General and specific turbojet design considerations for application in pure hoverjet aircraft; attempt made to establish overall power plant requirements, to define desirable characteristics and to indicate approaches toward improvement of engine specific weight through component design; factors required in maximizing transport range/payload performance are minimum overall to gross weight ratio, minimum hover time, and minimum life engine specific weight.


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    Title :

    Turbojet lift engine design for VTOL transports


    Additional title:

    Can Aeronautical J


    Contributors:
    Saari, M.J. (author)

    Published in:

    Publication date :

    1959


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English