1–10 von 12 Ergebnissen
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    Mars Sample Return using commercial capabilities: Propulsive Entry, Descent, and Landing

    Lemke, Lawrence G. / Gonzales, Andrew A. / Huynh, Loc C. | IEEE | 2014

    Mars Sample Return Using Commercial Capabilities: Propulsive Entry, Descent and Landing

    Lemke, Lawrence G. / Gonzales, Andrew A. / Huynh, Loc C. | NTRS | 2014

    Mars Sample Return: Mars Ascent Vehicle Mission and Technology Requirements

    Bowles, Jeffrey V. / Huynh, Loc C. / Hawke, Veronica M. et al. | NTRS | 2013

      Mars Sample Return: Mars Ascent Vehicle Mission and Technology Requirements

      Bowles, Jeffrey V. / Huynh, Loc C. / Hawke, Veronica M. | NTRS | 2013

    Advanced vehicle concepts systems and design analysis studies

    Waters, Mark H. / Huynh, Loc C. | NTRS | 1994

    Feasibility Study of A Direct-to-Earth Mars Sample Return Architecture Using a Dragon-Derived Mars Lander

    Lemke, Lawrence G. / Bowles, Jeffrey V. / Gonzales, Andrew A. et al. | NTRS | 2013

    Analysis of a hypersonic waverider research vehicle with a hydrocarbon scramjet engine

    Molvik, Gregory A. / Bowles, Jeffrey V. / Huynh, Loc C. | NTRS | 1993

    Economic Optimization of an Advanced Subsonic Transport

    Huynh, Loc C. / Moore, Mark D. / Waters, Mark H. et al. | SAE Technical Papers | 1997

    Comparison of Elastic and Rigid Blade-Element Rotor Models Using Parallel Processing Technology for Piloted Simulations

    Hill, Gary / Green, John A. / Huynh, Loc C. et al. | SAE Technical Papers | 1991

    A comparison of real-time blade-element and rotor-map helicopter simulations using parallel processing

    Corliss, Lloyd / Du Val, Ronald W. / Gillman, Herbert, III et al. | NTRS | 1990