Adaptable, Deployable, Entry, and Placement Technology (ADEPT) is a combination of a heatshield and an aerodynamic decelerator for atmospheric entry applications. The ADEPT Sounding Rocket (SR)-1 mission was a suborbital flight experiment of an 0.7 m-diameter ADEPT to verify system-level performance and to characterize dynamic stability behavior. The aerodynamic database for ADEPT SR-1 was constructed from non-continuum and continuum flowfield computations, along with data from recent ADEPT ground testing and the IRVE-3 flight test vehicle. High-altitude (free-molecular and transitional regimes) data were generated using DSMC methods. Pre-flight predictions of continuum static aerodynamics coefficients were derived from Reynolds-Averaged Navier-Stokes solutions at conditions along a design trajectory, with comparisons to available ground test data of the nano-ADEPT geometry. Dynamic pitch damping characteristics were taken from functional forms developed for the IRVE-3 flight test vehicle through ballistic range testing. Comparison of pre-flight predictions to post-flight reconstruction of aerodynamic force and moment coefficients is presented.


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    Titel :

    Aerodynamics for the ADEPT SR-1 Flight Experiment


    Beteiligte:

    Kongress:

    AIAA SciTech Forum and Exposition ; 2019 ; San Diego, CA, United States


    Erscheinungsdatum :

    2019-01-07


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamics for the ADEPT SR-1 Flight Experiment

    Korzun, Ashley M. / Dutta, Soumyo / McDaniel, Ryan D. et al. | AIAA | 2019


    AIAA-2019-2897: Aerodynamics for the ADEPT SR-1 Flight Experiment

    Korzun, Ashley M. / Dutta, Soumyo / McDaniel, Ryan D. et al. | British Library Conference Proceedings | 2019


    ADEPT SR-1 Flight Experiment

    P. F. Wercinski | NTIS | 2017


    ADEPT SR-1 Flight Experiment

    Wercinski, Paul F. | NTRS | 2017


    ADEPT sounding rocket one (SR-1) flight experiment overview

    Wercinski, Paul / Smith, Brandon / Yount, Bryan et al. | IEEE | 2017