SPACE FRONTIER OPERATIONS, INC.
Who Dares, Wins!
AIAA Publications | ||
| Document Number | Title | Author |
|---|---|---|
| SFL 000092 | An Innovative Two Stage-to-Orbit Launch Vehicle Concept | Ramon L. Chase L. E. McKinney H. D. Froning, Jr. |
| SFL 000093 | Helicon wave produced plasmas for electric propulsion | Jim Gilland, |
| SFL 000094 | Design and Fabrication of a 500 kWe Lithium-fed Lorentz Force Accelerator | Jay Polk, Jet Propulsion Laboratory; John Blandino1, Robert Shotwell1, Keith Goodfellow1, Van Luong, Alok Majumdar, and Frank Zimmerman |
| SFL 000095 | POSITION COVARIANCE VISUALIZATION | J. Woodburn, S. Tanygin |
| SFL 000096 | Uncertainty quantification of simulation codes based on experimental data | Ken Hanson and François Hemez |
| AIAA 2000-3537 | Application of a New Numerical Solver to the Simulation of MPD Flows | K. Sankarany, E.Y. Choueiriz and S.C. Jardinx, |
| AIAA 2003-6276 | HUMAN-ROBOTIC HYBRIDS FOR DEEP-SPACE EVA: THE SPACE CONSTRUCTION AND ORBITAL UTILITY TRANSPORT CONCEPT | David L. Akin, Mary L. Bowden |
| AIAA 2001-25391 | EFFICIENT UNCERTAINTY ANALYSIS METHODS FOR MULTIDISCIPLINARY ROBUST DESIGN | Xiaoping Du and Wei Chen |
| AIAA 98-4254 | Flight-Simulated Launch-Pad-Abortto-Landing Maneuvers for a Lifting Body | E. Bruce Jackson, Robert A. Rivers |
| AIAA 89-3312 | DEVELOPMENT OF A TACTICAL GUIDANCE RESEARCH AND EVALUATION SYSTEM (TGRES) | Kenneth H. Goodrich, John W. McManus |
| AIAA 91-1496 | Study of Cluster Formation and its Effects on Rayleigh and Raman Scattering Measurements in a Mach 6 Wind Tunnel | B. Shirinzadeh, M. E. Hillard, A. B. Blair, and R. J. Exton |
| AIAA 91-3209 | Generic Hypersonic Inlet Module Analysis | Charles E. Cockrell, Jr., Lawrence D. Huebner |
| AIAA 92-1057 | ELEMENTS OF DESIGNING FOR COST | Edwin B. Dean, Resit Unal |
| AIAA 92-4720 | INFORMATION MANAGEMENT FOR A LARGE MULTIDISCIPLINARY PROJECT | Kennie H. Jones, Donald P. Randall, Catherine K. Cronin |
| AIAA 93-2793 | APPLICATION OF AN ENGINEERING INVISCID-BOUNDARY LAYER METHOD TO SLENDER THREE-DIMENSIONAL VEHICLE FOREBODIES | Christopher J. Riley |
| AIAA 93-3932 | Post-Optimality Analysis in Aerospace Vehicle Design | Robert D Braun, Ilan M Kroo, Peter J Gage |
| AIAA 93-3966 | Why Does It Cost How Much? | Edwin B. Dean |
| AIAA 94-0218 | PARALLEL DSMC SOLUTION OF THREE-DIMENSIONAL FLOW OVER A FINITE FLAT PLATE | Robert P. Nance, Richard G. Wilmoth, Bongki Moon, H. A. Hassan, Joel Saltz |
| AIAA 94-0826 | DIRECT SIMULATION OF EVOLUTION AND CONTROL OF NONLINEAR INSTABILITIES IN ATTACHMENT{LINE BOUNDARY LAYERS | Ronald D. Joslin |
| AIAA 94-1579 | Thermoelastic Formulation of Stiffened, Unsymmetric Composite Panels for Finite Element Analysis of High Speed Aircraft | Craig S. Collier, Lockheed Engineering and Sciences Company, NASA Langley Research Center, Hampton, Virginia |
| AIAA 94-4325 | Multidisciplinary Optimization Methods For Aircraft Preliminary Designs | Ilan Kroo, Steve Altus, Robert Braun, Peter Gage, and Ian Sobieski |
| AIAA 91-3619 | Defining Suppport Requirements During Conceptual Design of Reusable Launch Vehicles | W.D. Morris, N.H. White, W.T Davis Dr. C. E. Ebeling |
| AIAA 2000-3824 | Low Cost Options for 2nd and 3rd Generation Reusable Launch Vehicles | J. Andrews & Dr. D. Andrews |
| AIAA 2000-5164 | Feasibility of Commercial Space-Based Microchip Fabrication | Jeff Johnson Glen Chapman Nick Pfeiffer Joe Hopkins |
| AIAA 2001-3702 | Air Collection and Enrichment System (ACES) for Advanced 2nd. Generation RLVs | Dana G. Andrews & Jason E. Andrews |
| AIAA 2001-3964 | Designing for Future Space Transportation Missions | Dana G. Andrews & Jason E. Andrews |
| AIAA 2003-5439 | Online Trajectory Command Reshaping for Reusable Launch Vehicles | J.D. Schierman, J.R. Hull & D.G. Ward |
| AIAA 2000-5104 | RLV Design Issues for Future Commercial Space Applications | J. Andrews |
| AIAA 2000-4884 | Optimized Solutions for the Kistler K-1 Branching Trajectory Using MDO Techniques | L.A. Ledsinger, J.R. Olds |
| AIAA 2000-4884 | Optimized Solutions for the Kistler K-1 Branching Trajectory Using MDO Techniques | Presentation Charts |
| AIAA 2001-3514 | ASPEN Revisited: The Challenge of Nuclear Propulsion for ETO | J. Weglian, J. Olds, L. Marcus, J. McIntire, D. Nelson J. Blevins |
| AIAA 2001-3514 | ASPEN Revisited: The Challenge of Nuclear Propulsion for ETO | Presentation Charts |
| AIAA 2001-3516 | Starsaber: A Small Payload-Class TSTO Vehicle Utilizing Rocket-Based Combined Cycle Propulsion | B. St. Germain, J.R. Olds, J. McIntire, D. Nelson, J. Weglian L.Ledsinger |
| AIAA 2001-3516 | Starsaber: A Small Payload-Class TSTO Vehicle Utilizing Rocket-Based Combined Cycle Propulsion | Presentation Charts |
| AIAA 2001-3524 | Moon-based Advanced Reusable Transportation Architecture | D.K. Nelsom, L.R. Marcus, R. Bechtel, T.A. Cornier, J.E. Weglian, R. Alexander |
| AIAA 2001-4542 | A Comparison of Modern and Historic Mass Estimating Relationships on a Two Stage to Orbit Launch Vehicle | R.R. Rohrschneider, J.R. Olds |
| AIAA 2001-4542 | A Comparison of Modern and Historic Mass Estimating Relationships on a Two Stage to Orbit Launch Vehicle | Presentation Charts |
| AIAA 2001-4623 | Technology Assessment for Manned Mars Exploration Using a ROSETTA Model of a Bimodal Nuclear Thermal Rocket (BNTR) | L.R. Marcus, D.W. Way, M. Medlin, T. Sakai, J.R. McIntire, J.R. Olds |
| AIAA 2001-4623 | Technology Assessment for Manned Mars Exploration Using a ROSETTA Model of a Bimodal Nuclear Thermal Rocket (BNTR) | Presentation Charts |
| AIAA 2002-3905 | Mission Capture Rate versus Turnaround Time and Fleet Size for the Military Spaceplane | T. Kokan, J.R. Olds |
| AIAA 2002-3905 | Mission Capture Rate versus Turnaround Time and Fleet Size for the Military Spaceplane | Presentation Charts |
| AIAA 2002-5535 | A Desin of Experiments-Based Method for Point Selection in Approximating Output Distributions | D. J. McCormick J.R.Olds |
| AIAA 2002-5587 | A Distributed Framework for Probabilistic Analysis | D. J. McCormick J.R.Olds |
| AIAA 2003-0909 | Flight Mechanics of Manned Sub-Orbital Reusable Launch Vehicles with Recommendations for Launch and Recovery | Marti Sariguil-Klijn & Nesrin Sariguil-Klijn |
| AIAA 2003-5027 | Fundamentals of PPT Discharge Initiation: Undervoltage Breakdown Through Electron Pulse Injection | James E. Cooley, Edgar Y.Choueiri |
| AIAA 2004-3735 | Centurion: A Heavy Lift Launch Vehicle Family for Cis-Lunar Exploration | David A. Young, John R. Olds, Virgil Hutchison, Zachary Krevor, Janssen Pimentel, John D. Reeves, Tadashi Sakai & James Young |
| AIAA 92-4791 | The Suitability of Selected Multidisciplinary Design and Optimization Techniques to Conceptual Aerospace Vehicle Design | J.Olds |
| AIAA 93-1096 | Multidisciplinary Design of a Rocket-Based Combined Cycle SSTO Launch Vehicle using Taguchi Methods | J. Olds & G. Walberg |
| AIAA 94-4339 | System Sensitivity Analysis Applied to the Conceptual Design of a Dual-Fuel Rocket SSTO | J. Olds |
| AIAA 96-2688 | Options for Flight Testing Rocket-Based Combined-Cycle (RBCC) Engines | J. Olds |
| AIAA 96-4092 | Application of a New Economic Analysis Tool to a Two Stage to Orbit RBCC Launch Vehicle design | J. Olds, H Lee |
| AIAA 97-2760 | SCCREAM (Simulated Combined Cycle Rocket Engine Analysis Module):A Conceptual RBCC Engine Design Tool | J. Olds, J. Bradford |
| AIAA 97-3122 | Sirius: A New Launch Vehicle Optioin for Mega-LEO Constellation Deployment | D. Way, J. Olds |
| AIAA 97-3911 | Integration of Cost Modeling and Business Simulation into Conceptual Launch Vehicle Design | H. Lee, J. Olds |
| AIAA 97-3953 | Component Level Weight Analysis for RBCC Engines | J.R. Olds, D.J. McCormick |
| AIAA 98-0302 | Constant Dynamic Pressure Trajectory Simulation with POST | J.R. Olds, I.A. Budianto |
| AIAA 98-1557 | Argus, A Highly Reusable SSTO Rocket-Based Combined Cycle Launch Vehicle with Maglifter Assist | J.R.Olds, P.X. Bellini |
| AIAA 98-3227 | SCORES: Developing an Object-Oriented Rocket Propulsion Analysis Tool | D.W. Way, J.R. Olds |
| AIAA 98-3775 | Improvements and Enhancements to SCCREAM, A Conceptual RBCC Engine AnalysisTool | J.E. Bradford, J.R. Olds |
| AIAA 98-4713 | Multidisciplinary Design Optimization Techniques for Branching Trajectories | L.A. Ledsinger, J.R. Olds |
| AIAA 98-4743 | Cross-Platform Computational Techniques for Analysis Code Integration and Optimization | J.R. Olds, K.B. Steadman |
| AIAA 98-4743 | Cross-Platform Computational Techniques for Analysis Code Integration and Optimization | Presentation Charts |
| AIAA 98-4942 | Computational Frameworks for Collaborative Multidisciplinary Design of Complex Systems | D.E. Acton, J.R. Olds |
| AIAA 98-4942 | Computational Frameworks for Collaborative Multidisciplinary Design of Complex Systems | Presentation Charts |
| AIAA 98-5179 | Economic Uncertainty of Weight and Market Parameters for Advanced Space Launch Vehicles | J.A. Whitfield, J.R. Olds |
| AIAA 98-5179 | Economic Uncertainty of Weight and Market Parameters for Advanced Space Launch Vehicles | Presentation Charts |
| AIAA 98-5208 | Transforming Aerodynamic Datasets into Parametric Equations for use in Multidisciplinary Design Optimization | J.M. Scott, J.R. Olds |
| AIAA 98-5209 | System Robustness Comparison of Advanced Space Launch Concepts | D.J. McCormick, J.R. Olds |
| AIAA 98-5209 | System Robustness Comparison of Advanced Space Launch Concepts | Presentation Charts |
| AIAA 98 ASM | Multidisciplinary Optimization Techniques for Branching Trajectories | J.R. Olds, L.A. Ledsinger |
| AIAA 99-0110 | Demonstration of CLIPS as an Intelligent Front-End for POST | I.A. Budianto, J.R. Olds, N.C. Baker |
| AIAA 99-0110 | Demonstration of CLIPS as an Intelligent Front-End for POST | Presentation Charts |
| AIAA 99-2104 | SCCREAM v5: A Web-Based Airbreathing Propulsion Analysis Tool | J. Bradford, J.R. Olds |
| AIAA 99-2104 | SCCREAM v5: A Web-Based Airbreathing Propulsion Analysis Tool | Presentation Charts |
| AIAA 99-2353 | SCORES: Web-Based Rocket Propulsion Analysis for Space Transportation System Design | D. Way, J. Olds |
| AIAA 99-2353 | SCORES: Web-Based Rocket Propulsion Analysis for Space Transportation System Design | Presentation Charts |
| AIAA 99-2354 | An Evaluation of Two Alternate Propulsion Concepts for Bantam-Argus: Deeply-Cooled Turbojet + Rocket and Pulsed detonation Rocket + Ramjet | B. St.Germain, J. Olds |
| AIAA 99-2354 | An Evaluation of Two Alternate Propulsion Concepts for Bantam-Argus: Deeply-Cooled Turbojet + Rocket and Pulsed detonation Rocket + Ramjet | Presentation Charts |
| AIAA 99-4806 | Integrating Aeroheating and TPS into Conceptual RLV design | K. Cowart, J. Olds |
| AIAA 99-4806 | Integrating Aeroheating and TPS into Conceptual RLV design | Presentation Charts |
| AIAA 99-4888 | Stargazer: A TSTO Bantam-X Vehicle Concept Utilizing Rocket-Based Conbined Cycle Propulsion. | J.Olds, L. Ledsinger, J. Bradford, A. Charania, D. McCormick D.R. Komar |
| AIAA 99-4888 | Stargazer: A TSTO Bantam-X Vehicle Concept Utilizing Rocket-Based Conbined Cycle Propulsion. | Presentation Charrts |
| AIAA 99-4944 | Hyperion: An SSTO Vision Concept Utilizing Rocket-Based Combined Cycle Propulsion | J. Olds, J. Bradford, A. Charania, L.Ledsinger, D. McCormick, K. Sorensen |
| AIAA 99-4944 | Hyperion: An SSTO Vision Concept Utilizing Rocket-Based Combined Cycle Propulsion | Presentation Charts |
| AIAA 03VGR | Uncertainty Quantification of Simulation Codes based on Experimental data | Ken Hansen Francois Hemez |
| AIAA 2000-3537 | Application of a New Numerical Solver to the Simulation of MPD Flows | K.Sankaran, E.Y. Choueiri, S.C. Jardin |
| AIAA 2000-4863 | Approximation of Probabilistic Distributions Using Selected Discrete Simulations | D.J. McCormick, J.R. Olds |
| AIAA 2000-4863 | Approximation of Probabilistic Distributions Using Selected Discrete Simulations | Presentation Charts |
| AIAA 2000-4885 | Comparison of Collaborative Optimization to Conventional Design Techn iques fro a Conceptual RLV | T. Cormier, A. Scott, L. Ledsinger, D. McCormick, D. Way, J. Olds |
| AIAA 2000-5136 | Exploration of the Design Space for the ABLV-GT SSTO Reusable Launch Vehicle | J. Bradford, J. Olds, R. Bechtel, T. Cormier D. Messitt |
| AIAA 2000-5136 | Exploration of the Design Space for the ABLV-GT SSTO Reusable Launch Vehicle | Presentation Charts |
| AIAA 2000-5265 | TCAT - A Tool for Automated Thermal Protection System Design | K. Cowart, J. Olds |
| AIAA 2000-5265 | TCAT - A Tool for Automated Thermal Protection System Design | Presentation Charts |
| AIAA 2001-4625 | An Introduction to the ROSETTA Modeling Process for Advanced Space Transportation Technology Investment | Andrew M. Crocker, A.C. Charania, Dr. John R. Olds |
| AIAA 2002-3605 | Rapid Prediction of Aftbody Nozzle Performance in SCCREAM | J. Bradford |
| AIAA 2002-3990 | SCORES II Design Tool for Liquid Rocket Engine Analysis | J. Bradford |
| AIAA 2003-5269 | A Study of ARTS: A Dual Fuel Reusable Launch Vehicle with Launch Assist | John Wallace, John Olds, A.C. Charania Gordon Woodcock |
| AIAA 2003-5269 | A Study of ARTS: A Dual Fuel Reusable Launch Vehicle with Launch Assist | Presentation Charts |
| AIAA 2004-3742 | Reusable Rocket Propulsion for Space Tourism Vehicles | Douglas Jones |
| AIAA 2006-4605 | Thermal Protection System Siziong and Selection for RLV's Using the Sentry Code | Bradford, J.E.; Olds, J.R. |
| AIAA 2006-4605 | Thermal Protection System Siziong and Selection for RLV's Using the Sentry Code | Presentation Charts |
| AIAA 2006-8018 | Mission Effectiveness Tradeoffs for Future Military Space Access Vehicles | A. Charania, J. bradford |
| AIAA 2006-8018 | Mission Effectiveness Tradeoffs for Future Military Space Access Vehicles | Presentation Charts |
| AIAA 2006-8056 | The Hypersonic ETO Space Transporter as an Enabling Element for Acquiring Commercial Human-rated Space Transportation Capabilities | William J.D. Escher |
| AIAA 2006-8056 | The Hypersonic ETO Space Transporter as an Enabling Element for Acquiring Commercial Human-rated Space Transportation Capabilities | Presentation Charts |
| AIAA 2006-8057 | Concept Study of an ARES Hybrid-OS Launch System | John G. Wallace, John Bradford, A.C. Charania, William J. D. Escher Dean Eklund |
| AIAA 2006-8057 | Concept Study of an ARES Hybrid-OS Launch System | Presentation Charts |
| AIAA 89-3312 | Development of a Tactical Guidance Research and Evaluation System ( TGRES) | Kenneth H. Goodrich, John W. mcManus |
| AIAA 92-1057 | Elements of Designing for Cost | Edwin B. Dean Resit Unal |
| AIAA 93-2793 | Application of an Engineering Inviscid-Boundary Layer Method to Slender Three-Dimensional Vehicle Forebodies | Christopher J. Riley |
| AIAA 94-4372 | A Distributed Computing Environment for Multidisciplinary Design | R.P. Weston, J. P. Townsend T.M. Eidson R.L. Gates |
| AIAA 95-0737 | Experimental Results on the Feasibility of an Aerospaike for Hypersonic Missiles | |
| AIAA 98-4254 | Flight Simulated Launch-Pad-Abort-to-Landing Maneuvers for a Lifting Body | E. Bruce Jackson, Robert A. Rivers |
| AIAA 99-2423 | Plume Study of a 1.35KW SPT-100 Using and EXB probe | Sang-Wook Kim, Alec D. Gallimore |
| AIAA-IEEE | Design for Validation | Sally C. Johnson, Ricky W. Butler |
| AIAA JSR SEP OCT 92 | A High Angle of Attack Inviscid Shuttle Orbiter Computation | William L. Kleb, K. James Wilmuenster |
| SSC99-X-7 | The Sprite Mini-Lift Vehicle:Performance, Cost and Schedule Projections for the First of the SCORPIUSTM Low-Cost Launch Vehicles | James V. Berry, Robert E. Conger, James R. Wertz |
Space Frontier Operations, Inc. in a "Not for Profit" Florida corporation.
All material is copyright Space Frontier Operations, Inc.
We welcome your comments
webmaster@sfo.org
All Material is either Copyright 2010 Space Frontier Operations, Inc. or Copyright the original publisher
Counter reset on 2010-10-05
Last edited on