This tutorial presents a summary of the environments, problems, and performance of the on-board instrumentation used on the U.S. Air Force Space and Missile Systems Organization (SAMSO) flight test programs to measure reentry vehicle (RV) performance. In addition, a brief description of the off-board instrumentation will be presented. In RV instrumentation, the specific discipline performance areas covered are the thermodynamic and the aerodynamic. Within the aerodynamic discipline are the group of instruments concerned with RV dynamics (gyros, magnetometers, etc.) and with RV fluid dynamic measurements (boundary layer transition and progression sensors, etc.). The thermodynamic instruments include radiation sensors, multiwire isothermal thermocouples, optical seedants, acoustic sensors, calorimeters, etc. The overriding objective of this tutorial is to provide the instrumentation supplier with a detailed feeling for SAMSO's RV instrumentation problems so that the supplier will be able to propose better instruments to solve these problems. (Author)


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    Titel :

    The Challenge of Reentry Vehicle Instrumentation


    Beteiligte:
    P. J. Legendre (Autor:in) / R. G. Fowler (Autor:in) / J. M. Cassanto (Autor:in) / W. R. Grabowsky (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    140 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Reentry vehicle nosetip instrumentation

    Legendre, P.J. | Tema Archiv | 1975


    Reentry vehicle instrumentation survey

    GRABOWSKY, W. / ELDRIDGE, H. / WHEATON, R. | AIAA | 1981