This final report summarizes the work performed on the development of a Three (3) Axis Accelerometer. The accelerometers were developed for determination of atmospheric density at low satellite altitudes by sensing the satellite deceleration due to aerodynamic drag. Systems no. 1 and no. 2 were successfully flown on the Air Force low altitude density research satellites CANNON BALL I and SPADES respectively. Three triaxial accelerometer systems were delivered to AFCRL. The funded contract activity, which began on 1 December 1966, was completed on 18 December 1970 with the delivery of Three Axis System no. 3. (Author)


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    Titel :

    Design and Development of a 3-Axis Accelerometer (Mesa)


    Beteiligte:
    W. G. Lange (Autor:in) / M. M. Meldrum (Autor:in) / D. W. Honkala (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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