Five XC-142 aircraft have been manufactured to provide operational prototypes of a V/STOL tactical transport for tri-service evaluation. This paper presents a description of the flight control and stability augmentation systems. Special emphasis is placed on the programmed functions which are characteristic of VTOL airplanes. Proposed changes in the control systems of production models of the C-142 are identified, and the simulation and flight test programs are outlined.


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    Titel :

    XC-142A Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Fling, G. K. (Autor:in)

    Kongress:

    Aerospace Systems Conference and Engineering Display ; 1967



    Erscheinungsdatum :

    1967-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    XC-142A propulsion system

    Carter, H.F. | Engineering Index Backfile | 1964


    THE XC-142A PROPULSION SYSTEM

    Carter, Howard F. | SAE Technical Papers | 1964