Paper considers design status (as of Dec 1964) of L-2000 with respect to features assuring safe, reliable, and comfortable travel under Mach-3 cruising flight conditions; system design to cope with speed-induced thermal environment of 2000 mph transport requires effective thermal management of all major heat sources and sinks; selection of heat sinks for L-2000 and vehicle characteristics that make this choice feasible; effects of flight profile (cruising altitude, in particular), airplane configuration, and significant modes of heat transfer both external and internal; subsystem concepts providing desired internal environment for occupants and equipment.


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    Title :

    Thermal management of Lockheed model 2000 supersonic transport


    Additional title:

    ASME -- Paper


    Contributors:

    Conference:

    ASME Meeting AV-40 ; 1965 Supersonic



    Publication date :

    1965


    Size :

    15 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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