The features of two aircraft designs were selected to be included in the single RSRA configuration. A study was conducted for further preliminary design and a more detailed analysis of development plans and costs. An analysis was also made of foreseeable technical problems and risks, identification of parallel research which would reduce risks and/or add to the basic capability of the aircraft, and a draft aircraft specification.


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    Title :

    Rotor systems research aircraft predesign study. Volume 3: Predesign report


    Contributors:

    Publication date :

    1972-10-06


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :