An assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, associated with the V/STOL technology airplane is presented. The risk is discussed in terms of weight, structure, aerodynamics, propulsion, mechanical drive, and flight controls. The analysis ensures that risks associated with the design and development of the airplane will be eliminated in the course of the program and a useful technology airplane that meets the predicted cost, schedule, and performance can be produced. (Author)


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    Title :

    Design Definition Study of a NASA/Navy Lift/Cruise Fan Technology V/STOL Airplane: Risk Assessment Addendum to the Final Report


    Contributors:
    J. M. Zabinsky (author) / R. W. Burnham (author) / C. C. Flora (author) / P. Gotlieb (author) / D. L. Grande (author)

    Publication date :

    1975


    Size :

    54 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English