Multi-turbine engine aircraft developed by McDonnell Aircraft Corp, St.Louis, Mo, has empty weight of 2400 lb and takeoff gross weight of 6300 lb; useful load is 62% of gross weight, achieved by using pressure jet powered rotor; compressed air for pressure jets supplied by three AiResearch GTC-85-35 gas turbine compressors.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    McDonnell's private venture model 120


    Additional title:

    Am Helicopter


    Contributors:
    Berry, M. (author)

    Published in:

    Publication date :

    1958


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :