal control of Mars rovers and landers using mini loop heat pipes

    Birur, G. C. / Pauken, M. T. / Novak, K. S. | NTRS | 2002


    LOOP HEAT PIPE WITH THERMAL CONTROL VALVE FOR VARIABLE THERMAL CONDUCTANCE LINK OF LUNAR LANDERS AND ROVERS

    Hartenstine, J. / Anderson, W. / Walker, K. et al. | British Library Conference Proceedings | 2011