The testing of 3- and 6-meter diameter Hypersonic Inflatable Aerodynamic Decelerator (HIAD) test articles was completed in the National Full-Scale Aerodynamics Complex 40 ft x 80 ft Wind Tunnel test section. Both models were stacked tori, constructed as 60 degree half-angle sphere cones. The 3-meter HIAD was tested in two configurations. The first 3-meter configuration utilized an instrumented flexible aerodynamic skin covering the inflatable aeroshell surface, while the second configuration employed a flight-like flexible thermal protection system. The 6-meter HIAD was tested in two structural configurations (with and without an aft-mounted stiffening torus near the shoulder), both utilizing an instrumented aerodynamic skin.


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    Titel :

    Design and Execution of the Hypersonic Inflatable Aerodynamic Decelerator Large-Article Wind Tunnel Experiment


    Beteiligte:

    Kongress:

    10th International Planetary Probe Workshop ; 2013 ; San Jose, CA, United States


    Erscheinungsdatum :

    2013-06-17


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Design and Execution of the Hypersonic Inflatable Aerodynamic Decelerator Large-Article Wind Tunnel Experiment

    Cassell, A. / Swanson, G.T. / Quach, B. et al. | British Library Conference Proceedings | 2013


    Morphing Hypersonic Inflatable Aerodynamic Decelerator

    Green, Justin S. / Dunn, Barry / Lindberg, Robert | AIAA | 2013


    Morphing Hypersonic Inflatable Aerodynamic Decelerator

    Green, J.S. / Dunn, B. / Lindberg, R. et al. | British Library Conference Proceedings | 2013