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NASA/AIAA Documents | ||
| Document Number | Title | Author |
|---|---|---|
| NASA-2000-1iwsrr-jww.pdf | Optimized Shielding for Space Radiation Protection | J. W. Wilson, F. A. Cucinotta, M.-H. Y. Kim¤, and W. Schimmerling |
| NASA-2000-nsmms-wdb.pdf | Alloys and Coating Development for Metallic | William D. Brewer, Keith Bird, Terryl Wallace, S.A. Sankaran |
| NASA-2001-33sampe-bwg.pdf | HYBRID COMPOSITES FOR LH2 FUEL TANK STRUCTURE | Brian W. Grimsley, Roberto J. Cano, and Norman J. Johnston, Alfred C. Loos, William M. McMahon |
| NASA/AIAA-85-0974 | Heating Rate Distributions at Mach 10 on a Circular Body Eath-to-Orbit Transport Vehicle | W L Wells, I O MacConochie, V T Helms III, and D Raney |
| NASA/AIAA-93-3536 | Three Dimensional Aerodynamic Analysis of a High-Lift Transport Configuration | Simha S Dodbele |
| NASA/AIAA-94-0061 | Recent Progress Toward a Three-Dimensional Unstructured Navier-Stokes Flow Solver | N T Frink |
| NASA/AIAA-94-0163 | On the Vortical-Flow Prediction Capability of an Unstructured-Grid Euler Solver | F Ghaffari |
| NASA/AIAA-94-1324 | FINITE ELEMENT ANALYSIS OF THE RANDOM RESPONSE SUPPRESSION OF COMPOSITE PANELS AT ELEVATED TEMPERATURES USING SHAPE MEMORY ALLOY FIBERS | Travis L. Turnery, Z W Zhongz, Chuh Mei |
| NASA/AIAA-94-4326 | ORDERING DESIGN TASKS BASED ON COUPLING STRENGTHS | J L Rogers, C L Bloebaum |
| NASA/AIAA-95-1317 | Effects of Stiffening and Mechanical Load on Thermal Buckling of Stiffened Cylindrical Shells | T F Johson, M F Card |
| NASA/AIAA-95-1850 | Hypersonic Aerodynamic Characteristics of a Proposed-Single-Stage-to-orbit Vehicle | K J Weilmuenster, P A Gnoffo, F A Greene, C J Riley, H H HAmilton II, S J Alter |
| NASA/AIAA-95-2016 | IN-FLIGHT THERMAL PERFORMANCE OF THE LIDAR IN-SPACE TECHNOLOGY EXPERIMENT | William A. Roettker |
| NASA/AIAA-95-2524 | CALCULATED EFFECTS OF NITRIC OXIDE FLOW CONTAMINATION ON SCRAMJET PERFORMANCE | K E Fischer and K E Rock |
| NASA/AIAA-95-3619 | Defining Support Requirements During Conceptual Design of Reusable Launch Vehicles | W D Morris, N H White, W T Davis, C E Ebeling |
| NASA/AIAA-96-0316 | Aerothermodynamic Analsis of Commercial Experiment Transporter (COMET) Reentry Capsule | W A Wood, P A Gnoffo, D F G Rault |
| NASA/AIAA-96-0711 | MULTIDISCIPLINARY AEROSPACE DESIGN OPTIMIZATION: SURVEY OF RECENT DEVELOPMENTS | J Sobieszczanski-Sobieski, R T Haftka |
| NASA/AIAA-96-0825 | Aerodynamic Characteristics of an Aerospace Vehicle During a Subsonic Pitch-Over Maneuver | W L Kleb |
| NASA/AIAA-96-0903 | Six Degree-of-Freedom Entry Dispersion Analysis for the METEOR Recovery Module | P N Desai, R D Braun, R W Powell, W C Engelund, P V Tartabini |
| NASA/AIAA-96-1800 | Analytic Corrections to CFD Heating Predictions Accounting for Changes in Surface Catalysis | P A Gnoffo, G R Ingery |
| NASA/AIAA-96-1812 | DSMC GRID METHODOLOGIES FOR COMPUTING LOW-DENSITY, HYPERSONIC FLOWS ABOUT REUSABLE LAUNCH VEHICLES | R G Wilmoth, A B Carlson, G J LeBeau, A B Carlson |
| NASA/AIAA-96-2416 | Geometric Model for a Parametric Study of the Blended-Wing-Body Airplane | C W Mastiny, R E Smithz, I Sadrehaghighix, M R Wiese |
| NASA/AIAA-96-2467 | Orbiter Aerodynamic Acceleration Flight Measurements in the Rarefied-Flow Transition Regime | R C Blanchard, R G Wilmouth, G J LeBeau |
| NASA/AIAA-96-2754 | FUNCTIONAL PERFORMANCE OF PYROVALVES | Laurence J. Bement |
| NASA/AIAA-96-3860 | A New Approach to Aircraft Robust Performance Analysis | I M Gregory, J E Tierno |
| NASA/AIAA-96-3991 | USE OF CAD GEOMETRY IN MDO | J A Samareh |
| NASA/AIAA-96-4018 | Use of the Collaborative Optimization Architecture for Launch Vehicle Design | R D Braun, A A Moore, I M Kroo |
| NASA/AIAA-96-4028 | MDO TEST SUITE AT NASA LANGLEY RESEARCH CENTER | S L Padula, N Alexandrov, L L Green |
| NASA/AIAA-96-4181 | Optimization of Operations Resources via Discrete Event Simulation Modeling | B. Joshi, D. Morris, N White, R Unal |
| NASA/AIAA-96-4245 | Analysis of Shuttle Orbiter Reliability and Maintainability Data for Conceptual Studies | W D Morris, N H White, C E Ebeling |
| NASA/AIAA-96-4589 | Analytic Corrections to CFD Heating Predictions Accounting for Changes in Surface Catalysis, Part II | P A Gnoffo, G R Ingery |
| NASA/AIAA-96-4591 | NASA's dual-Fuel Airreathing Hypersonic Vehicle Study | J L Hunt, E A Eiswirth |
| NASA/AIAA-97-0231 | Satellite Systems Design/Simulation Environment: A Systems Approach to Pre-Phase A Design | M J Ferebee Jr, P A Troutman, D W Monell |
| NASA/AIAA-97-0567 | Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical results | C Campbell, J Caram, S Berry, M DiFulvio, T Horvath |
| NASA/AIAA-97-2475 | Overview of X-38 Hypersonic Wind Tunnel Data and Comparison with Numerical results | C Campbell, J Caram, S Berry, M DiFulvio, T Horvath |
| NASA/AIAA-97-2698 | DETERMINING FUNCTIONAL RELIABILITY OF PYROTECHNIC MECHANICAL DEVICES | L J Bement, H A Multhaup |
| NASA/AIAA-97-3374 | Multidisciplinary Approach To Linear Aerospike Nozzle Optimization | J J Korte, A O Salas, H J Dunn, N M Alexandrov, W W Follet, G E Orient, A H Hadid |
| NASA/AIAA-98-0298 | Mars Pathfinder rarefied aerodynamics: Computations and Measurements | J N Moss, R C Blanchard, R G Wilmoth, R D Braun |
| NASA/AIAA-98-0328 | BOUNDARY LAYER FLOW CONTROL WITH A ONE ATMOSPHERE UNIFORM GLOW DISCHARGE SURFACE PLASMA | J R Roth, D M Sherman, Stephen P. Wilkinson |
| NASA/AIAA-98-0682 | Experimental Verification Of The Osculating Cones Method For Tw Waverider Forebodies At Mach 4 and 6 | R W Miller, B M Arrow, K B Center, G J Brauckmann, M N Rhode |
| NASA/AIAA-98-0867 | Hypersonic boundery-Layer Transitionn for X-33 Phase II Vehicle | R A Thompson, H H Hamilton II, S A Berry, T J Horvath, R J Nowak |
| NASA/AIAA-98-0869 | Computational/Experimental Aeroheating Predictions for X-33 Phase II Vehicle | H H Hamilton II, K J Weilmuenster, T J Horvath, S A Berry |
| NASA/AIAA-98-0880 | Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method | C J Riley, W L Kleb, S J Alter |
| NASA/AIAA-98-0881 | X-34 EXPERIMENTAL AEROHEATING AT MACH 6 AND 10 | S A Berry, T J Horvath, M DiFulvio, C Glass, N R Merski |
| NASA/AIAA-98-1532 | Hyper-X Engine Design and Ground Test Program | R T Voland, K E Rock, L D Huebner, D W Witte, K E Fischer, C R McClinton |
| NASA/AIAA-98-1708 | RESPONSE OF COMPOSITE FUSELAGE SANDWICH SIDE PANELS SUBJECTED TO INTERNAL PRESSURE AND AXIAL TENSION | M Rouse, D R Ambur, B Dopker, B Shah |
| NASA/AIAA-98-1749 | DESIGN-ORIENTED ANALYSIS OF AIRCRAFT FUSELAGE STRUCTURES | G L Giles |
| NASA/AIAA-98-1838 | NONLINEAR ANALYSIS OF THE SPACE SHUTTLE SUPERLIGHTWEIGHT LO2 TANK: PART I - BEHAVIOR UNDER BOOSTER ASCENT LOADS | R D Young, M P Nemeth†, T J Collins, J H Starnes Jr |
| NASA/AIAA-98-1839 | NONLINEAR ANALYSIS OF THE SPACE SHUTTLE SUPERLIGHTWEIGHT LO2 TANK: PART I - BEHAVIOR UNDER 3g END-OF-FLIGHT LOADS | R D Young, M P Nemeth†, T J Collins, J H Starnes Jr |
| NASA/AIAA-98-1840 | Effects of welding-Induced initial Geometric Imperfections o the onlinear Behaviorof the Space shuttle Superlightweight LO2 Tank | M P Neemth, R D Young, T J Collins, J H Starnes Jr |
| NASA/AIAA-98-1865 | OPTIMAL SENSOR/ACTUATOR LOCATIONS FOR ACTIVE STRUCTURAL ACOUSTIC CONTROL | S L Padula, D L Palumbo, R K Kincaid |
| NASA/AIAA-98-2445 | Prediction and Validation of Mars Pathfinder Hypersonic Aerodynamic Data Base | P A Gnoffo, R D Braun, K J Weilmuenster, R A Mitcheltree, W C Engelund, R W Powell |
| NASA/AIAA-98-2531 | X-34 Vehicle Aerodynamic Characteristics | G J Brauckmann |
| NASA/AIAA-98-2600 | Aerothermodynamic Flight simulation Capabilities for Aerospace Vehicles | C G Miller |
| NASA/AIAA-98-2850 | Mars Ascent Vehicle Flight Analysis | P N Desai, R D Braun, W C Engelund, F M Cheatwood, J A Kangas |
| NASA/AIAA-98-3783 | A METHOD FOR SIZING BOOSTER CHARGES IN PYROTECHNIC MECHANISMS | L J Bement |
| NASA/AIAA-98-4135 | PARAMETERIZATION OF MODEL VALIDATING SETS FOR UNCERTAINTY BOUND OPTIMIZATIONS | K B Lim, D P Giesy |
| NASA/AIAA-98-4254 | Flight-Simulated Launch-Pad-Abort-to-Landing Maneuvers for a Lifting Body | E B Jackson, R A Rivers |
| NASA/AIAA-98-4574 | Numerical Roll Reversal Predictor-Corrector Aerocapture and Precision Landing Guidance Algorithms for the Mars Surveyor Program 2001 Missions | R W Powell |
| NASA/AIAA-98-4706 | A WEB-BASED MONITORING SYSTEM FOR MULTIDISCIPLINARY DESIGN PROJECTS | J L Rogers, A O Salas, R P Weston |
| NASA/AIAA-98-4740 | FRAMEWORK REQUIREMENTS FOR MDO APPLICATION DEVELOPMENT | A O Salas, J C Townsend |
| NASA/AIAA-98-4758 | A COMPARISON OF APPROXIMATION MODELING TECHNIQUES: POLYNOMIAL VERSUS INTERPOLATING MODELS | A A Giunta, L T Watson |
| NASA/AIAA-98-4759 | RESPONSE SURFACE MODEL BUILDING AND MULTIDISCIPLINARY OPTIMIZATION USING D-OPTIMAL DESIGNS | R Unal, R A Lepsch, M L McMillin |
| NASA/AIAA-98-4791 | Bell-Curve Based Evolutionary Optimization Algorithm | J Sobieszczanski-Sobieski, K Laba, R Kincaid |
| NASA/AIAA-99-0835 | Nontangent, Developed Contour Bulkheads for a Wing-Body Single Stage Launch Vehicle | K C Wu, R A Lepsch Jr |
| NASA/AIAA-99-1044 | Analysis and Testing of High Temperature Fibrous Insulation for Reusable Launch Vehicles | K Daryabeigi |
| NASA/AIAA-99-3459 | Parametric Weight Comparison of Current and Proposed Thermal Protection System (TPS) Concepts | D E Myers, C J Martin, M L Blosser |
| NASA/AIAA-99-3558 | X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography | T J Horvath, S A Berry, B R Hollis, D S Liechty, H H Hamilton II, N R Merski |
| NASA/AIAA-99-3559 | X-33 Computational Aeroheating Predictions and Comparisons | B R Hollis, T J Horvath, S A Berry, H H Hamilton II, S J Alter |
| NASA/AIAA-99-3959 | UNCERTAINTY MODELING VIA FREQUENCY DOMAIN MODEL VALIDATION | M R Waszak, D Andrisani II |
| NASA/AIAA-99-4124 | Flight control Laws for NASA's HyperX Research Vehicle | J Davidson, F Lallman, J D McMinn, J Martin, J Pahle, M Stephenson, J Selmon |
| NASA/AIAA-99-4162 | X-33 Hypersonic Aerodynamic Characteristics | K J Murphy, R J Nowak, R A Thopson, B R Hollis, R K Prabhu |
| NASA/AIAA-99-4163 | X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel | K J Murphy, R J Nowak, C J Riley, W A Wood, S J Alter, R K Prabhu |
| NASA/AIAA-99-4818 | Hyper-X Stage Separation—Background and Status | D E Reubush |
| NASA/AIAA-99-4836 | Numerical andAnalytical Solutions of Hypersonic Interactions ivlving Surface Property Discontinuities | P A Gnoffo, G R Inger |
| NASA/AIAA-99-4948 | An Airbreathing Launch Vehicle Design with Turbine-Based Low-Speed Propulsion and Dual Mode Scramjet High-Speed Propulsion | P L Moses, K A Bouchard, R F Vause, S Z Pinckney, S M Ferlemann, C P Leonard, L W Taylor lll, J S Robinson, J G Martin, D H Petley, J L Hunt |
| NASA/AIAA-99-4978 | Airbreathing Hypersonic Technology Vision Vehicles and Development Dreams | C R McClinton, J L Hunt, R H Ricketts, P Reukauf, C L Peddie |
| NASA/AIAA-2000-0409 | Dynamics of Active Seperation Control at High Reynolds Numbers | L G Pack, A Seifert |
| NASA/AIAA-2000-0418 | MULTIDISCIPLINARY HIGH-FIDELITY ANALYSIS AND OPTIMIZATION OF AEROSPACE VEHICLES, PART 1: FORMULATION | J L Walsh, J C Townsend, A O Salas, J A Samareh, V Mukhopadhyay, J F Barthelemy |
| NASA/AIAA-2000-0419 | Multidisciplinary High-Fidelity Analysis and Optimization of Aerospace Vehicles, Part 2: Preliminary Results | J L Walsh, R P Weston, J A Samareh, B H Mason, L L Green, R T Biedron |
| NASA/AIAA-2000-0826 | Rapid Model Fabrication and Testing for Aerospace Vehicles | G M Buck |
| NASA/AIAA-2000-0900 | Aerodynamic Characteristics, Database Development and Flight Simulation of the X-34 Vehicle | B N Pamadi, G J Brauckmann, M J Ruth, H D Fuhrmann |
| NASA/AIAA-2000-1042 | Overview of Conceptual Design of Early VentureStarTM Configurations | M K Lockwood |
| NASA/AIAA-2000-1043 | Reusable Launch Vehicle Tank/Intertank Sizing Trade Study | J T Dorsey, D E Myers, C J Martin |
| NASA/AIAA-2000-1044 | PARAMETRIC MODEL OF AN AEROSPIKE ROCKET ENGINE | J J Korte |
| NASA/AIAA-2000-1045 | A Multidisciplinary Performance Analysis of a Lifting-Body Single-Stage-to-Orbit Vehicle | P V Tartabini, R A Lepsch, J J Korte, K E Wurster |
| NASA/AIAA-2000-1046 | An Entry Flight Controls Analysis for a Reusable Launch Vehicle | P Calhoun |
| NASA/AIAA-2000-1342 | BMI SANDWICH WING BOX ANALYSIS AND TEST | T Palm, M Mahler, C Shah, M Rouse, H Bush, C Wu, W S Small |
| NASA/AIAA-2000-1560 | Flight Control using Distributed Shape-Change Effector Arrays | D L Raney, R C Montgomery, L L Green, M A Park |
| NASA/AIAA-2000-2685 | X-38 Experimental Aerothermodynamics | T J Horvath, S A Berry, N R Merski, S M Fitzgerald |
| NASA/AIAA-2000-3605 | HYPER-X ENGINE TESTING IN THE NASA LANGLEY 8-FOOT HIGH TEMPERATURE TUNNEL | L D Huebner, K E Rock, D W Witte,E G Ruf, E H Andrews Jr |
| NASA/AIAA-2000-3704 | THREE-DIMENSIONAL EFFECTS IN MODELING OF DUAL-MODE SCRAMJETS | C G Rodriguez, J A White, D W Riggins |
| NASA/AIAA-2000-4006 | Aerodynamic Database Development for the Hyper-X Airframe Integrated Scramjet Propulsion Experiments | W C Engelund,, S D Holland, C E Cockrell Jr, R D Bittner |
| NASA/AIAA-2000-4009 | Prediction of Hyper-X Stage Separation Aerodynamics Using CFD | P G Buning, T-C Wong, A D Dilley, J L Pao |
| NASA/AIAA-2000-4010 | Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment | C E Cockrell Jr, W C Engelund, R D Bittner, A D Dilley, T N Jentink, A Frendi |
| NASA/AIAA-2000-4149 | ROBUSTNESS OF FLEXIBLE SYSTEMS WITH COMPONENT-LEVEL UNCERTAINTIES | P G Maghami |
| NASA/AIAA-2000-4321 | Steady–State Computation of Constant Rotational Rate Dynamic Stability Derivatives | M A Park, L L Green |
| NASA/AIAA-2000-4704 | A UNIFIED APPROACH TO MODELING MULTIDISCIPLINARY INTERACTIONS | J A Samareh, K G Bhatia |
| NASA/AIAA-2000-4718 | Analytical and Computational Properties of Distributed Approaches to MDO | N M Alexandrov, R M Lewis |
| NASA/AIAA-2000-4719 | Algorithmic Perspectives on Problem Formulations in MDO | N M Alexandrov, R M Lewis |
| NASA/AIAA-2000-4839 | AFFORDABLE DESIGN: A METHODOLOGY TO IMPLEMENT PROCESS-BASED MANUFACTURING COST MODELS INTO THE TRADITIONAL PERFORMANCE-FOCUSED MULTIDISCIPLINARY DESIGN OPTIMIZATION | H P Bao, J A Samareh |
| NASA/AIAA-2001-0134 | FEDERAL R&D REDUCTIONS, MARKET SHARE, AND AEROSPACE INFORMATION USAGE | J Rocker, G Roncaglia |
| NASA/AIAA-2001-0162 | Estimating Bias Error Distributions | T Liu, T D Finley |
| NASA/AIAA-2001-0170 | A Single-Vector Force Calibration Method Featuring the Modern Design of Experiments | P A Parker, M Morton, N Draper, W Line |
| NASA/AIAA-2001-0757 | Cryogenic Model Materials | W M Kimmel, N S Kuhn, R F Berry, J A Newman |
| NASA/AIAA-2001-0911 | Reynolds Number Effects on a Supersonic Transport at Subsonic High-Lift Conditions | L R Owens, R A Wahls |
| NASA/AIAA-2001-0912 | Reynolds Number Effects on a Supersonic Transport at Transonic Conditions | R A Wahls, L R Owens, S M B Rivers |
| NASA/AIAA-2001-1334 | STRUCTURAL RESPONSE AND FAILURE OF A FULL-SCALE STITCHED GRAPHITE-EPOXY WING | D C Jegley, H G Bush, A E Lovejoy |
| NASA/AIAA-2001-1431 | COUPLED AERODYNAMIC AND STRUCTUAL SENSITIVITY ANALYSIS OF A HIGH-SPEED CIVIL TRANSPORT | B H Mason, J L Walsh† |
| NASA/AIAA-2001-1599 | CRYOGENIC TANK STRUCTURE SIZING WITH STRUCTURAL OPTIMIZATION METHOD | J T Wang, T F Johnson, D W Sleight, E Saether |
| NASA/AIAA-2001-1666 | AN ADVANCED BUFFET LOAD ALLEVIATION SYSTEM | J K Burnham, D M Pitt, E V White, D A Henderson, R W Moses |
| NASA/AIAA-2001-1802 | Hyper-X Stage Separation—Simulation Development and Results | D E Reubush, J G Martin, J S Robinson, D M Bose, B K Strovers |
| NASA/AIAA-2001-1809 | Hyper-X Flight Engine Ground Testing for X-43 Flight Risk Reduction | L D Huebner, K E Rock, E G Ruf, D W Witte, E H Andrews Jr |
| NASA/AIAA-2001-1814 | Hyper-X Mach 10 Engine Flowpath Development: Fifth Entry Test Conditions and Methodology | R J Bakos, C-Y Tsai, R C Rogers, A T Shih |
| NASA/AIAA-2001-2528 | APPROACH FOR UNCERTAINTY PROPAGATION AND ROBUST DESIGN IN CFD USING SENSITIVITY DERIVATIVES | M M Putko, P A Newman, L L Green |
| NASA/AIAA-2001-2529 | SOME ADVANCED CONCEPTS IN DISCRETE AERODYNAMIC SENSITIVITY ANALYSIS | A C Taylor III, L L Green, P A Newman, M M Putko |
| NASA-AIAA-2001-2574 | Toward Optimal Multigrid Efficience for the Navier-Sokes Equations | R C Swanson |
| NASA/AIAA-2001-2828 | X-38 Experimental Aeroheating At Mach 10 | S A Berry, T J Horvath, K J Weilmuenster, S J Alter, N R Merski |
| NASA/AIAA-2001-2834 | Thermal Analysis and Design of Multi-layer Insulation for Re-entry Aerodynamic Heating | K Daryabeigi |
| NASA/AIAA-2001-2962 | Aerothermodynamic Characteristics in the Hypersonic Continuum-Rarefied Transitional Regime | C E Glass, J N Moss |
| NASA/AIAA-2001-3241 | SCRAMJET TESTS IN A SHOCK TUNNEL AT FLIGHT MACH 7, 10, AND 15 CONDITIONS | R C Rogers, A T Shih, C-Y Tsai, R O Foelsche |
| NASA/AIAA-2001-4119 | EXAMINING REUSE IN LASRS++-BASED PROJECTS | M M Madden |
| NASA/AIAA-2001-4273 | INTEGRATED ORBIT, ATTITUDE, AND STRUCTURAL CONTROL SYSTEM DESIGN FOR SPACE SOLAR POWER SATELLITES | B Wie, C Roithmayr |
| NASA/AIAA-2002-0282 | Using the Web for Competetive Intelligence (CI) Gathering | J Rocker, G Roncaglia |
| NASA/AIAA-2002-0502 | Metallic Thermal Protection System Technology Development: Concepts, Requirements And Assessment Overview | J T Dorsey, C C Poteet, R R Chen, K E Wurster |
| NASA/AIAA-2002-0503 | INVESTIGATION OF FUNDAMENTAL MODELING AND THERMAL PERFORMANCE ISSUES FOR A METALLIC THERMAL PROTECTION SYSTEM DESIGN | M L Blosser |
| NASA/AIAA-2002-0504 | ADVANCED METALLIC THERMAL PROTECTION SYSTEM DEVELOPMENT | M L Blosser, R R Chen, I H Schmidt, J T Dorsey, C C Poteet, R K Bird |
| NASA/AIAA-2002-0505 | Preliminary Thermal-Mechanical Sizing of Metallic TPS: Process Development and Sensitivity Studies | C C Poteet, H Abu-Khajeel, S-Y Hsu |
| NASA/AIAA-2002-0910 | Probabilistic Design Of A Mars Sample Return Earth Entry Vehicle Thermal Protection System | J A Dec,R A Mitcheltree |
| NASA/AIAA-2002-1525 | BUCKLING DESIGN STUDIES OF INVERTED, OBLATE BULKHEADS FOR A PROPELLANT TANK | S S Smeltzer III, L M Bowman |
| NASA/AIAA-2002-2744 | Discrete Roughness Effects on Shuttle Orbiter at Mach 6 | S A Berry, H H Hamilton II |
| NASA/AIAA-2002-3140 | PROBABILISTIC METHODS FOR UNCERTAINTY PROPAGATION APPLIED TO AIRCRAFT DESIGN | L L Green, H-Z Lin, M R Khalessi |
| NASA/AIAA-2002-3878 | Fuel-Air Mixing and Combustion in Scramjets | J P Drummond, G S Diskin, A D Cutler |
| NASA/AIAA-2002-4411 | Aerodynamic Database Development for Mars Smart Lander Vehicle Configurations | G J Bobskill, P C Parikh, R K Prabhu, E D Tyler |
| NASA/AIAA-2002-4482 | Flight Dynamic Model Exchange using XML | E B Jackson, B L Hildreth |
| NASA/AIAA-2002-4504 | ENTRY VEHICLE CONTROL SYSTEM DESIGN FOR THE MARS SMART LANDER | P C Calhoun, E M Queen |
| NASA/AiAA-2002-5020 | OPTIMAL CONTROL DESIGN USING AN H2 METHOD FOR THE GLOVEBOX INTEGRATED MICROGRAVITY ISOLATION TECHNOLOGY (G-LIMIT) | P C Calhoun, R D Hampton |
| NASA/AIAA-2002-5188 | Technology Roadmap for Dual-Mode Scramjet Propulsion to Support Space-Access Vision Vehicle Development | C E Cockrell Jr, A H Auslender, R W Guy, C R McClinton, S S Welch |
| NASA/AIAA-2002-5442 | MANAGING MDO SOFTWARE DEVELOPMENT PROJECTS | J C Townsend, A O Salas |
| NASA/AIAA-2003-0012 | Mach 4 Performance of a Fixed-Geometry Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition | M K Smart, C A Trexler |
| NASA-aiaa-2003-1423.pdf | Structural Stability of a Stiffened Aluminum Fuselage Panel Subjected to Combined Mechanical And Internal Pressure Loads | M Rouse, R D Young, R E Gehrki |
| NASA/AIAA-2003-1656 | On the Exploitation of Sensitivity Derivatives for Improving Sampling Methods | Y Cao, M Y Hussaini, T A Zang |
| NASA/AIAA-2003-1768 | ELECTROSPUN ELECTROACTIVE POLYMERS FOR AEROSPACE APPLICATIONS | K J Pawlowski, T L St.Clair, A C McReynolds, C Park, Z Ounaies, E J Siochi, J S Harrison |
| NASA/AIAA-2003-1961 | Contributions of the NASA Langley Research Center to the DARPA/AFRL/NASA/ Northrop Grumman Smart Wing Program | J P Florance, A W Burner, G A Fleming, C A Hunter, S S Graves, C A Martin |
| NASA/AIAA-2003-1991 | FAILURE CRITERIA FOR FRP LAMINATES IN PLANE STRESS | C G Dávila, N Jaunky, S Goswami |
| NASA/AIAA-2003-2125 | The Mars Exploration Rovers Entry Descent and Landing and the Use of Aerodynamic Decelerators | A Steltzner, P Desai, W Leef, R Brunol |
| NASA/AIAA-2003-2697 | STRUCTURES AND MATERIALS TECHNOLOGIES FOR EXTREME ENVIRONMENTS APPLIED TO REUSABLE LAUNCH VEHICLES | S J Scotti, C Clay, M Rezin |
| NASA/aiaa-2003-3639 | COMPUTATIONAL AEROHEATING PREDICTIONS FOR MARS LANDER CONFIGURATIONS | K T Edquist S J Alter |
| NASA/AIAA-2003-3764 | A Thermal Analysis Approach for the Mars Odyssey Spacecraft's Solar Array | J A Dec, R M Amundsen |
| NASA/AIAA-2003-4181 | VOLUMETRIC NEAR-FIELD MICROWAVE PLASMA GENERATION | R J Exton, R J Balla, G C Herring, S Popovic, L Vuskovic |
| NASA/AIAA-2003-6915 | SHARP REFRACTORY COMPOSITE LEADING EDGES ON HYPERSONIC VEHICLES | S P Walker, B J Sullivan |
| NASA/AIAA-2003-7084 | X-43C PLANS AND STATUS | P L Moses |
| NASA/AIAA-2004-5185 | Simulation and Analyses of Staging Maneuvers of Next Generation Reusable Launch Vehicles | B N Pamadi, T A Neirynck, P F Covell, N Hotchko, D Bose |
| NASA-ieee-95-tns | Effects of Target Fragmentation on Evaluation of LET Spectra From Space Radiation in Low-Earth Orbit (LEO) Environment: Impact on SEU Predictions | J L Shinn, F A Cucinotta, J W Wilson, G D Badhwar, P M O'Neill, F F Badavi |
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