Contents: Structural Loading Criteria; Summary of Minimum Margins of Safety; Analysis; Unoccupied Areas; Receiver Installation Models C-130E/H, WC-130E/H, HC-130H/N/P; Data Bus Coupler/Signal Splitter Installation Models C-130E/H, WC-130E/H, HC-130H/N/P; Receiver/Data Bus Coupler Installation Model C-130B; Signal Splitter/Relay Panel Installation Model C-130B; Front Antenna Installation; AFT Antenna Installation; AFT Antenna Installation; AFT Pressure Feed-Thru; Crew Occupied Areas; Top Antenna Installation; Relay Panel Installation; Relay Panel - Models C-130E/H/B; Relay Panel - Models C-130H (Late); Relay Panel - Models HC-130H/N/P, WC-130E/H; Forward Pressure Feed-Thru. (fr)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stress Analysis Report for the Microwave Landing System (MLS) Class V Modification C-130 Aircraft


    Erscheinungsdatum :

    1988


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Analysis of aircraft landing system integrity — The microwave landing system

    Cassell, Rick / Smith, Alex / Baldwin, Jon | IEEE | 1994



    Aircraft landing buffer device, aircraft landing control system and aircraft

    ZHOU GUANGZHAO / DU PENGFEI / YANG ZUYI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft landing blind landing system

    LIU JUN | Europäisches Patentamt | 2021

    Freier Zugriff

    The commutated doppler microwave landing system for aircraft - part 3

    Barratt, R.S. / Lawson, R.K. | Tema Archiv | 1976