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Issue DateTitleAuthor(s)Type
Apr-1998 Argus, a Highly Reusable SSTO Rocket-Based Combined Cycle Launch Vehicle with Maglifter Launch AssistBellini, Peter X.; Olds, John R.Paper
Jul-2004 Centurion: A Heavy-Lift Launch Vehicle Family for Cis-Lunar ExplorationYoung, James J.; Sakai, Tadashi; Reeves, John Daniel; Pimentel, Janssen; Krevor, Zachary C.; Hutchinson, Virgil L., Jr.; Olds, John R.; Young, David AnthonyPaper
Aug-2003 Chimera: A Low Cost Solution to Small Satellite Space AccessOlds, John R.; Piletsky, Pavel; Maatsch, John; Jackson, Jonathan; Curry, Mike; Young, David Anthony; Keisner, Alex; Hutchinson, Virgil L., Jr.; Crowley, JohnPaper
1995 Collaboration during Conceptual DesignPotts, Colin; Catledge, Lara D.Technical Report
Sep-2000 Comparison of Collaborative Optimization to Conventional Design Techniques for a Conceptual RLVOlds, John R.; Way, David Wesley; McCormick, David Jeremy; Ledsinger, Laura Anne; Scott, Andrew; Cormier, Timothy A.Paper
Oct-2002 A Conceptual Design for the Space Launch Capability of the Peacekeeper ICBMMavris, Dimitri N.; Villeneuve, Frédéric; Burg, Cecile M.; Barros, Peter. A., Jr.; Kumpel, Amy E.Paper
Oct-2002 Development of an Integrated Parametric Environment for Conceptual Hypersonic Missile SizingMavris, Dimitri N.; McClure, Erin Kathleen; Ender, Tommer RafaelPaper
Jul-2005 An Experimental and Analytical Study of High-Energy-Density propellants for Liquid Rocket EnginesOlds, John R.; Kokan, Timothy SalimPaper
Sep-2000 Exploration of the Design Space for the ABLV-GT SSTO Reusable Launch VehicleMessitt, Donald G.; Cormier, Timothy A.; Bechtel, Ryan S.; Olds, John R.; Bradford, John EdwardPaper
9-Apr-2007 A Generalized Sizing Method for Revolutionary Concepts under Probabilistic Design ConstraintsNam, Taewoo; Aerospace EngineeringDissertation
Nov-1999 Hyperion: An SSTO Vision Vehicle Concept Utilizing Rocket-Based Combined Cycle PropulsionSorensen, Kirk; McCormick, David Jeremy; Ledsinger, Laura Anne; Charania, Ashraf; Bradford, John Edward; Olds, John R.Paper
Jul-1998 Improvements and Enhancements to SCCREAM, A Conceptual RBCC Engine Analysis ToolOlds, John R.; Bradford, John EdwardPaper
Nov-1999 Integrating Aeroheating and TPS into Conceptual RLV DesignOlds, John R.; Cowart, Karl K.Paper
Sep-1997 Integration of Cost and Business Simulation into Conceptual Launch Vehicle DesignOlds, John R.; Lee, HosungPaper
28-Nov-2005 A Method for Aircraft Concept Exploration using Multicriteria Interactive Genetic AlgorithmsBuonanno, Michael Alexander; Aerospace EngineeringDissertation
Oct-2000 A Method for Concept Exploration of Hypersonic Vehicles in the Presence of Open and Evolving RequirementsMavris, Dimitri N.; Hollingsworth, Peter MichaelPaper
Oct-2000 Methodology for the Parametric Structural Conceptual Design of Hypersonic VehiclesMavris, Dimitri N.; De Baets, Peter Wilfried GastonPaper
Oct-2000 A Parametric Design Environment for Including Signatures Analysis in Conceptual DesignMavris, Dimitri N.; Hines, Nathan RobertPaper
31-Mar-2008 A Parametric Physics Based Creep Life Prediction Approach to Gas Turbine Blade Conceptual DesignSmith, Marcus Edward Brockbank; Aerospace EngineeringDissertation
Apr-2002 Potential Formulation for Aeroelastic Constraint Analysis in a Conceptual Design EnvironmentMavris, Dimitri N.; De Baets, Peter Wilfried GastonPaper
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