Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Robust Aerial Deployment of Mars Airplane with Tilted Folding-Axis (AIAA 2016-0023)


    Contributors:
    Fujita, Koji (author) / Nagai, Hiroki (author) / Oyama, Akira (author)

    Conference:

    AIAA Atmospheric Flight Mechanics Conference 2016 ; 2016 ; San Diego



    Publication date :

    2016-01-01


    Size :

    15 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Robust Aerial Deployment of Mars Airplane with Tilted Folding-Axis

    Fujita, Koji / Nagai, Hiroki / Oyama, Akira | AIAA | 2016


    Mars Helicopter Technology Demonstrator (AIAA 2018-0023)

    Balaram, Bob / Canham, Timothy / Duncan, Courtney et al. | British Library Conference Proceedings | 2018


    ICAS2016_0477: EFFECT OF YAW-TILTED HINGE AXIS ON DEPLOYMENT ROBUSTNESS OF MARS AIRPLANE

    Fujita, K. / Nagai, H. / Oyama, A. | British Library Conference Proceedings | 2016


    Conceptual Wing Design Methodology for Aircraft with Hybrid Laminar Flow Control (AIAA 2014-0023)

    Risse, K. / Schueltke, F. / Stumpf, E. et al. | British Library Conference Proceedings | 2014


    Numerical analysis for an aerial deployment motion of a folded-wing airplane (AIAA 2014-0383)

    Fujita, K. / Motoda, T. / Nagai, H. et al. | British Library Conference Proceedings | 2014