The S/MTD program has generated flight test data to validate four specific technologies: 2-D thrust vectoring & reversing nozzle; integrated flight/propulsion control; advanced pilot/vehicle interface including autonomous landing guidance; and rough field/high sink rate landing gear. These technologies have been integrated into an F-15B to provide mission benefits across the complete flight envelope from on-board guidance to a bad weather short landing, through significantly enhanced maneuvering benefits to supersonic performance. These technologies are either transitioning on to other aircraft, or can be considered viable design options for future aircraft.


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    Titel :

    Results from the STOL and Maneuver Technology Demonstration Program


    Beteiligte:

    Erscheinungsdatum :

    1994


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Results from the STOL and Maneuver Technology Demonstration Program

    Moorhouse, D. J. / Advisory Group for Aerospace Research and Development; Flight Mechanics Panel | British Library Conference Proceedings | 1994


    Results and Lessons Learned from the STOL & Maneuver Demonstration Program

    Moorhouse, David J. / Laughrey, James A. | SAE Technical Papers | 1991



    An Overview of the STOL and Maneuver Technology Demonstration Program

    Moorhouse, D. / AIAA | British Library Conference Proceedings | 1994


    STOL and Maneuver Technology Program

    Selegan, David R. | SAE Technical Papers | 1983