The results are presented of a flight-test program utilizing a CV-990 airplane, flow in low-lift-to-drag-ratio (LD) configurations, to simulate terminal area operation, approach, and landing of large unpowered vehicles. The results indicate that unpowered approaches and landings are practical with vehicles of the size and performance characteristics of the proposed shuttle vehicle. Low LD landings provided touchdown dispersion patterns acceptable for operation on runways of reasonable length. The dispersion pattern was reduced when guidance was used during the final approach. High levels of pilot proficiency were not required for acceptable performance. (Author)


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    Titel :

    Low-Lift-TO-Drag-Ratio Approach and Landing Studies Using a Cv-990 Airplane


    Beteiligte:
    B. M. Kock (Autor:in) / F. L. Fulton (Autor:in) / F. J. Drinkwater (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Low-lift-to-drag-ratio approach and landing studies using a CV-990 airplane

    Kock, B. M. / Fulton, F. L. / Drinkwater, F. J., III | NTRS | 1972


    Low-lift-to-drag-ratio approach and landing studies using a CV-990 airplane

    Kock, Berwin M. / Fulton, Fitzhugh L. / Drinkwater, Fred J. | TIBKAT | 1972



    MINIMUM LIFT-DRAG RATIO REQUIRED FOR GLOBAL LANDING COVERAGE

    GRAY, W. A. / WALLACE, R. A. | AIAA | 1963