Thermal-structural testing of three hot structure control surface subcomponent test articles (STA) designed for the X-37 (Boeing Phantom Works, Huntington Beach, California) Orbital Vehicle (OV) has been completed. The test articles were subcomponents of the X-37 OV bodyflap and flaperon control surfaces.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The X-37 Hot Structure Control Surface Testing


    Contributors:


    Publication date :

    2006-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    X-37 Hot Structure Control Surface Testing

    L. D. Hudson / C. A. Stephens | NTIS | 2006


    Control surface clearance testing equipment

    LUO WEI / WANG QI / NI LINXUAN et al. | European Patent Office | 2020

    Free access

    Load testing for flight control surface

    PERRY PAULINE | European Patent Office | 2022

    Free access

    Airplane control surface structure

    WANG ZHIGANG / XIAO WEIPING / FU SHUO | European Patent Office | 2024

    Free access

    Control surface mounting structure

    FU JIEBIN / HE FEI / CHEN LIGEN et al. | European Patent Office | 2022

    Free access