Attempt to ascertain the economic viability of the V/STOL capability for business aircraft and the manner in which this viability depends on the aircraft concept. A cost-benefit analysis is presented which indicates that a VTOL business aircraft would be more viable economically than a contemporary turbine-powered business aircraft. The combination of traveler's time value and trip distance for which each aircraft dominates is shown. The significance of disk loading in V/STOL concept application is discussed, and preliminary design configuration studies for three different business-aircraft-sized V/STOLs, using three concepts covering a range of disk loading, are presented as examples. Finally, a discussion of operational aspects of interest to future users of V/STOL business aircraft is presented which centers around the requirements for routine IFR terminal-area operations.


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    Titel :

    A look at V/STOL for business aircraft.


    Beteiligte:
    Feistel, T. W. (Autor:in) / Stewart, E. C. (Autor:in) / Gerdes, R. M. (Autor:in) / Smith, K. R., Jr. (Autor:in)

    Kongress:

    Society of Automotive Engineers, National Business Aircraft Meeting ; 1972 ; Wichita, KS


    Erscheinungsdatum :

    1972-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    A Look at V/STOL for Business Aircraft

    Stewart, E. C. / Smith, K. R. / Gerdes, R. M. et al. | SAE Technical Papers | 1972


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