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person:(Lewis, Mark)

    Corrected Shock-Based Design for Waverider Geometries

    Chauffour, Marie-Laure / Lewis, Mark | AIAA | 2003

    Corrected Waverider Design for Inlet Applications

    Chauffour, Marie-Laure / Lewis, Mark | AIAA | 2004

    Coupled Entry Heat Shield/Trajectory Optimization for Lunar Return

    Johnson, Joshua / Lewis, Mark / Starkey, Ryan | AIAA | 2008

    Development of a Tool to Recreate the Mars Science Laboratory Entry Aerothermal Environment

    Beerman, Adam / Lewis, Mark / Santos, Jose et al. | AIAA | 2010

    DSMC of Power-Law Leading Edge Ionization for Hypersonic Telemetry Applications

    Hoult, Daniel / Starkey, Ryan / Lewis, Mark | AIAA | 2003

    Entry Heat Shield Optimization for Mars Return

    Johnson, Joshua / Lewis, Mark / Starkey, Ryan | AIAA | 2009

    Extending the Flight Mach Number of the SR-71 Inlet

    Colville, Jesse / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Functional Fault Modeling Conventions and Practices for Real-Time Fault Isolation

    Ferrell, Bob / Brown, Barbara / Lewis, Mark et al. | AIAA | 2010

    Functional Fault Modeling of a Cryogenic System for Real-Time Fault Detection and Isolation

    Oostdyk, Rebecca / Ferrell, Bob / Lewis, Mark et al. | AIAA | 2010

    Horizontal Launch Vehicle Weight Modeling for Future Lunar Exploration-Class Payloads

    Scott, Christopher / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Hypersonic aerodynamics test facility using the external propulsion accelerator

    Rom, Joseph / Lewis, Mark / Gupta, Ashwani et al. | AIAA | 1995

    Hypersonic Airplane Space Tether Orbital Launch (HASTOL) system - Interim study results

    Bogar, Thomas / Bangham, Michal / Forward, Robert et al. | AIAA | 1999