Airspeed calibration tests were conducted on the Pacer Systems, Inc. LORAS II low-range airspeed system to determine its suitability for use as a helicopter airspeed instrument. Testing was conducted by the United States Army Aviation Systems Test Activity at Edwards Air Force Base, California between 29 January and 5 July 1973. The evaluation required 17.2 productive flight test hours. (Modified author abstract)


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    Title :

    Flight Evaluation - Pacer Systems, Inc. LORAS II Airspeed System


    Contributors:
    B. H. Boirun (author) / F. Dominick (author) / J. S. Kishi (author) / R. K. Merrill (author) / J. R. Smith (author)

    Publication date :

    1974


    Size :

    65 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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