Methods and systems for propelling an air vehicle with a molten salt reactor, a first heat exchanger, and a second heat exchanger are disclosed. A hot liquid molten salt from the molten salt reactor heats a fluid in the first heat exchanger to produce a hot fluid. The hot fluid heats air in the second heat exchanger to produce heated air which passes through a nozzle to propel the air vehicle.


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    Titel :

    High Speed Aircraft Propelled by Thorium or Uranium Fueled Molten Salt Reactor


    Beteiligte:
    KOTHARI AJAY P (Autor:in)

    Erscheinungsdatum :

    11.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G21C NUCLEAR REACTORS , Kernreaktoren / G21D NUCLEAR POWER PLANT , Kernkraftwerke



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