A device includes a harness system configured to be attached to a parachute harness of a parachute. The device also includes a propulsion system connected to the harness system, wherein the propulsion system is configured to be off when undeployed and during freefall, and wherein the propulsion system is configured to deploy during canopy flight stage to generate thrust for a parachutist of the parachute. The device further includes a circuitry configured to control power generation by the propulsion system to control the thrust. The device includes a power source configured to power the circuitry and the propulsion system.


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    Title :

    PARACHUTE RANGE AUGMENTER


    Contributors:

    Publication date :

    2024-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    PARACHUTE RANGE AUGMENTER

    RHEA DAVID MICHAEL / FOX BENJAMIN MICHAEL | European Patent Office | 2024

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