The objective of this study was to determine the feasibility of refueling V/STOL aircraft, including helicopters, by means of a ship-based refueling device which would circumvent the need for landing. Twp alternative high fuel flow rate systems are projected through exploratory designs. Feasibility is indicated through analyses of solutions required to support and stabilize the refueling device for engagement by V/STOL aircraft within the limits of available aircraft control power in a sea state 5 environment.


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    Title :

    Study of Ship Based Inflight Refueling of V/STOL Aircraft


    Publication date :

    1981


    Size :

    144 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English