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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


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