Ground Demonstration of a Spinning Solar Sail Deployment Concept (Englisch)
- Neue Suche nach: Salama, M.
- Neue Suche nach: White, C.
- Neue Suche nach: Leland, R.
- Neue Suche nach: Salama, M.
- Neue Suche nach: White, C.
- Neue Suche nach: Leland, R.
In:
JOURNAL OF SPACECRAFT AND ROCKETS
;
40
;
9-14
;
2003
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ISSN:
- Aufsatz (Zeitschrift) / Print
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Titel:Ground Demonstration of a Spinning Solar Sail Deployment Concept
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Beteiligte:
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Erschienen in:JOURNAL OF SPACECRAFT AND ROCKETS ; 40 ; 9-14
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Verlag:
- Neue Suche nach: AMERICAN INST OF AERONAUTICS AND ASTRONAUTICS
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Erscheinungsdatum:01.01.2003
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Format / Umfang:6 pages
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ISSN:
-
Medientyp:Aufsatz (Zeitschrift)
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Format:Print
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Sprache:Englisch
- Neue Suche nach: 629
- Weitere Informationen zu Dewey Decimal Classification
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Klassifikation:
DDC: 629 -
Datenquelle:
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Inhaltsverzeichnis – Band 40
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Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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Journal SupportE. Vincent Zoby et al. | 2003
- 1
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EDITORIAL - Journal SupportZoby, E.V. et al. | 2003
- 5
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Reviewers for 1 October 200130 September 2002| 2003
- 5
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Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty| 2003
- 5
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EDITORIAL - Reviewers for 1 October 2001-30 September 2002| 2003
- 5
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EDITORIAL - Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty| 2003
- 6
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EDITORIAL - Ethical Standards for Publication of Aeronautics and Astronautics Research| 2003
- 6
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Ethical Standards for Publication of Aeronautics and Astronautics Research| 2003
- 7
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EDITORIAL - AIAA Manuscript Review Process| 2003
- 8
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Introduction: Experiment and Testing of Gossamer SpacecraftChris Jenkins / John Lassiter et al. | 2003
- 8
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EXPERIMENT AND TESTING OF GOSSAMER SPACECRAFT - Introduction: Experiment and Testing of Gossamer SpacecraftJenkins, C. et al. | 2003
- 9
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EXPERIMENT AND TESTING OF GOSSAMER SPACECRAFT - Ground Demonstration of a Spinning Solar Sail Deployment ConceptSalama, M. et al. | 2003
- 9
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Ground Demonstration of a Spinning Solar Sail Deployment ConceptM. Salama / C. White / R. Leland et al. | 2003
- 15
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EXPERIMENT AND TESTING OF GOSSAMER SPACECRAFT - Structural Dynamics Experimental Activities in Ultralightweight and Inflatable Space StructuresPappa, R.S. et al. | 2003
- 15
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Structural Dynamics Experimental Activities in Ultralightweight and Inflatable Space StructuresRichard S. Pappa / John O. Lassiter / Brian P. Ross et al. | 2003
- 24
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Dynamic Characterization of an Inflatable Concentrator for Solar Thermal Propulsion (EN)Leigh, L. M. / Tinker, M. L. et al. | 2003
- 24
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EXPERIMENT AND TESTING OF GOSSAMER SPACECRAFT - Dynamic Characterization of an Inflatable Concentrator for Solar Thermal Propulsion (EN)Leigh, L.M. et al. | 2003
- 24
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Dynamic Characterization of an Inflatable Concentrator for Solar Thermal PropulsionLarry M. Leigh / Michael L. Tinker et al. | 2003
- 27
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Structural Modeling of a Five-Meter Thin-Film Inflatable Antenna/ConcentratorKurt B. Smalley / Michael L. Tinker / W. Scott Taylor et al. | 2003
- 27
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EXPERIMENT AND TESTING OF GOSSAMER SPACECRAFT - Structural Modeling of a Five-Meter Thin-Film Inflatable Antenna-Concentrator (EN)Smalley, K.B. et al. | 2003
- 27
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Structural Modeling of a Five-Meter Thin-Film Inflatable Antenna/Concentrator (EN)Smalley, K. B. / Tinker, M. L. / Taylor, W. S. et al. | 2003
- 30
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NavierStokes Computations for Body/Cruciform Grid Fin ConfigurationHerng Lin / Juan Cheng Huang / Ching-Chang Chieng et al. | 2003
- 39
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Semiempirical Method for Predicting Aerodynamics of Trailing-Edge FlapsF. G. Moore / T. C. Hymer et al. | 2003
- 419
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Simulation of Dual One-Way Ranging MeasurementsJeongrae Kim / Byron D. Tapley et al. | 2003
- 49
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Meteorological Forecast Model Applications to Aerodynamic DeceleratorsTerry C. Jameson / S. A. Luces / Stephen F. Kirby et al. | 2003
- 56
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Optimization of Low-Perigee Spacecraft AerodynamicsD. Stuart Bowman / Mark J. Lewis et al. | 2003
- 64
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Reentry Flight Controller Design Using Nonlinear Dynamic InversionR. R. da Costa / Q. P. Chu / J. A. Mulder et al. | 2003
- 72
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Probabilistic Risk Assessment Strategy for Damage-Tolerant Composite Spacecraft Component Structural DesignNorman F. Knight / Edward H. Glaessgen / David W. Sleight et al. | 2003
- 83
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Thermoelastic Analysis of a Kick Motor Nozzle Incorporating Spatially Reinforced CompositesJae-Seok Yoo / In-Hyun Cho / Chun-Gon Kim et al. | 2003
- 92
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Pseudodomain Fracture Analysis of Instrumented Analog Rocket MotorsF. C. Wong et al. | 2003
- 101
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Adaptive State Filtering for Space Shuttle Main Engine Turbine Health MonitoringRube B. Williams / Alexander G. Parlos et al. | 2003
- 110
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Modification of a 5-eV Atomic-Oxygen Laser Detonation SourceE. Grossman / I. Gouzman / V. Viel-Inguimbert / M. Dinguirard et al. | 2003
- 114
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Probability of a Laser Illuminating a Space ObjectRussell P. Patera et al. | 2003
- 119
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Fundamental Strategies for Control of a Tethered System in Elliptical OrbitsNoboru Takeichi / M. C. Natori / Nobukatsu Okuizumi et al. | 2003
- 126
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Mach 10 Hypersonic Nozzle: Improved Flow QualityJohn Lacey / Yasutoshi Inoue / Akio Higashida / Manabu Inoue / Kouichi Ishizaka / John J. Korte et al. | 2003
- 132
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ENGINEERING NOTES - Solar Array Modeling for Space Station S-Band-Global Positioning System Communications AnalysisHwu, S.U. et al. | 2003
- 132
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Solar Array Modeling for Space Station S-Band/Global Positioning System Communications AnalysisShian U. Hwu / Yin-Chung Loh / L. A. Johnson / R. J. Panneton et al. | 2003
- 133
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Investigation of a Laser-Supported Directed-Energy "Air Spike" in Hypersonic FlowM. A. S. Minucci / P. G. P. Toro / J. B. Chanes / A. G. Ramos / A. L. Pereira / H. T. Nagamatsu / L. N. Myrabo et al. | 2003
- 133
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ENGINEERING NOTES - Investigation of a Laser-Supported Directed-Energy "Air Spike" in Hypersonic FlowMinucci, M.A.S. et al. | 2003
- 136
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Plume Interference Effects on Missile BodiesS. Raghunathan / H. D. Kim / E. Benard / P. Mallon / R. Harrison et al. | 2003
- 136
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ENGINEERING NOTES - Plume Interference Effects on Missile BodiesRaghunathan, S. et al. | 2003
- 138
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Implementation of an Aerodynamic Toolbox in a Reentry Flight SimulatorA. Guidi / Q. P. Chu / J. A. Mulder / J. Buursink et al. | 2003
- 138
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ENGINEERING NOTES - Implementation of an Aerodynamic Toolbox in a Reentry Flight SimulatorGuidi, A. et al. | 2003
- 141
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ENGINEERING NOTES - Radiating Fin Analysis Using an Extended Perturbation Series Solution TechniqueHarris, D.K. et al. | 2003
- 141
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Radiating Fin Analysis Using an Extended Perturbation Series Solution TechniqueD. K. Harris / F. Simionescu et al. | 2003
- 143
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Temperature Dependence in Erosion Rates of Polyimide Under Hyperthermal Atomic Oxygen ExposuresKumiko Yokota / Masahito Tagawa / Nobuo Ohmae et al. | 2003
- 143
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ENGINEERING NOTES - Temperature Dependence in Erosion Rates of Polyimide Under Hyperthermal Atomic Oxygen ExposuresYokota, K. et al. | 2003
- 145
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New Forward/Backward Sweeping Parabolized NavierStokes AlgorithmHiromasa Kato / John C. Tannehill et al. | 2003
- 153
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Numerical Prediction of Laminar Shock/Shock Interactions in Hypersonic FlowDomenic D&apos / Ambrosio et al. | 2003
- 162
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Aeroelasticity of Composite Aerovehicle Wings in Supersonic FlowsZhanming Qin / Liviu Librescu / Piergiovanni Marzocca et al. | 2003
- 174
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Magnetohydrodynamic Control on Hypersonic Aircraft Under "Ajax" ConceptA. L. Kuranov / E. G. Sheikin et al. | 2003
- 183
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Challenges in Comparing Numerical Solutions for Optimum Weights of Stiffened ShellsSatchi Venkataraman / Luciano Lamberti / Raphael T. Haftka / Theodore F. Johnson et al. | 2003
- 193
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Computational Design Approach to Propellant SettlingG. D. Grayson et al. | 2003
- 201
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Assessment of Thermovibrational Theory: Application to G -Jitter on the Space StationR. Savino / M. Lappa et al. | 2003
- 211
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Laboratory Tests on 110-Volt Solar Arrays in Simulated Geosynchronous Orbit EnvironmentMengu Cho / Raju Ramasamy / Toshiaki Matsumoto / Kazuhiro Toyoda / Yukishige Nozaki / Masato Takahashi et al. | 2003
- 221
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Laboratory Tests on 110-Volt Solar Arrays in Ion Thruster Plasma EnvironmentMengu Cho / Raju Ramasamy / Kazuhiro Toyoda / Yukishige Nozaki / Masato Takahashi et al. | 2003
- 230
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Total Densities Derived from Accelerometer DataSean Bruinsma / Richard Biancale et al. | 2003
- 237
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Spacecraft Angular Velocity Estimation Using Sequential Observations of a Single Directional VectorYaakov Oshman / Franc-para / ois Dellus et al. | 2003
- 248
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Satellite Close-Approach Filtering Using Genetic AlgorithmsAnthony L. Faulds / David B. Spencer et al. | 2003
- 253
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Optimum Thrust Pitch Profiles for Certain Orbit Control ProblemsJean A. Ké / chichian et al. | 2003
- 260
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Optimal Control Law for Interplanetary Trajectories with Nonideal Solar SailGuido Colasurdo / Lorenzo Casalino et al. | 2003
- 266
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Multi-Objective Optimization of Communication Satellites with Two-Branch Tournament Genetic AlgorithmRania A. Hassan / William A. Crossley et al. | 2003
- 273
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Comparative Assessment of Rocket-Propelled Single-Stage-to-Orbit ConceptsMartin J. Bayer et al. | 2003
- 279
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Flexibility and the Value of On-Orbit Servicing: New Customer-Centric PerspectiveJoseph H. Saleh / Elisabeth S. Lamassoure / Daniel E. Hastings / Dava J. Newman et al. | 2003
- 292
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Hypersonic Missile Requirements and Operational Tradeoff StudiesRichard M. Stuckey / Mark J. Lewis et al. | 2003
- 292
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ENGINEERING NOTES - Hypersonic Missile Requirements and Operational Tradeoff StudiesStuckey, R.M. et al. | 2003
- 294
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Hypersonic Aerodynamic Heating Prediction Using Weighted Essentially Nonoscillatory SchemesTheodore K. Lee / Xiaolin Zhong / Leslie Gong / Robert Quinn et al. | 2003
- 294
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ENGINEERING NOTES - Hypersonic Aerodynamic Heating Prediction Using Weighted Essentially Nonoscillatory SchemesLee, T.K. et al. | 2003
- 298
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Stagnation-Point Density of Hypersonic Ions in a Repelling Plasma SheathIoannis G. Mikellides / Myron J. Mandell / Ira Katz et al. | 2003
- 298
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ENGINEERING NOTES - Stagnation-Point Density of Hypersonic Ions in a Repelling Plasma SheathMikellides, I.G. et al. | 2003
- 301
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Rationale for Supersonic Afterburning Rocket EnginesG. E. Dorrington et al. | 2003
- 301
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ENGINEERING NOTES - Rationale for Supersonic Afterburning Rocket EnginesDorrington, G.E. et al. | 2003
- 305
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Computational Aerothermodynamics in Aeroassist ApplicationsPeter A. Gnoffo et al. | 2003
- 313
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Methodology for Turbulence Model Validation: Application to Hypersonic FlowsChristopher J. Roy / Frederick G. Blottner et al. | 2003
- 326
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Compressibility Correction for the Spalart-Allmaras Model in Free-Shear FlowsRenato Paciorri / Filippo Sabetta et al. | 2003
- 332
-
Hypersonic Flight Transition Data Analysis Using Parabolized Stability Equations with Chemistry EffectsMujeeb R. Malik et al. | 2003
- 345
-
Chimera Simulations of Supersonic Flows over a Complex Satellite Launcher ConfigurationEdson Basso / Alexandre P. Antunes / Jo-agrave, o Luiz F. Azevedo et al. | 2003
- 356
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Prediction of Damping Coefficients Using the Unsteady Euler EquationsSoo Hyung Park / Yoonsik Kim / Jang Hyuk Kwon et al. | 2003
- 363
-
Numerical Investigation of Canard-Controlled Missile with Planar and Grid FinsJames De Spirito / Milton E. Vaughn / W. David Washington et al. | 2003
- 371
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Pitch Control During Autonomous Aerobraking for Near-Term Mars ExplorationWyatt R. Johnson / James M. Longuski / Daniel T. Lyons et al. | 2003
- 380
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Design and Optimization of Low-Thrust Trajectories with Gravity AssistsT. Troy McConaghy / Theresa J. Debban / Anastassios E. Petropoulos / James M. Longuski et al. | 2003
- 388
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Comparison of Obstacle Avoidance Strategies for Mars LandersAndrew J. Sinclair / Norman G. Fitz-Coy et al. | 2003
- 396
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Imagery Payload Design for Passive Magnetically Stabilized MicrosatelliteZuu-Chang Hong / Chung-Hsien Lin / Huan-Jung Lin et al. | 2003
- 405
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Forecast E10.7 for Improved Low-Earth-Orbit Satellite OperationsTobiska, W.K. et al. | 2003
- 405
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Forecast E for Improved Low-Earth-Orbit Satellite OperationsW. Kent Tobiska et al. | 2003
- 411
-
Probabilistic Methods for Aerospace System Conceptual DesignNatasha Smith / Sankaran Mahadevan et al. | 2003
- 426
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Probabilistic Risk Assessment of Solid-Propellant Rocket MotorsUnyime O. Akpan / Timothy E. Dunbar / Franklin C. Wong et al. | 2003
- 433
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ENGINEERING NOTES - Transfer Between Circular and Hyperbolic Orbits Using Analytical Maximum Thrust ArcsAzimov, D.M. et al. | 2003
- 433
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Transfer Between Circular and Hyperbolic Orbits Using Analytical Maximum Thrust ArcsDilmurat M. Azimov / Robert H. Bishop et al. | 2003
- 437
-
Performance Analysis of Thermal Protection System of a Solid Rocket NozzleV. Jones / K. N. Shukla et al. | 2003
- 437
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ENGINEERING NOTES - Performance Analysis of Thermal Protection System of a Solid Rocket NozzleJones, V. et al. | 2003
- 441
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Introduction: A Historical CelebrationE. Vincent Zoby et al. | 2003
- 441
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A HISTORICAL CELEBRATION - Introduction: A Historical CelebrationZoby, E.V. et al. | 2003
- 442
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Memoirs: Obtaining the Right Solution to Thermophysics ProblemsFrederick G. Blottner et al. | 2003
- 442
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A HISTORICAL CELEBRATION - Memoirs: Obtaining the Right Solution to Thermophysics ProblemsBlottner, F.G. et al. | 2003
- 459
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A HISTORICAL CELEBRATION - Dr. Antonio Ferri's Contribution to Supersonic Transport Sonic-Boom TechnologyBobbitt, P.J. et al. | 2003
- 459
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Dr. Antonio Ferri's Contribution to Supersonic Transport Sonic-Boom TechnologyPercy J. Bobbitt / Domenic J. Maglieri et al. | 2003
- 467
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Lester Lees and Hypersonic AerodynamicsRussell M. Cummings / Hsun-Tiao Yang et al. | 2003
- 467
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A HISTORICAL CELEBRATION - Lester Lees and Hypersonic AerodynamicsCummings, R.M. et al. | 2003
- 475
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A HISTORICAL CELEBRATION - Early Experimental Programs of the American Rocket Society 1930-1941Springer, A.M. et al. | 2003
- 475
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Early Experimental Programs of the American Rocket Society 19301941Anthony M. Springer et al. | 2003
- 491
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A HISTORICAL CELEBRATION - Development of U.S. Air Force Intercontinental Ballistic Missile Weapon SystemsLin, T.C. et al. | 2003
- 491
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Development of U.S. Air Force Intercontinental Ballistic Missile Weapon SystemsTony C. Lin et al. | 2003
- 510
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Evolution of Ordnance Subsystems and Components in Air Force Strategic Missile SystemsB. D. Webster / L. C. Yang et al. | 2003
- 510
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A HISTORICAL CELEBRATION - Evolution of Ordnance Subsystems and Components in Air Force Strategic Missile SystemsWebster, B.D. et al. | 2003
- 523
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A HISTORICAL CELEBRATION - Applying Jet Interaction TechnologyCassel, L.A. et al. | 2003
- 523
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Applying Jet Interaction TechnologyLouis A. Cassel et al. | 2003
- 538
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Introduction: Analysis and Design of Gossamer SpacecraftMark Lake et al. | 2003
- 538
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ANALYSIS AND DESIGN OF GOSSAMER SPACECRAFT - Introduction: Analysis and Design of Gossamer SpacecraftLake, M. et al. | 2003
- 539
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Scalable Solar-Sail Subsystem Design ConceptDavid M. Murphy / Thomas W. Murphey / Paul A. Gierow et al. | 2003
- 539
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ANALYSIS AND DESIGN OF GOSSAMER SPACECRAFT - Scalable Solar-Sail Subsystem Design ConceptMurphy, D.M. et al. | 2003
- 548
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ANALYSIS AND DESIGN OF GOSSAMER SPACECRAFT - Modeling of Gossamer Space Structures with Distributed Transfer Function MethodFang, H. et al. | 2003
- 548
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Modeling of Gossamer Space Structures with Distributed Transfer Function MethodHoufei Fang / Michael Lou / Bingen Yang / Yaubin Yang et al. | 2003
- 553
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Modeling Discontinuous Axisymmetric Active Optical MembranesJames W. Rogers / Gregory S. Agnes et al. | 2003
- 553
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ANALYSIS AND DESIGN OF GOSSAMER SPACECRAFT - Modeling Discontinuous Axisymmetric Active Optical MembranesRogers Jr, J.W. et al. | 2003
- 565
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ANALYSIS AND DESIGN OF GOSSAMER SPACECRAFT - Optimization of Ring Trusses for Antenna Structures Using Line GeometryKnight, B. et al. | 2003
- 565
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Optimization of Ring Trusses for Antenna Structures Using Line GeometryByron Knight / Joseph Duffy / Carl Crane et al. | 2003
- 570
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Investigations of a Control Surface Seal for Reentry VehiclesPatrick H. Dunlap / Bruce M. Steinetz / Donald M. Curry / Jeffrey J. Demange / H. Kevin Rivers / Su-Yuen Hsu et al. | 2003
- 584
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Diffusion and Chemical Reaction by the Finite Element MethodD. T. Wadiak / T. K. Hight et al. | 2003
- 591
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Feasibility of a Galileo-Style Tour of the Uranian SatellitesAndrew F. Heaton et al. | 2003
- 597
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Asymptotic Magnetic Field Expansion in Mini-Magnetospheric Plasma PropulsionIra Katz et al. | 2003
- 597
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ENGINEERING NOTES - Asymptotic Magnetic Field Expansion in Mini-Magnetospheric Plasma PropulsionParks, D.E. et al. | 2003
- 598
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Algebraic Correlation for High-Speed Transition Prediction on Sphere ConesKenneth K. Muramoto et al. | 2003
- 598
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ENGINEERING NOTES - Algebraic Correlation for High-Speed Transition Prediction on Sphere ConesMuramoto, K.K. et al. | 2003
- 601
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Comment on "X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data"Dinesh K. Prabhu / Joseph G. Marvin / Carol B. Davies / Michael J. Wright / Ethiraj Venkatapathy / Periklis E. Papadopoulos / James L. Brown et al. | 2003
- 601
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TECHNICAL COMMENTS - Comment on "X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data"Prabhu, D.K. et al. | 2003
- 602
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Reply by the Author to Prabhu et al.Brian R. Hollis et al. | 2003
- 602
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TECHNICAL COMMENTS - Reply by the Author to Prabhu et alHollis, B.R. et al. | 2003
- 605
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Novel Approach for Maneuvering Reentry Vehicle DesignT. C. Lin / L. K. Sproul / S. A. McKeel / T. P. Shivananda / J. Kealos / P. Fote / N. Thyson / B. L. Reeves et al. | 2003
- 615
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Flight-Dynamics Instability Induced by Heat-Shield Ablation Lag PhenomenonT. C. Lin / L. K. Sproul / M. Olmos / N. A. Thyson et al. | 2003
- 622
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Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5P. Gnemmi / J. Srulijes / K. Roussel / K. Runne et al. | 2003
- 632
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Computational Fluid Dynamics Prediction of the Beagle 2 Aerodynamic DatabasePeter A. Liever / Sami D. Habchi / Simon I. Burnell / J. Steve Lingard et al. | 2003
- 639
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Response of a Near Spherically Symmetric Spacecraft to a Stuck-On ThrusterTrevor Williams / Sergei Tanygin et al. | 2003
- 648
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Numerical Simulation of Titan IVB Transonic Buffet EnvironmentW. A. Engblom et al. | 2003
- 657
-
Approach for Combining Spacecraft Attitude and Thermal Control SystemsRenuganth Varatharajoo / Ralph Kahle / Stefanos Fasoulas et al. | 2003
- 665
-
Mission Profile of Targeted Splashdown for Space Station MirVladimir Luchinski / Rafail Murtazin / Oleg Sytin / Yuri Ulybyshev et al. | 2003
- 672
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Atmospheric Flight on Venus: A Conceptual DesignGeoffrey A. Landis / Anthony Colozza / Christopher M. Lamarre et al. | 2003
- 678
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Assessing the Instantaneous Risk of Direct Laser ImpingementSalvatore Alfano et al. | 2003
- 682
-
Analysis of Nonstationary Vibroacoustic Flight Data Using a Damage-Potential BasisS. J. Dimaggio / B. H. Sako / S. Rubin et al. | 2003
- 690
-
Mars Entry Simulation Using an Inductively Heated Plasma GeneratorG. Herdrich / M. Auweter-Kurtz / P. Endlich / H. Kurtz et al. | 2003
- 690
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ENGINEERING NOTES - Mars Entry Simulation Using an Inductively Heated Plasma GeneratorHerdrich, G. et al. | 2003
- 694
-
Assessment of TurbulenceChemistry Interactions in Missile Exhaust Plume Signature AnalysisW. H. Calhoon / D. C. Kenzakowski et al. | 2003
- 694
-
ENGINEERING NOTES - Assessment of Turbulence -- Chemistry Interactions in Missile Exhaust Plume Signature AnalysisCalhoon Jr, W.H. et al. | 2003
- 696
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ENGINEERING NOTES - Nonlinear Predictive Attitude Control of Spacecraft Under External DisturbancesMyung, H.-S. et al. | 2003
- 696
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Nonlinear Predictive Attitude Control of Spacecraft Under External DisturbancesHyun-Sam Myung / Hyochoong Bang et al. | 2003
- 700
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Hypersonic FlowLester Lees et al. | 2003
- 700
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A HISTORICAL CELEBRATION - Hypersonic Flow Reprinted from IAS-RAeS Proceedings -- 1955, pp. 241-276Lees, L. et al. | 2003
- 736
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A Time-Dependent Computaional Method for Blunt Body FlowsGino Moretti / Michael Abbett et al. | 2003
- 736
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A HISTORICAL CELEBRATION - A Time-Dependent Computational Method for Blunt Body Flows Reprinted from AIAA Journal, Vol. 4, No. 12, 1966, pp. 2136-2141Moretti, G. et al. | 2003
- 736
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A Time-Dependent Computational Method for Blunt Body FlowsMoretti, G. / Abbett, M. et al. | 2003
- 742
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Machine Calculaltion of Compressible Laminar Boundary LayersA. M. O. Smith / Darwin W. Clutter et al. | 2003
- 742
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A HISTORICAL CELEBRATION - Machine Calculation of Compressible Laminar Boundary Layers Reprinted from AIAA Journal, Vol. 3, No. 4, 1965, pp. 639-647Smith, A.M.O. et al. | 2003
- 742
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Machine Calculation of Compressible Laminar Boundary LayersSmith, A. M. O. / Clutter, D. W. et al. | 2003
- 751
-
Three-Dimensional Flow around Blunt BodiesGino Moretti / Gary Bleich et al. | 2003
- 751
-
A HISTORICAL CELEBRATION - Three-Dimensional Flow Around Blunt Bodies Reprinted from AIAA Journal, Vol. 5, No. 9, 1967, pp. 1557-1562Moretti, G. et al. | 2003
- 757
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A HISTORICAL CELEBRATION - The Effect of Viscosity in Hypervelocity Impact Cratering Reprinted from AIAA Paper 69-354, 1969MacCormack, R.W. et al. | 2003
- 757
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The Effect of Viscosity in Hypervelocity Impact CrateringRobert MacCormack et al. | 2003
- 764
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Theoretical and Experimental Study of Supersonic Steady Flow around Inclined Bodies of RevolutionJohn V. Rakich et al. | 2003
- 764
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A HISTORICAL CELEBRATION - Theoretical and Experimental Study of Supersonic Steady Flow Around Inclined Bodies of Revolution Reprinted from AIAA Journal, Vol. 8, No. 3, 1970, pp. 511-518Rakich, J.V. et al. | 2003
- 772
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Turbulence Modeling for Computational AreodynamicsJoseph G. Marvin et al. | 2003
- 772
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Turbulence Modeling for Computational AerodynamicsMarvin, J. G. et al. | 2003
- 772
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A HISTORICAL CELEBRATION - Turbulence Modeling for Computational Aerodynamics Reprinted from AIAA, Journal, Vol. 21, No. 7, 1983, pp. 941-955Marvin, J.G. et al. | 2003
- 787
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Numerical Solution of the Hypersonic Viscous Shock-Layer EquationsR. T. Davis et al. | 2003
- 787
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A HISTORICAL CELEBRATION - Numerical Solution of the Hypersonic Viscous Shock-Layer Equations Reprinted from AIAA Journal, Vol. 8, No. 5, 1970, pp. 843-851Davis, R.T. et al. | 2003
- 796
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Blunt-Nose Inviscid Airflows With Coupled Nonequilibrium ProcessesJ. Gorden Hall / Alan Q. Eschenroeder / Paul V. Marrone et al. | 2003
- 796
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A HISTORICAL CELEBRATION - Blunt-Nose Inviscid Airflows with Coupled Nonequilibrium Processes Reprinted from Journal of the Aerospace Sciences, Vol. 29, No. 9, 1962, pp. 1038-1051Hall, J.G. et al. | 2003
- 810
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Chemical Nonequilibrium Boundary LayerF. G. Blottner et al. | 2003
- 810
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A HISTORICAL CELEBRATION - Chemical Nonequilibrium Boundary Layer Reprinted from AIAA Journal, Vol. 2, No. 2, 1964, pp. 232-240Blottner, F.G. et al. | 2003
- 819
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An Engineering Survey of Radiating Shock LayersJohn D. Anderson et al. | 2003
- 819
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A HISTORICAL CELEBRATION - An Engineering Survey of Radiating Shock Layers Reprinted from AIAA Journal, Vol. 7, No. 9, 1969, pp. 1665-1675Anderson Jr, J.D. et al. | 2003
- 830
-
Direct Simulation of Transitional Flow for Hypersonic Reentry ConditionsJames N. Moss / Graeme A. Bird et al. | 2003
- 830
-
A HISTORICAL CELEBRATION - Direct Simulation of Transitional Flow for Hypersonic Reentry Conditions Reprinted from AIAA Paper 84-0223, Jan. 1984Moss, J.N. et al. | 2003
- 845
-
Governing Equations for Weakly Ionized Plasma Flowfields of Aerospace VehiclesEswar Josyula / William F. Bailey et al. | 2003
- 858
-
Dot-Projection Photogrammetry and Videogrammetry of Gossamer Space StructuresRichard S. Pappa / Jonathan T. Black / Joseph R. Blandino / Thomas W. Jones / Paul M. Danehy / Adrian A. Dorrington et al. | 2003
- 868
-
Optimal Active Control of Launch Vibrations of Space StructuresRatneshwar Jha / Matthew Pausley / Goodarz Ahmadi et al. | 2003
- 875
-
Spacecraft Charging for Microsatellite KITSAT-3H. J. Kim / J. J. Lee / J. G. Rhee / E. S. Lee / K. W. Min / D. K. Sung / J. Seon / Y. H. Jung / S. D. Park et al. | 2003
- 882
-
Genetic Algorithm and Calculus of Variations-Based Trajectory Optimization TechniqueAdam Wuerl / Tim Crain / Ellen Braden et al. | 2003
- 889
-
ENGINEERING NOTES - Station Collocation Design Algorithm for Multiple Geostationary Satellites OperationPark, B.-K. et al. | 2003
- 889
-
Station Collocation Design Algorithm for Multiple Geostationary Satellites OperationBong-Kyu Park / Min-Jea Tahk / Hyo-Choong Bang / Sung-Bong Choi et al. | 2003
- 893
-
Dual-Code Thin-Layer Parabolized NavierStokes Strategy for Supersonic Flows over Spinning BodiesOmid Abouali / Mohammad M. Alishahi / Homayoon Emdad / Goodarz Ahmadi et al. | 2003
- 893
-
ENGINEERING NOTES - Dual-Code Thin-Layer Parabolized Navier-Stokes Strategy for Supersonic Flows over Spinning BodiesAbouali, O. et al. | 2003
- 898
-
The Buckling of Thin Cylindrical Shells under Axial CompressionTheodore von K-Uuml / rm-Uuml / n, Hsue-Shen Tsien et al. | 2003
- 898
-
HISTORICAL CELEBRATION - The Buckling of Thin Cylindrical Shells under Axial Compression - Reprinted from Journal of the Aeronautical Sciences, Vol. 8, No. 8, 1941, pp. 303-312Kármán, T.von et al. | 2003
- 908
-
Some Recent Advances in the Investigation of Shell BucklingManuel Stein et al. | 2003
- 908
-
HISTORICAL CELEBRATION - Some Recent Advances in the Investigation of Shell Buckling - Reprinted from AIAA Journal, Vol. 6, No. 12, 1968, pp. 2339-2345; Technical Comment and Reply, pp. 2459-2461Stein, M. et al. | 2003
- 918
-
A Survey of Some Buckling ProblemsBernard Budiansky / John W. Hutchginson et al. | 2003
- 918
-
HISTORICAL CELEBRATION - A Survey of Some Buckling Problems - Reprinted from AIAA Journal, Vol. 4, No. 9, 1966, pp. 1505-1510Budiansky, B. et al. | 2003
- 924
-
HISTORICAL CELEBRATION - Stress, Buckling, and Vibration of Prismatic Shells - Reprinted from AIAA Journal, Vol. 9, No. 10, 1971, pp. 2004-2013Bushnell, D. et al. | 2003
- 924
-
Stress, Buckling and Vibration of Prismatic ShellsDavid Bushnell et al. | 2003
- 934
-
HISTORICAL CELEBRATION - Stability of Stiffened Cylinders - Reprinted from AIAA Journal, Vol. 3, No. 12, 1965, pp. 2275-2286Hedgepeth, J.M. et al. | 2003
- 934
-
Stability of Stiffened CylindersJohn R. Hedgepeth / David B. Hall et al. | 2003
- 946
-
Attitude Stability Criteria for Dual Spin SpacecraftPeter W. Likins et al. | 2003
- 946
-
HISTORICAL CELEBRATION - Attitude Stability Criteria for Dual Spin Spacecraft - Reprinted from Journal of Spacecraft and Rockets, Vol. 4, No. 12, 1967, pp. 1638-1643Likins, P.W. et al. | 2003
- 952
-
Optimal Two- and Three-Impulse Fixed-Time Rendezvous in the Vicinity of a Circular OrbitJohn E. Prussing et al. | 2003
- 952
-
HISTORICAL CELEBRATION - Optimal Two- and Three-Impulse Fixed-Time Rendezvous in the Vicinity of a Circular Orbit - Reprinted from AIAA Journal, Vol. 8, No. 7, 1970, pp. 1221-1228Prussing, J.E. et al. | 2003
- 960
-
Optimum Low-Thrust Rendezvous and Station KeepingTheodore N. Edelbaum et al. | 2003
- 960
-
HISTORICAL CELEBRATION - Optimum Low-Thrust Rendezvous and Station Keeping - Reprinted from AIAA Journal, Vol. 2, No. 7, 1964, pp. 1196-1201Edelbaum, T.N. et al. | 2003
- 966
-
Optimal Guidance for the Space Shuttle TransitionRobert F. Stengel et al. | 2003
- 966
-
HISTORICAL CELEBRATION - Optimal Guidance for the Space Shuttle Transition - Reprinted from Journal of Spacecraft and Rockets, Vol. 11, No. 3, 1974, pp. 173-179Stengel, R.F. et al. | 2003
- 973
-
A Manually Retargeted Automatic Landing System for the Lunar Module (LM)Allan R. Klumpp et al. | 2003
- 973
-
HISTORICAL CELEBRATION - A Manually Retargeted Automatic Landing System for the Lunar Module (LM) - Reprinted from Journal of Spacecraft and Rockets, Vol. 5, No. 2, 1968, pp. 129-138Klumpp, A.R. et al. | 2003
- 983
-
Two-Dimensional Subsonic Flow of Compressible FluidsHsue-Shen Tsien et al. | 2003
- 983
-
HISTORICAL CELEBRATION - Two-Dimensional Subsonic Flow of Compressible Fluids - Reprinted from Journal of the Aeronautical Sciences, Vol. 6, No. 10, 1939, pp. 399-407Tsien, H.-S. et al. | 2003
- 992
-
HISTORICAL CELEBRATION - Compressibility Effects in Aerodynamics - Reprinted from Journal of the Aeronautical Sciences, Vol. 8, No. 9, 1941, pp. 337-356Kármán, T.von et al. | 2003
- 992
-
Compressibility Effects in AerodynamicsT H. von K-Uuml / rm-Uuml / n et al. | 2003
- 1012
-
HISTORICAL CELEBRATION - Turbulent Boundary Layer in Compressible Fluids - Reprinted from Journal of the Aeronautical Sciences, Vol. 18, No. 3, 1951, pp. 145-160, 216Driest, E.R.Van et al. | 2003
- 1012
-
Turbulent Boundary Layer in Compressible FluidsE. R. van Driest et al. | 2003
- 1029
-
First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionMilton D. van Dyke et al. | 2003
- 1029
-
HISTORICAL CELEBRATION - First- and Second-Order Theory of Supersonic Flow Past Bodies of Revolution - Reprinted from Journal of the Aeronautical Sciences, Vol. 18, No. 3, 1951, pp. 161-178, 216Dyke, M.D.Van et al. | 2003
- 1048
-
HISTORICAL CELEBRATION - Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail Configuration - Reprinted from Journal of the Aeronautical Sciences, Vol. 20, No. 5, 1953, pp. 297-308Bryson Jr, A.E. et al. | 2003
- 1048
-
Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail ConfigurationArthur F. Bryson et al. | 2003
- 1060
-
2003 JOURNAL OF SPACECRAFT AND ROCKET INDEX - Subject Index| 2003
- 1064
-
2003 JOURNAL OF SPACECRAFT AND ROCKET INDEX - Author Index| 2003
- 1066
-
2003 JOURNAL OF SPACECRAFT AND ROCKET INDEX - Chronological Index| 2003