1–16 von 16 Ergebnissen
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    Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions

    Grant, Michael / Clark, Ian / Braun, Robert | AIAA | 2011

    Rapid Entry Corridor Trajectory Optimization for Conceptual Design

    Grant, Michael / Clark, Ian / Braun, Robert | AIAA | 2010

    Aerothermodynamic Shape Optimization of Hypersonic Entry Aeroshells

    Theisinger, John / Braun, Robert / Clark, Ian | AIAA | 2010

    Survey of Blunt Body Dynamic Stability in Supersonic Flow

    Kazemba, Cole / Braun, Robert / Clark, Ian et al. | AIAA | 2012

    Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars

    Smith, Brandon / Hill, Jeremy / Clark, Ian et al. | AIAA | 2011

    An Evaluation of Ballute Entry Systems for Lunar Return Missions

    Clark, Ian / Braun, Robert / Theisinger, John et al. | AIAA | 2006

    High Mass Mars Entry, Descent, and Landing Architecture Assessment

    Steinfeldt, Bradley / Theisinger, John / Korzun, Ashley et al. | AIAA | 2009

    Application of a Method to Estimate Heating for Three-Dimensional Hypersonic Aeroshells

    Bopp, Matthew / Theisinger, John / Ruffin, Stephen et al. | AIAA | 2011

    Mars Entry, Descent, and Landing Parametric Sizing and Design Space Visualization Trades

    Alemany, Kristina / Wells, Grant / Theisinger, John et al. | AIAA | 2006

    Aerodynamic Stability and Performance of Next-Generation Parachutes for Mars Entry, Descent, and Landing

    Gonyea, Keir / Braun, Robert / Tanner, Christopher L. et al. | AIAA | 2013