Stratospheric airship is capable of station-keeping at high altitude in precondition of the balance of buoyancy and weight and of thrust and drag. Based on computation process, when some initial technology guidelines and conditions are supposed, the size of airship is gained and it is analyzed that certain technology guideline has more or less influence on length and payload of airship. It is concluded from the analyses that envelope mass/area ratio had the largest effect on key elements of airship, such as length and payload etc. Meanwhile, based on some available design parameters of typical traditional-shape airships being in development, the envelope mass/area ratio required for corresponding airships is scheduled for station-keeping at destine altitude and several technology approaches are proposed.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Feasibility Research on Traditional-Shape Stratospheric Airship


    Contributors:

    Published in:

    Advanced Materials Research ; 457-458 ; 1554-1566


    Publication date :

    2012-01-24


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Fin of stratospheric airship and stratospheric airship

    JIANG JING / GAO JUN / CHEN CHAOQUN et al. | European Patent Office | 2024

    Free access

    Airship capsule and stratospheric airship

    DUAN YI / JIANG JING / FU GONGYI et al. | European Patent Office | 2023

    Free access

    TRANSFORMABLE STRATOSPHERIC AIRSHIP

    ZHOU MENG / TAN BAIHE / XU ZHONGXIN et al. | European Patent Office | 2021

    Free access

    Semi-hard stratospheric airship framework and semi-hard stratospheric airship

    WANG ZENGJIA / FU GONGYI / DUAN MIYI et al. | European Patent Office | 2020

    Free access