Table Of Content

JOURNAL OF SPACECRAFT AND ROCKETS Volume 41, No. 6, November—December 2004 2004 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 1076-1079, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, pages 1080—1081, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1082-1087, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. Subject Index AIRCRAFT TECHNOLOGY, Boundary-Layer Stability and Transition A04-119 Preconditioned Newton-Method for CONVENTIONAL, STOL/VTOL 404-031 X-38 Experimental Aerothermody- Computing Supersonic and Hypersonic Non- namics equilibrium Flows Aerodynamics A04-032 X-38 Experimental Aeroheating at 404-138 Effect of Afterbody Configuration on Computational Fluid Dynamics Mach 10 Damping Coefficients for Axisymmetric Projec- A04-119 Preconditioned Newton-Method for Inlet, Nozzle, Diffuser, and Channel tiles Computing Supersonic and Hypersonic Non- Flows 404-031 X-38 Experimental Aerothermody- equilibrium Flows namics 404-118 Hybrid Large-Eddy/Reynolds-Aver- 404-075 Modeling of Chemically Reacting Communication and Air Traffic Control aragteedd NFalvoiwse r-Stokes Simulation of Shock-Sepa- Flows from a Side Jet at High Altitudes 404-035 International Space Station Ku-Band A04-060 Multiblock Compressible Navier- Jets, Wakes, and Viscid-Inviscid Flow Communications Antenna Blockage Analysis Stokes Flow Solver Applied to Complex Launch Interactions Vehicles Flight Mechanics A04-092 Three-Dimensional Hypersonic Flow A04-118 Hybrid Large-Eddy/Reynolds-Aver- Computation over Reentry Capsule Using Ener- aged Navier-Stokes Simulation of Shock-Sepa- 404-099 Navier-Stokes Computation of Pitch- gy Relaxation Method rated Flows Damping Coefficients Using Steady Coning A04-099 Navier-Stokes Computation of Pitch- Motions Damping Coefficients Using Steady Coning Plasmadynamics and MHD Motions A04-132 Arcjet Plasma Neutralization of Hall ENERGY A04-120 Compressible Wall-Injection Flows in Thrusters, Part 2: Experimental Demonstration Laminar, Transitional, and Turbulent Regimes: Photovoltaic Power Numerical Prediction Rarefied Flows 404-133 Interactions of High-Voltage Solar A04-138 Effect of Afterbody Configuration on Arrays with Their Plasma Environment: Physi- Damping Coefficients for Axisymmetric Projec- A04-121 Attitude Stability of Blunt-Body Cap- cal Processes tiles sules in Hypersonic Rarefied Regime 404-134 Interactions of High-Voltage Solar A04-137 New Computational Method to Deter- A04-075 Modeling of Chemically Reacting Arrays with Their Plasma Environment: Ground mine Trim Angle of Attack for Reentry Vehicles Flowsfrom a Side Jet at High Altitudes Tests A04-028 Numerical Simulation of a Spinning A04-093 Heat Transfer on a Hypersonic Sphere Missile with Dithering Canards Using Unstruc- with Diffuse Rarefied-Gas Injection tured Grids FLUID DYNAMICS Reacting Flows and Combustion Hypersonic Flow Boundary Layers and Heat Transfer- A04-119 Preconditioned Newton-Method for Laminar A04-093 Heat Transfer on a Hypersonic Sphere Computing Supersonic and Hypersonic Non- with Diffuse Rarefied-Gas Injection 404-032 X-38 Experimental Aeroheating at A04-092. Three-Dimensional Hypersonic Flow equilibrium Flows Mach 10 Computation over Reentry Capsule Using Ener- Separated Flows 404-034 Surface Recombination Coefficients gy Relaxation Method and Boundary-Layer Hypersonic-Flow Calcula- A04-121 Attitude Stability of Blunt-Body Cap- A04-032 X-38 Experimental Aeroheating at tions on Different Surfaces sules in Hypersonic Rarefied Regime Mach 10 1076 JOURNAL OF SPACECRAFT AND ROCKETS Volume 41, No. 6, November—December 2004 2004 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 1076-1079, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, pages 1080—1081, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1082-1087, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. Subject Index AIRCRAFT TECHNOLOGY, Boundary-Layer Stability and Transition A04-119 Preconditioned Newton-Method for CONVENTIONAL, STOL/VTOL 404-031 X-38 Experimental Aerothermody- Computing Supersonic and Hypersonic Non- namics equilibrium Flows Aerodynamics A04-032 X-38 Experimental Aeroheating at 404-138 Effect of Afterbody Configuration on Computational Fluid Dynamics Mach 10 Damping Coefficients for Axisymmetric Projec- A04-119 Preconditioned Newton-Method for Inlet, Nozzle, Diffuser, and Channel tiles Computing Supersonic and Hypersonic Non- Flows 404-031 X-38 Experimental Aerothermody- equilibrium Flows namics 404-118 Hybrid Large-Eddy/Reynolds-Aver- 404-075 Modeling of Chemically Reacting Communication and Air Traffic Control aragteedd NFalvoiwse r-Stokes Simulation of Shock-Sepa- Flows from a Side Jet at High Altitudes 404-035 International Space Station Ku-Band A04-060 Multiblock Compressible Navier- Jets, Wakes, and Viscid-Inviscid Flow Communications Antenna Blockage Analysis Stokes Flow Solver Applied to Complex Launch Interactions Vehicles Flight Mechanics A04-092 Three-Dimensional Hypersonic Flow A04-118 Hybrid Large-Eddy/Reynolds-Aver- Computation over Reentry Capsule Using Ener- aged Navier-Stokes Simulation of Shock-Sepa- 404-099 Navier-Stokes Computation of Pitch- gy Relaxation Method rated Flows Damping Coefficients Using Steady Coning A04-099 Navier-Stokes Computation of Pitch- Motions Damping Coefficients Using Steady Coning Plasmadynamics and MHD Motions A04-132 Arcjet Plasma Neutralization of Hall ENERGY A04-120 Compressible Wall-Injection Flows in Thrusters, Part 2: Experimental Demonstration Laminar, Transitional, and Turbulent Regimes: Photovoltaic Power Numerical Prediction Rarefied Flows 404-133 Interactions of High-Voltage Solar A04-138 Effect of Afterbody Configuration on Arrays with Their Plasma Environment: Physi- Damping Coefficients for Axisymmetric Projec- A04-121 Attitude Stability of Blunt-Body Cap- cal Processes tiles sules in Hypersonic Rarefied Regime 404-134 Interactions of High-Voltage Solar A04-137 New Computational Method to Deter- A04-075 Modeling of Chemically Reacting Arrays with Their Plasma Environment: Ground mine Trim Angle of Attack for Reentry Vehicles Flowsfrom a Side Jet at High Altitudes Tests A04-028 Numerical Simulation of a Spinning A04-093 Heat Transfer on a Hypersonic Sphere Missile with Dithering Canards Using Unstruc- with Diffuse Rarefied-Gas Injection tured Grids FLUID DYNAMICS Reacting Flows and Combustion Hypersonic Flow Boundary Layers and Heat Transfer- A04-119 Preconditioned Newton-Method for Laminar A04-093 Heat Transfer on a Hypersonic Sphere Computing Supersonic and Hypersonic Non- with Diffuse Rarefied-Gas Injection 404-032 X-38 Experimental Aeroheating at A04-092. Three-Dimensional Hypersonic Flow equilibrium Flows Mach 10 Computation over Reentry Capsule Using Ener- Separated Flows 404-034 Surface Recombination Coefficients gy Relaxation Method and Boundary-Layer Hypersonic-Flow Calcula- A04-121 Attitude Stability of Blunt-Body Cap- A04-032 X-38 Experimental Aeroheating at tions on Different Surfaces sules in Hypersonic Rarefied Regime Mach 10 1076 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX Shock Waves and Detonations Missile Guidance and Control Analytical and Numerical Methods A04-118 Hybrid Large-Eddy/Reynolds-Aver- A04-062 Analysis of Optimal Weaving Frequen- A04-013 |O verview of Satellite Thermal Analyti- aged Navier-Stokes Simulation of Shock-Sepa- cy of Maneuvering Targets cal Mode! rated Flows A04-075 Modeling of Chemically Reacting A04-090 Analytical Methods for Predicting A04-114 Unsteady Gasdynamics Effects in Flowsfrom a Side Jet at High Altitudes Grain Regression in Tactical Solid-Rocket Pyrotechnic Actuators Optimization Techniques Motors A04-140 Simplified Approach to Identifying Transonic Flow A04-062 Analysis of Optimal Weaving Frequen- Influential Uncertainties in Monte Carlo Analy- A04-060 Multiblock Compressible Navier— cy of Maneuvering Targets sis Stokes Flow Solver Applied to Complex Launch Pointing Systems Atmospheric and Space Sciences Vehicles A04-081 Robust Spacecraft Attitude Determina- A04-089 Simulation of Wind-Profile Perturba- Unsteady Flows tion Using Global Positioning System Receivers tions for Launch-Vehicle Design A04-113 Design and Performance of Tip-Tilt A04-114 Unsteady Gasdynamics Effects in Mirror System for Solar Telescope Environmental Effects Pyrotechnic Actuators A04-028 Numerical Simulation of a Spinning Robotics A04-110 Simultaneous Analysis of Multi-Instru- Missile with Dithering Canards Using Unstruc- A04-015 Space Test of Sensor-Fused Telerobot- ment Satellite Measurements of Atmospheric tured Grids ics for High-Precision Tasks Density A04-137 New Computational Method to Deter- Lasers and Laser Applications mine Trim Angle of Attack for Reentry Vehicles Spacecraft Dynamics A04-078 Aerogravity-Assist Maneuvering of a A04-115 |N ozzle Scale Optimum for the Impulse GUIDANCE, CONTROL, AND Tethered Satellite System Generation in a Laser Pulsejet DYNAMICS TECHNOLOGY A04-110 Simultaneous Analysis of Multi-Instru- Multidisciplinary Design Optimization ment Satellite Measurements of Atmospheric Astrodynamics Density i A04-061 Parametric Scaling Model for Nongeo- A04-129 Hybrid Precise Orbit Determination synchronous Communications Satellites A04-116 Prolonged Payload Rendezvous Using Strategy by Global Position System Tracking A04-008 Applications of Uncertainty Analysis a Tether Actuator Mass Applied to Architecture Selection of Satellite Spacecraft Guidance and Control A04-019 Oblate Earth Eclipse State Algorithm Systems for Low-Earth-Orbiting Satellites A04-088 Solar System Escape Trajectories A04-005 Risk Chair for Concurrent Design A04-088 Solar System Escape Trajectories Using Solar Sails Engineering: Satellite Swarm Illustration Using Solar Sails A04-036 Optimal Control of Tethered Planetary A04-101 Optimal Conceptual Design of Two- A04-130 Design of Tether Sling for Human Capture Missions Stage Reusable Rocket Vehicles Including Tra- Transportation System Between Earth and Mars A04-116 Prolonged Payload Rendezvous Using jectory Optimization A04-080 Optimal Low-Thrust Trajectories a Tether Actuator Mass A04-059 Minimum Mass Design of Insulation Combined with an Aeroassist Maneuver Made of Functionally Graded Material State Estimation A04-077 Tethered Planetary Capture Maneuvers A04-001 New Methods for Rapid Architecture A04-078 Aerogravity-Assist Maneuvering of a A04-081 Robust Spacecraft Attitude Determina- Selection and Conceptual Design Tethered Satellite System tion Using Global Positioning System Receivers A04-002 Multi-Attribute Tradespace Explo- A04-129 Hybrid Precise Orbit Determination ration as Front End for Effective Space System Computer Science Strategy by Global Position System Tracking Design A04-140 Simplified Approach to Identifying Trajectory Optimization A04-004 Multi-Objective, | Multidisciplinary Influential Uncertainties in Monte Carlo Analy- Design Optimization Methodology for Distrib- A04-101 Optimal Conceptual Design of Two- uted Satellite Systems SIS Stage Reusable Rocket Vehicles Including Tra- Dynamics jectory Optimization Reliability, Maintainability, and Logistics A04-080 Optimal Low-Thrust Trajectories Support A04-121 Attitude Stability of Blunt-Body Cap- Combined with an Aeroassist Maneuver sules in Hypersonic Rarefied Regime A04-016 Small-Body Encounters Using Solar A04-005 Risk Chair for Concurrent Design Sail Propulsion Engineering: Satellite Swarm Illustration Flight Mechanics A04-091 Minimum Transfer Times for Nonper- A04-010 Bayesian Analysis of Launch Vehicle A04-029 Projectile Performance, Stability, and fectly Reflecting Solar Sailcraft Success Rates Free-Flight Motion Prediction Using Computa- A04-116 Prolonged Payload Rendezvous Using A04-006 Modeling the Effects of Dispersion of tional Fluid Dynamics a Tether Actuator Mass Design Teams on System Failure Risk A04-036 Optimal Control of Tethered Planetary A04-138 Effect of Afterbody Configuration on Damping Coefficients for Axisymmetric Projec- Capture Missions LAUNCH VEHICLE AND MIS- tiles SILE (LV/M) TECHNOLOGY INTERDISCIPLINARY TOPICS Launch Vehicle Guidance and Control Aerodynamics Aerospace Management A04-018 Optimal Ascent Trajectory for Efficient A04-060 Multiblock Compressible Navier- Air Launch into Orbit A04-083 Validation and Verification of Deep- Stokes Flow Solver Applied to Complex Launch A04-082 Global Positioning System Sensor with Space Missions Vehicles A04-006 Modeling the Effects of Dispersion of Instantaneous-Impact-Point Prediction for A04-029 Projectile Performance, Stability, and Design Teams on System Failure Risk Sounding Rockets A04-009 Method for Determining Margins in Free-Flight Motion Prediction Using Computa- Missile Dynamics Conceptual Design tional Fluid Dynamics A04-010 Bayesian Analysis of Launch Vehicle A04-123 Engineering Estimates of Normal A04-029 Projectile Performance, Stability, and Success Rates Loads on Slender Airbreathing Bodies Free-Flight Motion Prediction Using Computa- A04-011 Evaluating the Cost and Risk Impacts A04-137 New Computational Method to Deter- tional Fluid Dynamics of Launch Choices mine Trim Angle of Attack for Reentry Vehicles A04-062 Analysis of Optimal Weaving Frequen- A04-012 Measuring the Value of Designing for A04-117 Skin Friction Prediction for High- cy of Maneuvering Targets Uncertain Future Downward Budget Instabilities Speed Turbulent Boundary Layers with Ablation 1078 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX A04-099 Navier-Stokes Computation of Pitch- Trajectories and Tracking Systems Mission Design and Analysis Damping Coefficients Using Steady Coning A04-018 Optimal Ascent Trajectory for Efficient A04-130 Design of Tether Sling for Human Motions Air Launch into Orbit Transportation System Between Earth and Mars Launch Vehicle and Sounding Rocket A04-082 Global Positioning System Sensor with A04-083 Validation and Verification of Deep- Systems Instantaneous-Impact-Point Prediction — for Space Missions Sounding Rockets A04-019 Oblate Earth Eclipse State Algorithm A04-101 Optimal Conceptual Design of Two- for Low-Earth-Orbiting Satellites Stage Reusable Rocket Vehicles Including Tra- Vibration A04-113 Design and Performance of Tip-Tilt jectory Optimization Mirror System for Solar Telescope A04-030 Nonlinear Aeroelastic Analysis of a A04-100 Kerosene vs. Methane: A Propellant A04-106 Effect of Space Environment on Space- Deployable Missile Control Fin Tradeoff for Reusable Liquid Booster Stages craft Surfaces Control in Sun-Synchronous Orbits Propulsion and Propellant Systems PROPULSION A04-100 Kerosene vs. Methane: A Propellant Tradeoft for Reusable Liquid Booster Stages A04-100 Kerosene vs. Methane: A Propellant Advanced Space Propulsion A04-131 Arcjet Plasma Neutralization of Hall Tradeoff for Reusable Liquid Booster Stages Thrusters, Part 1: Hybrid Thruster Mission A04-016 Small-Body Encounters Using Solar Simulation Analysis Sail Propulsion A04-091 Minimum Transfer Times for Nonper- 404-089 Simulation of Wind-Profile Perturba- A04-077 Tethered Planetary Capture Maneuvers fectly Reflecting Solar Sailcraft tions for Launch-Vehicle Design A04-014 Resonant and Ground Experimental A04-007 Creating Advanced Architecture for A04-120 Compressible Wall-Injection Flows in Study on Microwave Plasma Thruster Space Systems: Emergent Lessons from New Laminar, Transitional, and Turbulent Regimes: A04-091 Minimum Transfer Times for Nonper- Processes Numerical Prediction fectly Reflecting Solar Sailcraft A04-008 Applications of Uncertainty Analysis 404-140 Simplified Approach to Identifying A04-017 Propulsive Impulse Measurement of a Applied to Architecture Selection of Satellite Influential Uncertainties in Monte Carlo Analy- Microwave-Boosted Vehicle in the Atmosphere Systems SIS A04-115 Nozzle Scale Optimum for the Impulse A04-033 Beating the Rocket Equation: Air Generation in a Laser Pulsejet Launch with Advanced Chemical Propulsion Structural Design (Including Loads) 404-036 Optimal Control of Tethered Planetary A04-001 New Methods for Rapid Architecture A04-022 Development of Advanced Metallic- Capture Missions Selection and Conceptual Design Thermal-Protection System Prototype Hardware A04-033 Beating the Rocket Equation: Air A04-004 Multi-Objective, | Multidisciplinary Launch With Advanced Chemical Propulsion Design Optimization Methodolegy for Distrib- Subsystem Design and Ground Support uted Satellite Systems Electric Propulsion A04-002. Multi-Attribute Tradespace Explo- 404-114 Unsteady Gasdynamics Effects in ration as Front End for Effective Space System Pyrotechnic Actuators 404-132 Arcjet Plasma Neutralization of Hall Design 404-013 Overview of Satellite Thermal Analyti- Thrusters, Part 2: Experimental Demonstration cal Model A04-131 Arcjet Plasma Neutralization of Hall Mission Trajectories (Earth and Thrusters, Part 1: Hybrid Thruster Mission Interplanetary) Testing, Flight and Ground Analysis A04-016 Small-Body Encounters Using Solar A04-013 Overview of Satellite Thermal Analyti- Engine Performance Sail Propulsion cal Model A04-019 Oblate Earth Eclipse State Algorithm A04-134 Interactions of High-Voltage Solar A04-115 Nozzle Scale Optimum for the Impulse for Low-Earth-Orbiting Satellites Arrays with Their Plasma Environment: Ground Generation in a Laser Pulsejet A04-130 Design of Tether Sling for Human Tests Transportation System Between Earth and Mars Liquid Rocket Engines A04-133 Interactions of High-Voltage Soiar A04-110 Simultaneous Analysis of Multi-Instru- Arrays with Their Plasma Environment: Physi- A04-033 Beating the Rocket Equation: Air ment Satellite Measurements of Atmospheric cal Processes Launch with Advanced Chemical Propulsion Density Thermal Protection Systems Solid Rocket Motors Space Experiments A04-074 Catalytic Atom Recombination on A04-120 Compressible Wall-Injection Flows in A04-113, Design and Performance of Tip-Tilt ZrB2/SiC and HfB2/SiC Ultrahigh-Temperature Laminar, Transitional, and Turbulent Regimes: Mirror System for Solar Telescope Ceramic Composites Numerical Prediction A04-015 Space Test of Sensor-Fused Telerobot- A04-059 Minimum Mass Design of Insulation A04-090 Analytical Methods for Predicting ics for High-Precision Tasks Made of Functionally Graded Material Grain Regression in Tactical Solid-Rocket Space Systems A04-022 Development of Advanced Metallic- Motors Thermal-Protection System Prototype Hardware A04-078 Aerogravity-Assist Maneuvering of a A04-021 Preliminary Thermal-Mechanical Siz- SPACE TECHNOLOGY Tethered Satellite System ing of a Metallic Thermal Protection System A04-004 Multi-Objective. Multidisciplinary A04-020 Metallic Thermal Protection System Aerobraking Flight Mechanics Design Optimization Methodology for Distrib- Requirements, Environments, and Integrated uted Satellite Systems Concepts A04-080 Optimal Low-Thrust Trajectories A04-001 New Methods for Rapid Architecture A04-025 Development of Protective Coatings Combined with an Aeroassist Maneuver Selection and Conceptual Design A04-061 Parametric Scaling Model for Nongeo- for High-Temperature Metallic Materials Global Positioning System synchronous Communications Satellites A04-023 Fundamental Modeling and Thermal A04-084 Electromagnetic Formation Flight for Performance Issues for Metallic Thermal Protec- A04-129 Hybrid Precise Orbit Determination Multisatellite Arrays tion System Concept Strategy by Global Position System Tracking A04-083 Validation and Verification of Deep- A04-024 Metallic Thermal-Protection-System A04-082 Global Positioning System Sensor with Space Missions Panel Flutter Study Instantaneous-Impact-Point Prediction — for A04-077 Tethered Planetary Capture Maneuvers A04-139 Development of an Ablative Insulation Sounding Rockets A04-008 Applications of Uncertainty Analysis Material for Ramjet Applications International Space Station Applied to Architecture Selection of Satellite A04-026 Improving Metallic Thermal Protection Systems System Hypervelocity Impact Resistance A04-035 International Space Station Ku-Band A04-009 Method for Determining Margins in Through Numerical Simulations Communications Antenna Blockage Analysis Conceptual Design J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX 1079 A04-007 Creating Advanced Architecture for STRUCTURAL MECHANICS A04-025 Development of Protective Coatings Space Systems: Emergent Lessons from New AND MATERIALS for High-Temperature Metallic Materials Processes Aeroelasticity and Control THERMOPHYSICS Spacecraft Attitude Determination A04-030 Nonlinear Aeroelastic Analysis of a AND HEAT TRANSFER A04-081 Robust Spacecraft Attitude Determina- Deployable Missile Control Fin Ablation, Pyrolysis, Thermal tion Using Global Positioning System Receivers Materials Structural Properties Decomposition and Degradation Spacecraft Communication A04-025 Development of Protective Coatings A04-117 Skin Friction Prediction for High- for High-Temperature Metallic Materials Speed Turbulent Boundary Layers with Ablation A04-035 International Space Station Ku-Band A04-139 Development of an Ablative Insulation Structural Design Communications Antenna Blockage Analysis Material for Ramjet Applications A04-061 Parametric Scaling Model for Nongeo- A04-023 Fundamental Modeling and Thermal Aerothermodynamics/Thermal synchronous Communications Satellites Performance Issues for Metallic Thermal Protec- Protection tion System Concept Spacecraft Contamination/Sterilization A04-020 Metallic Thermal Protection System A04-093 Heat Transfer on a Hypersonic Sphere Requirements, Environments, and Integrated with Diffuse Rarefied-Gas Injection A04-106 Effect of Space Environment on Space- Concepts A04-117 Skin Friction Prediction for High- craft Surfaces Control in Sun-Synchronous A04-022, Development of Advanced Metallic- Speed Turbulent Boundary Layers with Ablation Orbits Thermal-Protection System Prototype Hardware A04-020 Metallic Thermal Protection System A04-089 Simulation of Wind-Profile Perturba- Requirements, Environments, and Integrated Spacecraft Propulsion System tions for Launch-Vehicle Design Concepts A04-074 Catalytic Atom Recombination on Integration Structural Dynamics and ZrB2/SiC and HfB2/SiC Ultrahigh-Temperature A04-018 Optimal Ascent Trajectory for Efficient Characterization Ceramic Composites A04-034 Surface Recombination Coefficients Air Launch into Orbit A04-030 Nonlinear Aeroelastic Analysis of a and Boundary-Layer Hypersonic-Flow Calcula- Deployable Missile Control Fin Spacecraft Structural Configuration, tions on Different Surfaces Design, and Analysis Structural Modeling A04-031 X-38 Experimental Aerothermody- namics A04-021 Preliminary Thermal-Mechanical Siz- A04-069 Staged Microgravity Deployment of a ing of a Metallic Thermal Protection System Thermal Modeling and Analysis Pressurizing Scale-Model Spacecraft A04-024 Metallic Thermal-Protection-System A04-021 Preliminary Thermal-Mechanical Siz- Spacecraft Test and Evaluation Panel Flutter Study ing of a Metallic Thermal Protection System Structural Optimization Thermochemistry and A04-069 Staged Microgravity Deployment of a Pressurizing Scale-Model Spacecraft A04-059 Minimum Mass Design of Insulation Chemical Kinetics Made of Functionally Graded Material A04-074 Catalytic Atom Recombination on Spacecraft Thermal Management Thermal Effects ZrB2/SiC and HfB2/SiC Ultrahigh-Temperature Ceramic Composites A04-106 Effect of Space Environment on Space- A04-023 Fundamental Modeling and Thermal A04-034 Surface Recombination Coefficients craft Surfaces Control in Sun-Synchronous Performance Issues for Metallic Thermal Protec- and Boundary-Layer Hypersonic-Flow Calcula- Orbits tion System Concept tions on Different Surfaces 1080 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX Author Index Abe, Toshio, AO4-112 Duren, Riley M., A04-083 Janssen, Susan G., A04-102 Mcintyre, T. J., A04-695 Abu-Khajeel, Hasan, A@4-021 Dutton, J. C., A04-057 Janus, J. Mark, A04-060 McManus, Hugh, A04-007 Abuseli, P. A. M., AO4-129 Edwards, Jack R., AO4-118 Jenkin, Alan, A04-105 McManus, Hugh L., A04-001 Adelfang, S. 1., A04-089 Eichmann, T. N., A04-095 Jenkin, Alan B., A04-087 Meakin, Robert L., A@4-096 Adhya, Sima, A04-019 Elias, Laila M., A04-084 Jenkins, C. H., A04-071 Mease, K. D., A04-128 Aftosmis, Michael J., A04-054 Erlandson, R. E., A04-063, A04-064, Jenkins, Rhonald, A04-090 Mee, D. J., A04-053 Alet, Irénée, A04-106 A04-065, A04-066, A04-068 Jilla, Cyrus D., A04-004 Meng, Cheng I., A04-068 Alexeenko, A. A., A04-075 Erlandson, Robert E., A04-067 Johnson, Wyatt R., A04-104 Meng, C. |., A04-064, A04-065, Alter, Stephen J., A04-032 “an, Chen-Chuan, A04-118 Jokic, Michael, A04-078 A04-066 Anderson, Jason P., A04-105 “ang, Houfei, A04-070 Jokic, Michael D., A04-130 Merski Jr., N. Ronald, A04-032 Arabshahi, Abdollah, A04-060 -ang, Yichuan, AO4-117 Juan, Yang, A04-014 Merski, N. Ronald, A04-031 Arakawa, Y., AO4-115 -armer, Dan, A04-135 Kalimuthu, R., A04-092 Mihara, Yorichika, A04-017 Armenise, |., A04-034 saye, Delphine, A04-106 Kamenetzky, Rachel, A04-037 Miller, David W., A04-004, A04-084 Ash, J. T., AO4-071 Ferguson, Dale, A04-133, A04-134 Kano, Ryouhei, A04-113 Miller, Sharon K., A04-039 Auweter-Kurtz, M., A04-119 Fink, Dale R., A04-136 Kashiwase, Toshio, A04-113 Milligan, D., A04-038 Azevedo, Joao Luiz F., A04-098 Fitzgerald, Steve M., A04-031 Kassanchine, R. H., A04-049 Minton, Timothy K., A04-050 Bacono, Shinjii, AO4-112 Foster, Winfred, A04-090 Kearns, Justin, A04-069 Moe, Kenneth, A04-110 Bae, Jae-Sung, A04-030 Freudenreich, Henry T., A04-068 Kerdanyan, Grigor, A04-070 Moe, Mildred M., A04-110 Bakos, R. J., AO4-053 Fruit, M., A04-047 Ketzer, |. L., A04-063 Montemerlo, Patrick, A04-072 Balachandar, S., A04-120 Fujita, Kazuhisa, A04-121 Kimbrel, Scott, A04-108 Montenbruck, Oliver, A04-082 Banks, Bruce A., A04-039, A05-040 Fukushima, Kazuhiko, A04-113 Kim, Dae-Kwan, A04-030 Moore, F. G., A04-027, A04-122 Barbato, M., A04-034 Galica, Gary E., AM4-112 Kimoto, Yugo, A04-112 Morgan, R. G., A04-095 Baurle, Robert A., AO4-118 Galofaro, Joel, A04-133, A04-134 Kim, Seung-Ho, A04-030 Mori, K., AO4-115 Bay, P. Michael, A04-136 Galygin, A. N., A04-049 Kiselev, Y., A04-063, A04-065, Mori, Takashige, A04-101 Beall, Gary W., A04-139 Garber, Russ, A04-006 A04-066 Moser, R. D., A04-120 Benjamin, James L., A04-005 Gascon, Nicolas, A04-132 Kleiman, J., A04-038 Motoda, Toshikazu, A04-140 Berger, Marsha J., A04-054 Gatsonis, N. A., A04-063 Klevanski, Josef, A04-100 Murata, Shinji. AO4-112 Berry, Scott A., A04-031, A04-032 Gatsonis, Nikolaos A., A04-067 Klinshpont, Edward R., A04-044 Murman, Scott M., A04-054 Bird, R. K., A04-022 Gavrilov, B. G., A04-063, A04-064, Kluever, C. A., A04-058 Nagata, Shinichi, A04-113 Bird, R. Keith, A04-025 404-065, A04-066 Kodeki, Kazuhide, A04-113 Nakagawa, Tatsuo, A04-017 Bishop, A. L., A04-095 Gavrilov, Boris G., A04-068 Komurasaki, K., AO4-115 Nakamura, Takashi, AO4-112 Blades, Eric L., A04-028 Geng, Hongbin, A04-048 Komurasaki, Kimiya, A04-017 Nathanson, Gilbert M., A04-050 Blanksby, Chris, AO04-077, A04-116 Genwang, Mao, A04-014 Kong, Edmund M. C., A04-084 Ng, R., A04-038 Blosser, Max L., A04-023, A04-024, Gibson, Glenn R., A04-102 Kosch, M. J., A04-085 Ng, Ti 404-026. A04-059 Gimelshein, S. F., A04-075 Koshiishi, Hideki, AO4-112 Ng, T. Terry, A04-055 Blosser, M. L., AO4-022 Goka, Tateo, A04-112 Kroll, Quin D., A04-035 Normand, Eugene, A04-037 Boltz, Frederick W., A04-018 Gopinath, N. S., A@4-107 Kumar, C. K., A04-063 Nota, Fabrizio, A04-126 Bounds, S., A04-063 Gorse, C., A04-034 Kumar, K. D., AO4-127 Noter, Y., A04-042, A04-043 Bounds, Scott, A04-068 Gouzman, |., A04-042, A04-043 Kwon, Daniel W., A04-084 Nozaki, Yukishige, AO4-111 Bourdon, C. J., AO4-057 Green, B. D., AO4-112 Kwon, Jang Hyuk, A04-099, A04-138 Nygaard, Tor A., A04-096 Bradford, Liselotte F.. AO4-102 Grigorevskiy, A. V., A04-049 Leavitt, J. A.. A04-128 O'Donnell, Jr., James R., A04-136 Bray, Alan, A04-139 Groom, Richard S., A04-102 Lee, Hobin S., A@4-114 Oh, David Y., A04-108 Briskman, Boris A., A04-044 Grossman, E., A04-042, A04-043 Lee, In, A04-030 Ohmae, Nobuo, A04-041 Bruno, Claudio, A04-086 Gudimenko, Y., A04-038 Lee, Kwang-Seop, A04-097 Olawsky, F., AO4-119 Budianto, Irene A., AO4-125 Guikema, Seth D., A04-010 Lee, Seungwoo, A04-129 Olds, John R., AO4-125 Burchett, Bradley T., A04-056 Guo, Zheng, A04-137 Lempert, G., A04-042, A04-043 Olguin, Daniella M., A04-094 Burkhalter, John, A04-090 Gupta, Amar, A04-003 Leveson, Nancy G., A64-073 Park, Seung-O, A04-097 Burkhardt, Holger, A04-100 Gusarov, A., A04-047 Levin, D. A., A04-075 Park, Soo Hyung, A04-099, A04-138 Byrnes, Dennis V., A04-079 Haftka, Raphael T., A04-059 Li, Chun-Dong, A04-046 Paté-Cornell, M. Elisabeth, A04-005, ‘ampbell, Eric T., AO4-105 Hall, Christopher D., A04-124 Lifshitz, Y., A04-042, A04-043 A04-006, A04-010 ‘ampbell, Jennie, A04-069 Hara, Hirohisa, AO4-113 Lightsey, E. Glenn, A04-081 Patel, Mehul P., A04-055 “apitelli, M., AO4-034 Hargus, William A., AO4-131, A04-132 Liou, William W., A04-117 Paterna, D., A04-126 ‘appelli, Mark A., AO4-131, A04-132 Harris, Stewart, A04-139 Liu, Jun, AO4-137 Patil, M. M., AO04-092 “asali, Daniele, A04-086 Hartfield, Roy J., A04-090 Loh, Yin-Chung, A04-035 Pereira, Alexandre, A04-106 ‘hamberlain, Adam, A04-074 Hassan, Hassan A., AO4-118 Longuski, James, A04-104 Petropoulos, Anastassios E., A04-103 ‘hen, D. T., A04-128 Hastings, Daniel, A04-008 Longuski, James L., A04-079 Pfaff, R. F., A04-063, A04-064, ‘hen, Roger R., A04-020, A04-024 Hastings, Daniel E., A04-001, A04-002, Longuski, James M., A04-103, A04-066 Pwelheaeaae e ? ‘ h en, R. R., AO4-022 404-011, A04-012 A04-130 Pfaff. Robert F., A04-068 ry “hernouss, S. A., A04-085 Heiner, Nicholas C., A04-094 Lou, Michael, A04-070 Pippin, H. Gary, A04-037 Chokani, Ndaona, A04-052 Herbertz, Armin, A04-100 Lourel, 1., A04-095 Platov, Y. V., AO04-085 Cho, Mengu, A04-111 He, Shi-yu, A04-046 Lynch, K. A., A04-063, A04-064 Podgorny, I. M., A04-064 Chutter, M., A04-065 He, Shiyu, A04-048 Lynch, Kristina A., A04-065 Poteet, Carl C., A04-020, A04-021, Coverstone, Victoria L., A04-080 Hiraki, Koujyu, AO4-121 Lyons, Daniel T., A04-104 A04-026 Cross, Paul, A04-019 Hoffmann, Klaus A., A04-076 Machida, Kazuo, A04-015 Poteet, C. C., A04-022 Crunkleton, Daniel, A04-074 Honggqing, He, A04-014 Madsen, Jared, A04-081 Qu, Zhang-hua, A04-137 Dachwald, Bernd, A04-091 Hong. Seung-Kyu, A04-097 Main, J. A., A04-069 Rajan, S.C., A04-123 Daniel, William J. T., A04-078 Horvath, Thomas J., A04-031, Mains, Deanna L., A04-105 Ramachandran, Prabhu, A04-123 de Groh, Kim K., A04-039, A04-045 A04-032, A04-094 Maji, Arup, A04-072 Randolph, Thomas, A04-108 Delamere, P. A., A04-063, A04-066 Hsia, Lih-Min, A04-070 Mandal, J. C., A04-092 Riabov, Vladimir V., A04-093 Delamere, Peter A., A04-068 Hsu, Sun-Yuen, A04-021 Manning, Melissa L., A04-052 Rice, Carl J., A04-110 DeMagistris, Michael, A04-067 Huang, John, A04-070 Marcum, David L., A04-028 Robinson, M. J., A04-053 Demko, Rikako, A04-039 Hughes, Gareth, A04-016 Marker, D. K., A04-071 Rogers, Bridget, A04-074 de Weck, Olivier L., A04-061 Hughes, P. C., A04-038 Markgraf, Markus, A04-082 Ross, Adam M., A04-002 Dietiker, Jean-Francois, A04-076 Hwu, Shian U., A04-035 Marschall, Jochen, A04-074 Roussel. Jean-FranAois, A04-106 Diller, Nathan P., A04-002 Hymer, T. C., A04-027, A04-122 Martinez-Sanchez, Manuel, A04-108 Sakamoto, Keishi, A04-017 Dinguirard, M., A04-042 Imai, Tsuyoshi, A04-017 Martin, Morgana, A04-045 Sakao, Taro, A04-113 Dogra, V. K., A04-063 Inatani, Yoshifumi, A04-121 Matsumoto, Hirahisu, AO4-112 Sandfry, Ralph A., A04-124 Donahue, Benjamin B., A04-033 Infed, F., A04-119 Matsumoto, Toshiaki, A04-111 Sankaran, Sankara N., A04-025 Dorsey, John T., A04-020 Inoue, Masao, A04-113 Matsumoto, Yoichiro, A04-051 Sankar, Bhavani V., A04-059 Dorsey, |. T., A04-022 Iskanderova, Z., A04-038 McConaghy, T. Troy, A04-079 Santhakumar, S., A04-123 Doyle, D., A04-047 Jacobs, P. A., A04-095 McInnes, Colin R., A04-016 Saraf, A., A04-128 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX Savino, R., A04-126 Stenbaek-Nielsen, H. C., A04-063, Tsutoi, Noboyuki, A04-051 Wooten, Mickey, A04-139 Scheeres, D. J., A04-088 A04-066 Tsuchiya, Takeshi, A04-101 Wurster, Kathryn E., A04-020 Schilling, John H., A04-131, A04-132 Stepanov, Vladimir F., A04-044 Tsuneta, Saku, A04-113 Wurster, K. E., A04-022 Schmidt, 1. H., AO4-022 Stoyanov, B. J., A04-063 Vayner, Boris, A04-133, A04-134 Xianwei, Han, A04-014 Schutz, Bob E., A04-129 Strauss, Daniel, A04-098 Venkataraman, Satchi, A04-059 Schweighart, Samuel A., A04-084 Subramanian, B., A04-107 Viel-Inguimbert, V., A04-042 Xiao, Xudong, A04-118 Sedwick, Raymond J., A04-084 Sullivan, James D., AO4-112 Vighnesam, N. V., A04-107 Xu, Shuxuan, A04-117 Seshasai, Satwiksai, A04-003 Swaminathan, P. K., A04-063 Volchek, A., A04-047 Yamaguchi, Hiroki, A04-051 Sham, Catherine C., A04-035 Swaminathan, S., A04-092 Walker, Quentin E., A04-131, A04-132 Yang, De-zhuang, A04-046 Sharma, Deepti N., A04-088 Tagawa, M., A04-041 Wallace, Terryl A., A04-025 Yang. Shi-qin, A04-046 Shimizu, Toshifumi, A04-113 Tagawa, Masahito, A04-050 Walton, Myles A., A04-008 Yang, Shigin, A04-048 Shin, Won-Ho, A04-030 Takahashi, Koji, A04-017 Ward, David K., A04-136 Shirin, Zahida, A04-139 Takahashi, Masato, A04-111 Warmkessel, Joyce M., A04-001, Yanushevsky, Rafael, A04-062 Sibthorpe, Anthony, A94-019 Tennyson, R. C., A04-038 A04-002, A04-007 Yasaka, T., AO4-127 Silverberg, Larry, A04-135 Thunnisen, Daniel P., A04-009 Wasistho, B., A04-120 Yokota, Kumiko, A04-041 Sippel, Martin, A04-100 Tilmann, Carl P., A04-055 Weigel, Annalisa L., A04-011, A04-012 Yoshida, Tsuyoshi, A04-113 Smith, Casey, A04-139 Tlebaev, Kairat B., A04-044 Weilmuenster, K. James, A04-032 Zetzer, J. 1., A04-064, A04-065, Smith, Suzanne Weaver, A04-069 Torbert, R. B., A04-065 Weinacht, Paul, A04-029 A04-066 Snyder, Aaron, A04-039, A04-040 Toyoda, Kazuhiro, A04-111 Wilkes, J. M., A04-071 Zetzer, Julius 1., A04-068 Sobyanin, D. B., A04-064 Trask, Aaron J., A04-080 Williams, Paul, A04-036, Sonney, Anatta, A04-107 Trivailo, Pavel, A04-077 A04-077, A04-116 Zhang, Linxin, A04-048 Springmann, Philip N., A04-061 Tsai, C. Y., A04-053 Wolf, Suzanne L. B., A04-037 Zhu, Huadong, A04-059 Starin, Scott, A04-136 Tsai, Jih-Run, A04-013 Wollack, Edward J., A04-136 Ziebart, Marek, A04-019, A04-109 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX Chronological Index A04-001 New Methods for Rapid Architecture Selection and A04-016 Small-Body Encounters Using Solar Sail Propulsion. Conceptual Design. Hugh L. McManus, Daniel E. Hastings, and Gareth Hughes and Colin R. McInnes, University of Glasgow, Joyce M. Warmkessel, Massachusetts Institute of Technology (41, Great Britain (41, 1, p. 140) Article 1, p. 10) Article A04-017 Propulsive Impulse Measurement of a Microwave- A04-002 Multi-Attribute Tradespace Exploration as Front End Boosted Vehicle in the Atmosphere. Tatsuo Nakagawa, Yorichika for Effective Space System Design. Adam M. Ross, Daniel E. Mihara, and Kimiya Komurasaki, University of Tokyo, Japan; Koji Hastings, and Joyce M. Warmkessel, Massachusetts Institute of Takahashi, Keishi Sakamoto, and Tsuyoshi Imai, Japan Atomic Technology, and Nathan P. Diller, United States Air Force, Energy Research Institute, Japan (41, 1, p. 151) Technical Note Sheppard Air Force Base (41, 1, p. 20) Article A04-018 Optimal Ascent Trajectory for Efficient Air Launch A04-003 Knowledge-Based Approach to Facilitate Engineering into Orbit. Frederick W. Boltz, Launch Vehicle Technology (41, 1, Design. Satwiksai Seshasai, /BM; and Amar Gupta, Massachusetts p. 153) Technical Note Institute of Technology (41, |, p. 29) Article A04-019 Oblate Earth Eclipse State Algorithm for Low-Earth- A04-004 Multi-Objective, Multidisciplinary Design Orbiting Satellites. Sima Adhya, Anthony Sibthorpe, Marek Optimization Methodology for Distributed Satellite Systems. Ziebart, and Paul Cross, University College London, Great Britain Cyrus D. Jilla and David W. Miller, Massachusetts Institute of (41, 1, p. 157) Technical Note Technology (41, 1, p. 39) Article A04-020 Metallic Thermal Protection System Requirements, A04-005 Risk Chair for Concurrent Design Engineering: Environments, and Integrated Concepts. John T. Dorsey, NASA Satellite Swarm Illustration. James L. Benjamin and M. E. Paté- Langley Research Center, Roger R. Chen, Lockheed Martin Space Cornell, Stanford University (41, 1, p. 51) Article Operations; Kathryn E. Wurster and Carl C. Poteet, NASA Langley Research Center (41, 2, p. 162) Article A04-006 Modeling the Effects of Dispersion of Design Teams on System Failure Risk. Russ Garber and M. Elisabeth Paté- A04-021 Preliminary Thermal-Mechanical Sizing of a Metallic Cornell, Stanford University (41, 1, p. 60) Article Thermal Protection System. Carl C. Poteet, NASA Langley Research Center; Hasan Abu-Khajeel and Sun-Yuen Hsu, Lockheed A04-007 Creating Advanced Architecture for Space Systems: Martin Space Operations (41, 2, p. 173) Article Emergent Lessons from New Processes. Hugh McManus, Massachusetts Institute of Technology, and Joyce M. Warmkessel, A04-022 Development of Advanced Metallic-Thermal- (41, 1, p. 69) Article Protection System Prototype Hardware. M. L. Blosser, C. C. Poteet, R. R. Chen, J. T. Dorsey, I. H. Schmidt, R. K. Bird, and A04-008 Applications of Uncertainty Analysis Applied to K. E. Wurster, NASA Langley Research Center (41, 2, p. 183) Architecture Selection of Satellite Systems. Myles A. Walton and Article Daniel Hastings, Massachusetts Institute of Technology (41, 1, p. 75) Article A04-023 Fundamental Modeling and Thermal Performance Issues for Metallic Thermal Protection System Concept. Max L. A04-009 Method for Determining Margins in Conceptual Blosser, NASA Langley Research Center (41, 2, p. 195) Article Design. Daniel P. Thunnisen, California Institute of Technology (41, 1, p. 85) Article A04-024 Metallic Thermal-Protection-System Panel Flutter Study. Roger R. Chen and Max L. Blosser, NASA Langley Research A04-010 Bayesian Analysis of Launch Vehicle Success Rates. Center (41, 2, p. 207) Article Seth D. Guikema and M. E. Paté-Cornell, Stanford University (41, 1, p. 93) Article A04-025 Development of Protective Coatings for High- Temperature Metallic Materials. R. K. Bird and Terryl A. A04-011 Evaluating the Cost and Risk Impacts of Launch Wallace, NASA Langley Research Center; and Sankara N. Choices. Annalisa L. Weigel and Daniel E. Hastings, Sankaran, Lockheed Martin Space Operations (41, 2, p. 213) Massachusetts Institute of Technology (41, 1, p. 103) Article Article A04-012 Measuring the Value of Designing for Uncertain A04-026 Improving Metallic Thermal Protection System Future Downward Budget Instabilities. Annalisa L. Weigel and Hypervelocity Impact Resistance Through Numerical Daniel E. Hastings, Massachusetts Institute of Technology (41, Simulations. Carl C. Poteet and Max L. Blosser, NASA Langley 1, p. L11) Article Research Center (41, 2, p. 221) Article A04-013 Overview of Satellite Thermal Analytical Model. Jih- A04-027 2002 Version of the Aeroprediction Code (AP02). F. G. Run Tsai, National Space Program Office, Taiwan (ROC) (41, Moore, Aeroprediction, Inc.; and T. C. Hymer, U.S. Naval Surface 1, p. 120) Article Warfare Center (41, 2, p. 232) Article A04-014 Resonant and Ground Experimental Study on A04-028 Numerical Simulation of a Spinning Missile with Microwave Plasma Thruster. Yang Juan, He Hongging, Mao Dithering Canards Using Unstructured Grids. Eric L. Blades Genwang, and Han Xianwei, Northwestern Polytechnical and David L. Marcum, Mississippi State University (41, 2, p. 248) University, China (PRC) (41, 1, p. 126) Article Article A04-015 Space Test of Sensor-Fused Telerobotics for High- A04-029 Projectile Performance, Stability, and Free-Flight Precision Tasks. Kazuo Machida, University of Tokyo, Japan Motion Prediction Using Computational Fluid Dynamics. Paul (41, 1, p. 132) Article Weinacht, U.S. Army Research Laboratory (41, 2, p. 257) Article J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX 1083 A04-030 Nonlinear Aeroelastic Analysis of a Deployable A04-042 Atomic Oxygen Durability of a Silicone Paint: A Missile Control Fin. Jae-Sung Bae, Virginia Polytechnic Institute Comparison Between Two Simulation Methods. I. Gouzman, E. and State University, Dae-Kwan Kim, Won-Ho Shin, and In Lee, Grossman, G. Lempert, and Y. Noter, Soreg NRC; Y. Lifshitz, City Korea Advanced Institute of Science and Technology, South Korea; University of Hong Kong; V. Viel-Inguimbert and M. Dinguirard, and Seung-Ho Kim, Korea Aerospace Industry, South Korea (41, 2, ONERA (Al, 3, p. 350) Article p. 264) Article A04-043 Assessment of Atomic-Oxygen Flux in Low-Earth- A04-031 X-38 Experimental Aerothermodynamics. Thomas J. Orbit Ground Simulation Facilities. E. Grossman, 1. Gouzman, Horvath, Scott A. Berry, and N. R. Merski, NASA Langley Research G. Lempert, and Y. Noter, Soreg NRC; and Y. Lifshitz, City Center; and Steve M. Fitzgerald, NASA Johnson Space Center (41, University of Hong Kong (41, 3, p. 356) Article 2, p. 272) Article A04-044 Determination of Dose Rate Effects in Polymers A04-032 X-38 Experimental Aeroheating at Mach 10. Scott A. Irradiated in Vacuum. Boris A. Briskman, Edward R. Klinshpont, Berry, Thomas J. Horvath, K. J. Weilmuenster, Stephen J. Alter, and and Vladimir F. Stepanov, Karpov Institute of Physical Chemistry: N. R. Merski Jr., NASA Langley Research Center (41, 2, p. 293) and Kairat B. Tlebaev, /nstitute of Physics and Technology (41, 3, p. 360) Article Article A04-045 Thermal Contributions to the Degradation of Ground A04-033 Beating the Rocket Equation: Air Launch with Laboratory and Space-Irradiated Teflon. Kim K. de Groh, NASA Advanced Chemical Propulsion. Benjamin B. Donahue, Boeing John H. Glenn Research Center at Lewis Field; and Morgana Phantom Works (41, 2, p. 302) Article Martin, Ohio Aerospace Institute (41, 3, p. 366) Article A04-034 Surface Recombination Coefficients and Boundary- A04-046 Degradation of Teflon Film Under Radiation of Layer Hypersonic-Flow Calculations on Different Surfaces. I. Protons and Electrons. Chun-Dong Li, De-zhuang Yang, Shi-yu Armenise, Istituto di Metodologie Inorganiche e dei Plasmi, He, and Shi-qin Yang, Harbin Institute of Technology (41, 3, p. 373) Consiglio Nazionale delle Ricerche, Italy; M. Barbato, Scuola Article Universitaria Professionale della Svizera Italiana,, Italy; M. Capitelli, Bari University and Istituto di Metodologie Inorganiche e A04-047 Methodology for Prediction of Near-Earth Space dei Plasmi, Italy; and C. Gorse, Bari University and Istituto di Radiation Effects on Optical Glasses. A. Gusarov, SCK-CEN Metodologie Inorganiche e dei Plasmi, Italy (41, 2, p. 310) Belgian Nuclear Research Center, D. Doyle, ESA: M. Fruit, Technical Note Astrium, and A. Volchek, Research and Technological Institute of Optical Material Science (41, 3, p. 377) Article A04-035 International Space Station Ku-Band Communications Antenna Blockage Analysis. Shian U. Hwu and A04-048 Study on Damage Effects of Methyl Silicone Rubber Yin-Chung Loh, Lockheed Martin Space Operations; Quin D. Kroll Induced by Proton Radiation. Linxin Zhang, Hongbin Geng, and Catherine C. Sham, NASA Johnson Space Center (41, 2, p. 313) Shigin Yang, and Shiyu He, Harbin Institute of Technology (A1, 3, Technical Note p. 381) Article A04-049 Simulation of Outgassing Processes in Spacecraft A04-036 Optimal Control of Tethered Planetary Capture Coatings Induced by Thermal Vacuum Influence. R. H. Missions. Paul Williams, Royal Melbourne Institute of Technology, Australia (41, 2, p. 315) Technical Note Kassanchine, Joint-Stock Company “Kompozit™; A. NV. Grigorevskiy and A. N. Galygin, Joint Stock Company “Kompozit” A04-037 Analysis of Metallized Teflon™ Thin-Film Materials (41, 3, p. 384) Article Performance on Satellites. H. Gary Pippin, Eugene Normand, and A04-050 Energy Accommodation in Hyperthermal Gas- Suzanne L. Wolf, Boeing Phantom Works; and Rachel Kamenetzky, Surface Collisions: Aerobraking in Planetary Atmospheres. NASA Marshall Space Center (41, 3, p. 322) Article Timothy K. Minton, Montana State University; Masahito Tagawa, A04-038 Enhancement of Space Durability of Materials and Kobe University: and Gilbert M. Nathanson, University of External Components Through Surface Modification. Y. Wisconsin (41, 3, p. 389) Article Gudimenko, R. Ng, J. Kleiman, and Z. Iskanderova, /ntegrity A04-051 Direct Simulation Monte Carlo Method on Rarefied Testing Laboratory, Inc.; D. Milligan, MacDonald Detwiler Space Hypersonic Gas Flow Around Flat Plates. Noboyuki Tsuboi, and Advanced Robotics, Ltd.; R. C. Tennyson and P. C. Hughes, Institute of Space and Astronautical Science; Hiroki Yamaguchi and University of Toronto (41, 3, p. 326) Article Yoichiro Matsumoto, University of Tokyo (41, 3, p. 397) Article A04-039 Atomic-Oxygen Undercutting of Protected Polymers A04-052 Computational Evaluation of Quiet Tunnel in Low Earth Orbit. Bruce A. Banks, Aaron Snyder, Sharon K. Hypersonic Boundary-Layer Stability Experiments. Melissa L. Miller, and Kim K. de Groh, NASA John H. Glenn Research Center Manning and Ndaona Chokani, North Carolina State University at Lewis Field; and Rikako Demko, Cleveland State University (41, 3, p. 406) Article (41, 3, p. 335) Article A04-053 Three-Component Force Measurements on a Large A04-040 Fast Three-Dimensional Modeling of Atomic Oxygen Scramjet in a Shock Tunnel. M. J. Robinson and D. J. Mee, Undercutting of Protected Polymers. Aaron Snyder and Bruce A. University of Queensland; C. Y. Tsai and R. J. Bakos, Allied Banks, NASA John H. Glenn Research Center at Lewis Field (41, 3, Aerospace Industries (41, 3, p. 416) Article p. 340) Article A04-054 Numerical Simulation of Rolling Airframes Using a A04-041 Synergistic Study on Atomic Oxygen-Induced Erosion Multilevel Cartesian Method. Scott M. Murman, ELOURKET: of Polyethylene with Vacuum Ultraviolet. M. Tagawa, Kumiko Michael J. Aftosmis, NASA Ames Research Center; and Marsha J. Yokota, and Nobuo Ohmae, Kobe University (41, 3, p. 345) Article Berger, Courant Institute (41, 3, p. 426) Article 1984 J. SPACECRAFT, VOL. 41, NO. 6: 2004 INDEX A04-055 Closed-Loop Missile Yaw Control via Manipulation of A04-066 Dynamics of the Active Plasma Experiment North Forebody Flow Asymmetrics. Mehul P. Patel, Orbital Research Star Artificial Plasma Jet. P. A. Delamere, University of Inc.; Carl P. Tilmann, U.S. Air Force Research Laboratory, Colorado; H. C. Stenbaek-Nielsen, University of Alaska Fairbanks; R. F. Pfaff, NASA Goddard Space Flight Center; R. E. Erlandson Wright-Patterson Air Force Base, and T. T. Ng, University of and C. I. Meng, Johns Hopkins University, Applied Physics Toledo (41, 3, p. 436) Article Laboratory; J. 1. Zetzer, Y. Kiselev, and B. G. Gavrilov, /nstitutfeo r A04-056 Fuzzy Logic Trajectory Design and Guidance for Dynamics of Geospheres (41, 4, p. 503) Article Terminal Area Energy Management. Bradley T. Burchett, Rose- A04-067 Three-Dimensional Magnetohydrodynamic Modeling Hulman Institute of Technology (41, 3, p. 444) Article of Plasma Jets in the North Star Space Experiment. Nikolaos A. Gatsonis and Michael DeMagistris, Worcester Polytechnic Institute; A04-057 Turbulence Structure of a Compressible Base Flow and Robert E. Erlandson, Johns Hopkins University, Applied with a Central Bleed Jet. C. J. Bourdon and J. C. Dutton, Physics Laboratory (41, 4, p. 509) Article University of Illinois at Urbana-Champaign (41, 3, p. 451) Article A04-068 Electric Field, Magnetic Field, and Density A04-058 Geostationary Orbit Transfers Using Solar Electric Measurements on the Active Plasma Experiment Sounding Propulsion with Specific Impulse Modulation. C. A. Kluever, Rocket. Robert F. Pfaff, Henry T. Freudenreich, and Scott Bounds, University of Missouri—Columbia (41, 3, p. 461) Article NASA Goddard Space Flight Center, Peter A. Delamere, University of Colorado; R. E. Erlandson and Cheng I. Meng, Johns Hopkins A04-059 Minimum Mass Design of Insulation Made of University, Applied Physics Laboratory; Julius |. Zetzer and Boris Functionally Graded Material. Huadong Zhu, Bhavani V. Sankar, G. Gavrilov, Institute of Geospheres Dynamics (41, 4, p. 521) and Raphael T. Haftka, University of Florida; Satchi Venkataraman, Article San Diego State University; and Max L. Blosser, NASA Langley A04-069 Staged Microgravity Deployment of a Pressurizing Research Center (41, 3, p. 467) Technical Note based on AIAA Scale-Model Spacecraft. Jennie Campbell, Suzanne W. Smith, J. Paper 2002-1425 A. Main, and Justin Kearns, University of Kentucky (41, 4, p. 534) Article A04-060 Multiblock Compressible Navier-Stokes Flow Solver Applied to Complex Launch Vehicles. Abdollah Arabshahi and J. A04-079 Inflatable Structure for a Three-Meter Reflectarray Mark Janus, Mississippi State University (41, 3, p. 469) Technical Antenna. Houfei Fang, Michael Lou, and John Huang, Jet Propulsion Laboratory; Lih-Min Hsia and Grigor Kerdanyan, Note based on AIAA Paper 99-3378 California State University at Los Angeles (41, 4, p. 543) Article A04-061 Parametric Scaling Model for Nongeosynchronous A04-071 Shape Achievement of Optical Membrane Communications Satellites. Philip N. Springmann and Olivier L. MirrorsUsing Coating/Substrate Intrinsic Stresses. J.T. Ash and de Weck, Massachussetts Institute of Technology (41, 3, p. 472) C. H. Jenkins, South Dakota School of Mines and Technology; Technical Note based on AIAA Paper 2003-2310 D. K. Marker and J. M. Wilkes, U.S. Air Force Research Laboratory (41, 4, p. 551) Article A04-062 Analysis of Optimal Weaving Frequency of Maneuvering Targets. Rafae! Yanushevsky, Technology Service A04-072 Shape Correction of Inflatable Membranes by Corporation (41, 3, p. 477) Technical Note Rigidization and Actuation. Arup Maji, U.S. Air Force Research Laboratory; Patrick Montemerlo, University of New Mexico; and A04-063 North Star Plasma-Jet Space Experiment. R. E. Tang-tat Ng, U.S. Air Force Research Laboratory (41, 4, p. 558) Erlandson, P. K. Swaminathan, C. K. Kumar, V. K. Dogra, and B. J. Article Stoyanov, Johns Hopkins University, Applied Physics Laboratory; A04-073 Role of Software in Spacecraft Accidents. Nancy G. B. G. Gavrilov, Y. Kiselev, and J. I. Ketzer, Institutfeo r Dynamics Leveson, Massachusetts Institute of Technology (41, 4, p. 564) of Geospheres,; H. C. Stenbaek-Nielsen, University of Article Alaska/Geophysical Institute; K. A. Lynch, Dartmouth College: A04-074 Catalytic Atom Recombination on ZrB2/SiC and R. F. Pfaff, NASA Goddard Space Flight Center; P. A. Delamere, HfB2/SiC Ultrahigh-Temperature Ceramic Composites. Jochen University of Colorado; S. Bounds, University of lowa; and N. A. Marschall, SRI International; Adam Chamberlain, University of Gatsonis, Worcester Polytechnic Instituie (41, 4, p. 483) Missouri—Rolla; Daniel Crunkleton and Bridget Rogers, Vanderbilt Article University (41, 4, p. 576) Article A04-064 North Star Plasma-Jet Experiment Particles and A04-075 Modeling of Chemically Reacting Flowsfrom a Side Electric and Magnetic Field Measurements. B. G. Gavrilov, I. M. Jet at High Altitudes. S. F. Gimelshein, D. A. Levin, and A. A. Podgorny, D. B. Sobyanin, and J. 1. Zetzer, Russian Academy of Alexeenko, Pennsylvania State University (41, 4, p. 582) Article Sciences; R. E. Erlandson and C. I. Meng, Johns Hopkins based on AIAA Paper 2002-0212 University, Applied Physics Laboratory; R. F. Pfaff, NASA Goddard A04-076 Numerical Simulation of Magnetohydrodynamic Space Flight Center; and K. A. Lynch, New Hampshire University Flows. Jean-Francois Dietiker and Klaus A. Hoffmann, Wichita (41, 4, p. 490) Article State University (41, 4, p. 592) Article A04-065 Active Plasma Experiment: North Star Particle Data. A04-077 Tethered Planetary Capture Maneuvers. Paul Kristina A. Lynch, Dartmouth College; R. B. Torbert and M. Williams, Chris Blanksby, and Pavel Trivailo, Royal Melbourne Chutter, University of New Hampshire; R. E. Erlandson and C. I. Institute of Technology, Australia (41, 4, p. 603) Article Meng, Johns Hopkins University, Applied Physics Laboratory; J. 1. A04-078 Aerogravity-Assist Maneuvering of a Tethered Zetzer, B. G. Gavrilov, and Y. Kiselev, Russian Academy of Satellite System. Michael Jokic and William J. Daniel, University Sciences (41, 4, p. 496) Article of Queensland, Australia (41, 4, p. 614) Article