System is described which can, besides accurately measuring and displaying loaded aircraft's take-off gross weight and center of gravity (CG) in digital form in cockpit or load-station, provide in-flight weight and CG determination as well by accepting fuel flow meter readouts; called STAN (summed total and nosegear); it can also, through incorporation of computer technology, take inputs from engines, barometric altimeter, temperature gages, and wind speed, airspeed and ground speed indicators, etc, and provide accurate "Go - No Go" system for pilot to provide him with rotation velocity point at which he must become airborne or abort flight.


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    Title :

    Self contained aircraft weight and balance system


    Additional title:

    IEEE -- Nat Aerospace Electronics Conference -- Proc


    Contributors:

    Conference:

    17th IEEE -- National Aerospace and Navigational Electronics Conference ; 1965 Loading



    Publication date :

    1965


    Size :

    7 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Aircraft weight and balance

    Anderson, W.C. / Rocke, J.W. | Engineering Index Backfile | 1949


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