Significant improvements in thermal management technologies will be required to support NASA’s planned Lunar and Mars missions. The developments needed include the application of advanced materials to reduce radiator system masses, enhanced survivability, and the use of alternative working fluids. Current thermal management systems utilize one of two heat rejection alternatives; either single phase pumped loops, or two phase heat pipes constructed with thick walled metal casings. These two technologies have proven themselves to be reliable performers in the transport and rejection of waste heat from spacecraft. As thermal management needs increase with increased power consumption and activity required on spacecraft, these metal based thermal management systems will become mission limiting. Investigations into the use of light weight ceramic materials for high temperature thermal management systems have been conducted by NASA, the Department of Energy, and the Department of Defense since the early 1980s, with results showing that significant mass savings can be obtained by replacing some of the metallic functions with ceramic materials.


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    Titel :

    Advanced thermal management needs for Lunar and Mars missions


    Beteiligte:
    Klein, Andrew C. (Autor:in) / Webb, Brent J. (Autor:in) / El-Genk, Mohamed S. (Herausgeber:in) / Hoover, Mark D. (Herausgeber:in)

    Kongress:

    10th SymposiumùSpace Nuclear Power and Propulsion ; 1993 ; Albuquerque, NM, USA


    Erschienen in:

    AIP Conference Proceedings ; 271 , 2 ; 847-851


    Erscheinungsdatum :

    15.01.1993


    Format / Umfang :

    5 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Advanced Thermal Management Needs for Lunar and Mars Missions

    Klein, A. C. / Webb, B. J. / American Institute of Physics | British Library Conference Proceedings | 1993


    Propulsion needs for lunar/Mars missions

    Woodcock, Gordon R. | NTRS | 1990


    Propulsion Needs for Lunar/Mars Missions

    G. R. Woodcock | NTIS | 1990