The Pegasus air-launched space booster successfully completed its maiden flight on April 5, 1990. Many recent advances in digital avionics and computer technology simplified the vehicle and its testing. The single-string Pegasus avionics comprise multiple microcontroller-based remote units for controlling actuators, firing thrusters and pyrotechnics, and gathering telemetry arranged in a serial digital star network centered on the VMEBUS flight computer. Flight, aircraft, and test software is in C, with small amounts of FORTH and assembly language. A series of laboratory, simulation, mobile test bed, motor static firing, and captive flight tests verified that the avionics system was ready for free flight.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Pegasus avionics system design


    Weitere Titelangaben:

    Systementwurf für die Pegasus-Avionik


    Beteiligte:
    Steffy, D.A. (Autor:in)


    Erscheinungsdatum :

    1990


    Format / Umfang :

    7 Seiten, 3 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Pegasus thermal design

    Bannister, T. C. / Eby, R. J. | NTRS | 1966


    Pegasus thermal design

    Bannister, Tommy C. / Eby, Robert J. | TIBKAT | 1966


    Pegasus Thermal Design

    T. C. Bannister / R. J. Eby | NTIS | 1966



    Pegasus thermal design

    Bannister, T. C. | NTRS | 1965