The results of a design study resulting in the proposed CONDOR aircraft are presented. The basic requirements are for the aircraft to maintain continuous altitude at or above 45,000 feet for at least a 3-day mission, be able to comfortably support a two-man crew during this period with their field of vision not obstructed to a significant degree, carry a payload of 200 pounds, and provide a power supply to the payload of 2000 watts. The take-off and landing distances must be below 5000. feet, and time to reach cruise altitude must not exceed 3 hours. The subjects discussed are configuration selection, structural analysis, stability and control, crew and payload accomodations, and economic estimates.


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    Titel :

    CONDOR: Long endurance high altitude vehicle, volume 5


    Beteiligte:
    Andrews, L. Cullen (Autor:in) / Augsburger, Bill (Autor:in) / Cote, Thomas (Autor:in) / Ghitea, Mihael (Autor:in) / Lee, Il Sik (Autor:in) / Lee, Susik (Autor:in) / Leong, Gary (Autor:in)

    Erscheinungsdatum :

    1988-06-11


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    CONDOR: Long Endurance High Altitude Vehicle, Volume 5

    L. C. Andrews / B. Augsburger / T. Cote et al. | NTIS | 1988





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