The goal of the current work was to develop an analytical framework for design of composite struts using various levels of model fidelity. An additional goal of this work was to perform an initial assessment of using automated fiber placement (AFP) and other advanced manufacturing methods to explore their feasibility for the fabrication of struts for lunar landers, strut-braced wings, and other aerospace components. In particular, designs were considered for fabrication at the Integrated Structural Assembly of Advanced Composites (ISAAC) facility at Langley Research Center (LaRC). The designs presented in this paper do not represent the exact geometry and material systems currently in use by the Artemis landing system, but they are considered to be representative. The designs produced during this study will be used to develop manufacturing demonstration units (MDU) that can be fabricated at ISAAC and tested in lab facilities at LaRC


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    Titel :

    Design of a Manufacturing Demonstration Unit for a Composite Lunar Landing Gear Strut


    Beteiligte:
    Brian H Mason (Autor:in) / Alana Zahn (Autor:in) / Kevin E Gould (Autor:in) / Adam Przekop (Autor:in)

    Kongress:

    2021 AIAA SciTech Forum ; 2021 ; Nashville, TN, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design of a Manufacturing Demonstration Unit for a Composite Lunar Landing Gear Strut

    Brian H Mason / Alana Zahn / Kevin E. Gould et al. | NTRS


    Design of a Manufacturing Demonstration Unit for a Composite Lunar Landing Gear Strut

    Mason, Brian H. / Zahn, Alana / Gould, Kevin et al. | AIAA | 2021


    DESIGN OF A MANUFACTURING DEMONSTRATION UNIT FOR A COMPOSITE LUNAR LANDING GEAR STRUT

    Mason, Brian H. / Zahn, Alana / Gould, Kevin et al. | TIBKAT | 2021


    COMPOSITE LUG FOR LANDING GEAR STRUT

    LUCE WILLIAM E | Europäisches Patentamt | 2018

    Freier Zugriff