A wind tunnel test was conducted using 0.05-scale models to study the separation characteristics of the SUU-51/B from the F-4C aircraft. The separation trajectories were initiated from the left-wing inboard pylon station utilizing the Triple Ejection Rack and from the centerline pylon utilizing the Multiple Ejection Rack. The flight conditions simulated were Mach numbers from 0.66 to 0.90 at an altitude of 5000 ft. Parent aircraft dive angles of 0, 30, and 45 deg were simulated. (Author)


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    Titel :

    Separation Characteristics of the SUU-51/B from the F-4C Aircraft


    Beteiligte:
    J. Kukainis (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    66 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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