In support of the X-33 single-stage-to-orbit program, NASA Dryden Flight Research Center was selected to provide continuous range communications of the X-33 vehicle from launch at Edwards Air Force Base, California, through landing at Malmstrom Air Force Base Montana, or at Michael Army Air Field, Utah. An extensive real-time range simulation capability is being developed to ensure successful communications with the autonomous X-33 vehicle. This paper provides an overview of various levels of simulation, integration, and test being developed to support the X-33 extended range subsystems. These subsystems include the flight termination system, L-band command uplink subsystem, and S-band telemetry downlink subsystem.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    X-33 Integrated Test Facility Extended Range Simulation


    Contributors:

    Conference:

    International Telemetry Conference ; 1998 ; San Diego, CA, United States


    Publication date :

    1998-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    DLR-HR Compact Test Range Facility

    Limbach, Markus / Gabler, Bernd / Horn, Ralf et al. | German Aerospace Center (DLR) | 2009

    Free access

    X-33 Extended Flight Test Range

    D. A. Mackall / R. Sakahara / S. E. Kremer | NTIS | 1998


    Light assembly with integrated test facility

    MARK JORDAN / TOM WARD / DANIEL FOSTER et al. | European Patent Office | 2020

    Free access