The feasibility of using low-cost, portable computer technology to help a helicopter pilot optimize flight parameters to minimize fuel consumption and takeoff and landing noise was demonstrated. Eight separate computer programs were developed for use in the helicopter cockpit using a hand-held computer. The programs provide the helicopter pilot with the ability to calculate power required, minimum fuel consumption for both range and endurance, maximum speed and a minimum noise profile for both takeoff and landing. Each program is defined by a maximum of two magnetic cards. The helicopter pilot is required to key in the proper input parameter such as gross weight, outside air temperature or pressure altitude.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Helicopter Mission Optimization Study


    Contributors:
    J. R. Olson (author)

    Publication date :

    1978


    Size :

    122 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Helicopter mission optimization study

    Olson, John R. | TIBKAT | 1978


    Helicopter mission optimization study

    Olson, J. R. | NTRS | 1978


    Helicopter Mission Definition

    SAE Technical Papers | 1997


    Helicopter Engine Optimization for Minimum Mission Fuel Burn

    Alexiou, A. / Cobas, P. / Mathioudakis, K. et al. | British Library Conference Proceedings | 2013