Tests were conducted on the Rosemount Engineering Company Model 853 orthogonal true airspeed sensor to determine its suitability for operational and flight test use as an airspeed system for helicopters. The sensor has no moving parts, and operates on the principle that differential pressures, measured between a pair of orthogonal chambers, are proportional to the airspeed in a given direction. Flight tests at Edwards Air Force Base, California, were started on 24 January 1974 and were continued as additional hardware became available.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flight Evaluation: Rosemount Orthogonal Low Airspeed System Low Airspeed Sensor


    Beteiligte:
    R. P. Jefferis (Autor:in) / J. C. O'Connor (Autor:in) / J. R. Bullock (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    48 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Flight Evaluation - J-TEC Airspeed System

    F. Dominick / B. H. Boirun / J. S. Kishi et al. | NTIS | 1974


    Flight Evaluation Elliott Low-Airspeed System

    A. L. Winn / J. S. Kishi | NTIS | 1972


    Airspeed ambassador

    Engineering Index Backfile | 1947