Thrust with the minimum ejection of propellant by a levitating mass blocking the exhaust stream within the propellant producing structure. The reaction of accumulated propellant pressure between the levitating mass the hollow passageway and the propellant producing engine create thrust thus propelling the propellant producing engine and the vehicle in which it is mounted. Fuel consumption is decrease because a significant amount of propellant is not allowed to escape and is trapped in the vehicle's structure. The levitating mass is not physically attached to the propellant producing engine or the vehicle's structure. The rated pounds of thrust can be significantly increase and is determine by the strength of the magnetic field holding the levitating mass in place the composition of the hollow passageway the mechanical and structural components of the propellant producing engine.


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    Titel :

    THRUST WITH THE MINIMUM EJECTION OF PROPELLANT


    Beteiligte:

    Erscheinungsdatum :

    2022-02-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / B63H Schiffsantrieb oder Steuerung der Schiffe , MARINE PROPULSION OR STEERING / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    On minimum propellant paths for thrust limited rockets

    Keller, J.L. | Engineering Index Backfile | 1964




    High-thrust mechanism for ejection device, ejection system and ejection method

    GUO JIUMING / MA XIAOXIAO / LI YANMING et al. | Europäisches Patentamt | 2021

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