Described herein are features for a high altitude lighter-than-air (LTA) system and associated methods. A zero-pressure balloon (ZPB) is attached in tandem with one or more air super-pressure balloons (SPB). The ZPB provides lift for the system while the SPB may provide a variable amount of ballast air by pumping in or expelling out ambient air. Various advanced performance targets relating to ascent rate, descent rate, range and maximum altitude are achievable with various scaled versions of the basic design of the LTA system. Advanced navigation and control techniques, such as more efficient high altitude station-keeping approaches, made possible with the LTA system are also described.


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    Titel :

    HIGH ALTITUDE BALLOON SYSTEMS AND METHODS


    Beteiligte:
    MACCALLUM TABER KYLE (Autor:in) / PADILLA SEBASTIAN (Autor:in) / FARLEY RODGER (Autor:in) / BEVERIDGE IAIN (Autor:in) / LEE G RYAN (Autor:in) / BASTA TIM (Autor:in) / LEIDICH JARED (Autor:in) / STRAUS JOHN (Autor:in) / MACCAGNANO JOHN Z (Autor:in)

    Erscheinungsdatum :

    2021-10-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



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