1–20 of 76 hits
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    Integrated Propulsion and Power Modeling for Bimodal Nuclear Thermal Rockets

    Clough, Joshua / Starkey, Ryan / Lewis, Mark et al. | AIAA | 2007

    Reactor Modeling for Bimodal Nuclear Thermal Rockets

    Clough, Joshua / Starkey, Ryan / Lewis, Mark et al. | AIAA | 2006

    A Design Comparison of Atmospheric Flight Vehicles for the Exploration of Titan

    Gasbarre, Joseph / Wright, Henry / Lewis, Mark | AIAA | 2005

    Inverse Waverider Design for Inward Turning Inlets

    Barkmeyer, Daniel / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Extending the Flight Mach Number of the SR-71 Inlet

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

    Investigation of Two-Stage-to-Orbit Air-Breathing Launch Vehicle Configurations

    Dissel, Adam / Kothari, Ajay / Lewis, Mark | AIAA | 2005

    Weight Growth Study of Reusable Launch Vehicle Systems

    Dissel, Adam / Kothari, Ajay / Lewis, Mark | AIAA | 2005

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

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

    Aerodynamic Stability of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle

    Johnson, Joshua / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    System Analysis of Launch Transportation Options for Crew Exploration Vehicle

    Dissel, Adam / Kothari, Ajay / Raghavan, Venkat et al. | AIAA | 2005

    Corrected Waverider Design for Inlet Applications

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

    Transient Rarefaction Models for Hypersonic Blowdown Tunnels

    Smith, Kerrie / Lewis, Mark | AIAA | 2004

    Component Matching for the Air Turborocket

    Clough, Joshua / Lewis, Mark | AIAA | 2004

    Aerodynamics for Optimal Engine-Integrated Airbreathing Launcher Configurations

    Lewis, Mark / Boyd, I. / Cockrell, Charles | AIAA | 2004

    Comparison of HTHL and VTHL Airbreathing and Rocket Systems for Access to Space

    Dissel, A. / Kothari, Ajay / Raghavan, V. et al. | AIAA | 2004