- Recent NASA missions have included total heat flux sensors (THFS) embedded in the thermal protection system (TPS) to measure the combined convective and radiative heating during atmospheric entry. These measurements are key to fundamental entry science and mission design. - The THFSs for the Mars Entry, Descent, and Landing Instrumentation 2 (MEDLI2) sensor suite on the Mars 2020 entry vehicle and the Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) technology demonstration mission were passively cooled Schmidt–Boelter gauges. - As presented at IPPW 2021, THFS calibration is notoriously difficult and includes several sources of measurement uncertainty [1]. - Recent work has been conducted to understand and quantify the measurement uncertainty in the MEDLI2 and LOFTID Schmidt-Boelter THFSs.


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    Titel :

    Atmospheric Entry Heat Flux Sensor Calibration and Flight Data Analysis


    Beteiligte:
    R. A. Miller (Autor:in) / H. S. Alpert (Autor:in) / G. T. Swanson (Autor:in) / C. Y. Tang (Autor:in)

    Erscheinungsdatum :

    2023


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Advanced In-flight Sensor Systems for Atmospheric Entry Maneuvers

    Auweter-Kurtz, Monika / Fertig, Markus / Herdrich, Georg et al. | AIAA | 2004


    A study on heat flux predictions for re-entry flight analysis

    Park, Seong-Hyeon / Neeb, Dominik / Plyushchev, Gennady et al. | Elsevier | 2021


    UNCERTAINTY QUANTIFICATION OF RADIATIVE HEAT FLUX MODELING FOR TITAN ATMOSPHERIC ENTRY

    Ghaffari, S. / Magin, T. / Iaccarino, G. et al. | British Library Conference Proceedings | 2010


    Uncertainty Quantification of Radiative Heat Flux Modeling for Titan Atmospheric Entry

    Ghaffari, Shirin / Magin, Thierry / Iaccarino, Gianluca | AIAA | 2010