Table Of Content

JOURNAL OF SPACECRAFT AND ROCKETS Vol. 36, No. 6, November—December 1999 1999 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 926—930, each technical paper is listed under a maximum oft hree appropriate headings. Note the number in boldface type following each paper title, and use that number to locate the paper in the Chronological Index. The Author Index, page 931, lists all authors associated with a given technical paper. The !ocating numbers are identical to those in the Subject Index. The Chronological Index, pages 932-936, lists all papers by their unique code 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, as well as the ISBN number if the paper was published in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 1999, that paper also will appear in the Chronological Index. Authors of Comments also are listed in the Author Index. Subject Index Aircraft Technology, Conventional, Structural Materials Boundary-Layer Stability and Transition STOL/VTOL In Situ Erosion Study of Kapton™ Using a Novel Flight Data for Boundary-Layer Transition at Aerodynamics Hyperthermal Oxygen Atom Source Hypersonic and Supersonic Speeds A99-007 A99-001 Computational Simulation Improvements of Su- personic High-Angle-of-Attack Missile Flows Testing, Flight and Ground Computational Fluid Dynamics A 99-005 Numerical Study of Hypersonic Rarefied-Gas Plasma Electron Density Measurement Around Erratum on “Aerodynamic Interference for Hy- Flows About a Torus Hypersonic Flight Experiment Vehicle personic Missiles at Low Angle of Attack” A99-035 A99-072 A98-117 Aerodynamics of the Mars Microprobe Entry Hypersonic Flowfield Analysis of X-33 Model Computational Aerothermodynamic Design Is- Vehicles A99-047 with the Electric Discharge Method sues for Hypersonic Vehicles Aecrothermal Heating Predictions for Mars A99-103 A99-002 Microprobe 499-049 Aerothermodynamic Environment for a Generic Aerodynamics of the Stardust Sample Return Missile A99-003 Capsule A99-052 Energy Statistical Comparison of Computed Surface Acrodynamics of a Spinning Cylinder in Rar- Pressure Predictions A99-018 efied Gas Flows 499-059 Rotating Machinery Numerical Investigation of Shock/Vortex Inter- Engineering Intermediate-, and High-Lev- action in Hypersonic Thermochemical Non- el Aerodynamic Prediction Methods and Aerodynamics of a Spinning Cylinder in Rar- equilibrium Flow A99-028 Applications 499-079 efied Gas Flows A99-059 Base Flow Predictions for a Lightsat Launcher at High-Angle-of-Attack Aerodynamics of a Mis Supersonic Speeds A99-029 sile Geometry at Low Speed Prediction and Validation of Mars Pathfinder Fluid Dynamics Hypersonic Aerodynamic Database AW-100 Hypersonic Flowfield Analysis of X-33 Model A99-044 with the Electric Disc harge Method Boundary Layers and Heat Transfer—Laminar Viscous Multiblock Simulations of Axisymmet- A99-103 ric Launch Vehicle Flows A99-060 Euler and Navier-Stokes Solutions for Missiles X-34 Experimental Aeroheating at Mach 6 Plasma Electron Density Measurement Around at High Angles of Attack 499-111 and 10 A99-021 Hypersonic Flight Experiment Vehicle Engineering Aerothermal Analysis for X-34 A99-072 Aeroelasticity and Aeroservoelasticity Thermal Protection System Design Asymmetric Divert Jet Performance of a Super- 499-026 sonic Missile: Computational and Experimen- High-Supersonic/Hypersonic Flutter of Prismat- Three-Dimensional Shock/Boundary-Layer In- tal Comparisons A99-080 ic Composite Plate/Shell Panels teraction Between a Rocket and a Booster Transition Effects on Heating in the Wake of a A99-097 A99-087 Blunt Body A99-085 Analysis of Linear Aerospike Plume-Induced X- Aerothermodynamic Analyses of Hypersonic, Aerospace Plane 33 Base-Heating Environment Blunt-Body Flows A99-119 A99-102 Simple Analytical Model for Parametric Studies Euler and Navier-Stokes Solutions for Missiles of Hypersonic Waveriders 499-064 Boundary Layers and Heat Transfer— at High Angles of Attack Turbulent Hypersonic Flowfield Analysis of X-33 Model A99-111 with the Electric Discharge Method Aerothermodynamic Analyses of Hypersonic, Statistical Comparison of Computed Surface A99-103 Blunt-Body Flows A99-119 Pressure Predictions A99-018 Simulation Engineering Aerothermal Analysis for X-34 Hypersonic Flow Thermal Protection System Design Automatic Landing Flight Experiment Flight A99-026 Erratum on “Aerodynamic Interference for Hy- Simulation Analysis and Flight Testing Effects of Shock Wave Impingement on Super- personic Missiles at Low Angle of Attack” 499-069 sonic Film Cooling A99-077 A98-117 926 JOURNAL OF SPACECRAFT AND ROCKETS Vol. 36, No. 6, November—December 1999 1999 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 926—930, each technical paper is listed under a maximum oft hree appropriate headings. Note the number in boldface type following each paper title, and use that number to locate the paper in the Chronological Index. The Author Index, page 931, lists all authors associated with a given technical paper. The !ocating numbers are identical to those in the Subject Index. The Chronological Index, pages 932-936, lists all papers by their unique code 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, as well as the ISBN number if the paper was published in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they refer. If the paper to which they refer was published prior to 1999, that paper also will appear in the Chronological Index. Authors of Comments also are listed in the Author Index. Subject Index Aircraft Technology, Conventional, Structural Materials Boundary-Layer Stability and Transition STOL/VTOL In Situ Erosion Study of Kapton™ Using a Novel Flight Data for Boundary-Layer Transition at Aerodynamics Hyperthermal Oxygen Atom Source Hypersonic and Supersonic Speeds A99-007 A99-001 Computational Simulation Improvements of Su- personic High-Angle-of-Attack Missile Flows Testing, Flight and Ground Computational Fluid Dynamics A 99-005 Numerical Study of Hypersonic Rarefied-Gas Plasma Electron Density Measurement Around Erratum on “Aerodynamic Interference for Hy- Flows About a Torus Hypersonic Flight Experiment Vehicle personic Missiles at Low Angle of Attack” A99-035 A99-072 A98-117 Aerodynamics of the Mars Microprobe Entry Hypersonic Flowfield Analysis of X-33 Model Computational Aerothermodynamic Design Is- Vehicles A99-047 with the Electric Discharge Method sues for Hypersonic Vehicles Aecrothermal Heating Predictions for Mars A99-103 A99-002 Microprobe 499-049 Aerothermodynamic Environment for a Generic Aerodynamics of the Stardust Sample Return Missile A99-003 Capsule A99-052 Energy Statistical Comparison of Computed Surface Acrodynamics of a Spinning Cylinder in Rar- Pressure Predictions A99-018 efied Gas Flows 499-059 Rotating Machinery Numerical Investigation of Shock/Vortex Inter- Engineering Intermediate-, and High-Lev- action in Hypersonic Thermochemical Non- el Aerodynamic Prediction Methods and Aerodynamics of a Spinning Cylinder in Rar- equilibrium Flow A99-028 Applications 499-079 efied Gas Flows A99-059 Base Flow Predictions for a Lightsat Launcher at High-Angle-of-Attack Aerodynamics of a Mis Supersonic Speeds A99-029 sile Geometry at Low Speed Prediction and Validation of Mars Pathfinder Fluid Dynamics Hypersonic Aerodynamic Database AW-100 Hypersonic Flowfield Analysis of X-33 Model A99-044 with the Electric Disc harge Method Boundary Layers and Heat Transfer—Laminar Viscous Multiblock Simulations of Axisymmet- A99-103 ric Launch Vehicle Flows A99-060 Euler and Navier-Stokes Solutions for Missiles X-34 Experimental Aeroheating at Mach 6 Plasma Electron Density Measurement Around at High Angles of Attack 499-111 and 10 A99-021 Hypersonic Flight Experiment Vehicle Engineering Aerothermal Analysis for X-34 A99-072 Aeroelasticity and Aeroservoelasticity Thermal Protection System Design Asymmetric Divert Jet Performance of a Super- 499-026 sonic Missile: Computational and Experimen- High-Supersonic/Hypersonic Flutter of Prismat- Three-Dimensional Shock/Boundary-Layer In- tal Comparisons A99-080 ic Composite Plate/Shell Panels teraction Between a Rocket and a Booster Transition Effects on Heating in the Wake of a A99-097 A99-087 Blunt Body A99-085 Analysis of Linear Aerospike Plume-Induced X- Aerothermodynamic Analyses of Hypersonic, Aerospace Plane 33 Base-Heating Environment Blunt-Body Flows A99-119 A99-102 Simple Analytical Model for Parametric Studies Euler and Navier-Stokes Solutions for Missiles of Hypersonic Waveriders 499-064 Boundary Layers and Heat Transfer— at High Angles of Attack Turbulent Hypersonic Flowfield Analysis of X-33 Model A99-111 with the Electric Discharge Method Aerothermodynamic Analyses of Hypersonic, Statistical Comparison of Computed Surface A99-103 Blunt-Body Flows A99-119 Pressure Predictions A99-018 Simulation Engineering Aerothermal Analysis for X-34 Hypersonic Flow Thermal Protection System Design Automatic Landing Flight Experiment Flight A99-026 Erratum on “Aerodynamic Interference for Hy- Simulation Analysis and Flight Testing Effects of Shock Wave Impingement on Super- personic Missiles at Low Angle of Attack” 499-069 sonic Film Cooling A99-077 A98-117 926 927 J. SPACECRAFT, VOL. 36, NO. 6: 1999 INDEX Flight Data for Boundary-Layer Transition at Rarefied Flows Navigation Flight Operations for Mars Pathfinder Hypersonic and Supersonic Speeds A9-041 A99-001 Numerical Study of Hypersonic Rarefied-Gas Low-Thrust Trajectory Optimization Based on Computational Aerothermodynamic Design Is- Flows About a Torus A99-035 Epoch Eccentric Longitude Formulation sues for Hypersonic Vehicles Rarefied Aerothermodynamic Predictions for A99-068 A99-002 Mars Global Surveyor A99-038 X-34 Experimental Aeroheating at Mach 6 Mars Pathfinder Rarefied Aerodynamics: Com- Computer Science and i0 A99-021 putations and Measurements Computational Aeroheating Predictions for A99-040 Direct Simulation Monte Carlo Calculations of X-34 A99-022 Direct Simulation Monte Carlo Calculations of Aerothermodynamics for Mars Microprobe Heating Analysis of the Nosecap and Leading Aerothermodynamics for Mars Microprobe Capsules A99-048 Edges of the X-34 Vehicle Capsules A99-048 Automatic Landing Flight Experiment Flight A99-024 Low-Density Aerodynamics of the Stardust Sam- Simulation Analysis and Flight Testing Numerical Investigation of Shock/Vortex Inter- ple Return Capsule A99-053 A99-069 action in Hypersonic Thermochemical Non- Aerodynamics of a Spinning Cylinder in Rar- equilibrium Flow A99-028 efied Gas Flows A99-059 Flight Mechanics Numerical Study of Hypersonic Rarefied-Gas Detailed Simulation of Surface Chemistry Lead- Flows About a Torus A99-035 ing to Spacecraft Glow A99-071 Low-Thrust Trajectory Optimization Based on Mars Pathfinder Rarefied Aerodynamics: Com- Analysis of Pressure Measurements During Epoch Eccentric Longitude Formulation putations and Measurements Cold-Gas Thruster Firings Onboard Suborbital A99-068 A99-040 Spacecraft A99-088 Limit Cycle and Chaotic Behavior in Persistent Prediction and Validation of Mars Pathfinder Resonance of Unguided Missiles Hypersonic Aerodynamic Database Shock Waves and Detonations A99-112 A99-044 Low-Density Aerodynamics of the Stardust Sam- Performance Study of a Power Law Starbody Launch Vehicle Dynamics ple Return Capsule A99-082 Entry Dispersion Analysis for the Stardust A99-053 Power Law Shapes for Leading-Edge Blunting Aerothermodynamics of the Stardust Sample Re- with Minimal Shock Standoff Comet Sample Return Capsule Opttiurmna lC apsAurltief icially Blunted LeadingA9-9E-d0g5e4 A99-083 Elastic Response of Generic Space VehiclAe9 9-H0a5v5- Airfoils for Enhanced Aerothermodynamic Subsonic Flow ing Degraded Interstage Joints Performance A99-061 A99-058 Simple Analytical Model for Parametric Studies Reynolds Number Effects on Low-Speed Aero- of Hypersonic Waveriders dynamics of a Hypersonic Configuration Launch Vehicle Guidance and Control A99-064 A99-031 Preliminary Static Aeroelastic Analysis of Re- Plasma Electron Density Measurement Around Ceramics Catalysis Evaluation at High Tempera- usable Launch Vehicle Stability and Control Hypersonic Flight Experiment Vehicle ture Using Thermal and Chemical Approaches Derivatives A99-006 A99-072 A99-032 Performance Study of a Power Law Starbody Missile Dynamics A99-082 Supersonic Flow Power Law Shapes for Leading-Edge Blunting Erratum on “Aerodynamic Interference for Hy- with Minimal Shock Standoff Flight Data for Boundary-Layer Transition at personic Missiles at Low Angle of Attack” A99-083 Hypersonic and Supersonic Speeds A98-117 Three-Dimensional Shock/Boundary-Layer In- A99-001 Angular Motion Effects on Kinetic Energy Pro- teraction Between a Rocket and a Booster jectile Performance A99-034 A99-087 Transonic Flow Limit Cycle and Chaotic Behavior in Persistent Surface Heating Effects of X-33 Vehicle Ther- Resonance of Unguided Missiles mal-Protection-System Panel Bowing A99-109 ComWpruatpaatrioounn do f FiRnolsl UMsionmge nEtu lefro r EPqruoajteicotinl e with A99-112 Aerothermodynamic Analyses of Hypersonic, A99-004 Missile Guidance and Control Blunt-Body Flows A99-119 Unsteady Flows Engineering-, Intermediate-, and High-Lev- Inlet, Nozzle, Diffuser, and Channel Flows el Aerodynamic Prediction Methods and Numerical Investigation of Shock/Vortex Inter- Applications A99-079 Development of Pulsed Arc Heater for Small Hy- action in Hypersonic Thermochemical Non- personic High-Enthalpy Wind Tunnel equilibrium Flow A99-028 Navigation A99-091 Low-Speed Aerodynamics of a Planetary Entry Capsule A99-084 Technology of Automated Rendezvous and Cap- Jets, Wakes, and Viscid-Inviscid Flow Utilization of Low-Speed Experiments in Tran- ture in Space A99-033 Interactions sonic Capsule Stability Research Navigation Flight Operations for Mars Pathfinder A99-101 A99-041 Base Flow Predictions for a Lightsat Launcher at Supersonic Speeds A99-029 Vortices Optimization Techniques Viscous Multiblock Simulations of Axisymmet- ric Launch Vehicle Flows Computational Simulation Improvements of Su- Multiple-Burn Families of Optimal Low- and A99-060 personic High-Angle-of-Attack Missile Flows Medium-Thrust Orbit Transfers Low-Speed Aerodynamics of a Planetary Entry A99-005 A99-113 Capsule A99-084 Reynolds Number Effects on Low-Speed Aero- Three-Dimensional Shock/Boundary-Layer In- dynamics of a Hypersonic Configuration Spacecraft Dynamics teraction Between a Rocket and a Booster A99-031 A99-087 Nanometer Regularity in the Mechanics of a Pre- Utilization of Low-Speed Experiments in Tran- cision Deployable Spacecraft Structure Joint sonic Capsule Stability Research Guidance, Control, and Dynamics A99-098 A99-101 Technology Inverse Simulation of Aeroassisted Orbit Plane Change of a Spacecraft A99-115 Plasmadynamics and MHD Astrodynamics Spacecraft Guidance and Control Expansion of Multicharged Plasma Clouds into Application of Accelerometer Data to Mars Glo- lonospheric Plasma with Magnetic Field bal Surveyor Aerobraking Operations Analysis of Hubble Space Telescope Reaction A99-118 A99-039 Wheel Lubricant A99-013 928 J. SPACECRAFT, VOL. 36, NO.6: 1999 INDEX Technology of Automated Rendezvous and Cap- Computation of Roll Moment for Projectile with Solid Rocket Motor Development for Land- ture in Space A99-033 Wraparound Fins Using Euler Equation Based Intercontinental Ballistic Missiles Multiple-Burn Families of Optimal Low- and A99-004 A99-116 Medium-Thrust Orbit Transfers Study of Roll Stability Derivatives A99-113 A99-019 Simulation Inverse Simulation of Aeroassisted Orbit Plane X-34 Vehicle Aerodynamic Characteristics Change of a Spacecraft A99-115 A99-027 Payload Fairing Separation Dynamics Measuring Attitude Rates Through Angular Mo- Base Flow Predictions for a Lightsat Launcher at A99-063 Supersonic Speeds A99-029 mentum Gyros A99-121 Grooves Effect on Lift: Data Correlation and Pre- Structural Design (Including Loads) Trajectory Optimization diction for Kinetic Energy Projectiles A99-030 Probability of Structural Failure of a Satellite Entry Dispersion Analysis for the Stardust Reynolds Number Effects on Low-Speed Aero- Launching Motor: A Case Study Comet Sample Return Capsule dynamics of a Hypersonic Configuration A99-011 A99-055 A99-031 Fracture Control of Space Flight Structures and Low-Thrust Trajectory Optimization Based on Entry Dispersion Analysis for the Stardust Pressure Vessels A99-067 Epoch Eccentric Longitude Formulation Comet Sample Return Capsule A99-068 A99-055 Subsystem Design and Ground Support Multiple-Burn Families of Optimal Low- and Viscous Multiblock Simulations of Axisymmet- Medium-Thrust Orbit Transfers ric Launch Vehicle Flows Postfire Short Circuit Phenomena of Electroex- A99-113 A99-060 plosive Initiators A99-074 Orbit Transfer with a Variable Thrust Hall Optimal Artificially Blunted Leading-Edge Air- foils for Enhanced Aerothermodynamic Per- Testing, Flight and Ground Thruster Under Drag A99-114 formance A99-061 Asymmetric Divert Jet Performance of a Super- Aerothermodynamic Environment for a Generic Interdisciplinary Topics sonic Missile: Computational and Experimen- Missile A99-003 tal Comparisons A99-080 Atmospheric Reentry Demonstrator Balloon Aerospace Management Application of the 1998 Version of the Aeropre- Flight Test A99-062 diction Code A99-081 Two Options for Flight Testing Rocket-Based Market-Based Approach for Manifesting Shuttle Euler and Navier-Stokes Solutions for Missiles Combined-Cycle Engines Secondary Payloads A99-017 at High Angles of Attack A99-089 A99-111 Solid Rocket Motor Development for Land- Analytical and Numerical Methods Based Intercontinental Ballistic Missiles Configuration Design Grooves Effect on Lift: Data Correlation and Pre- A99-116 diction for Kinetic Energy Projectiles Study of Roll Stability Derivatives Thermal Protection Systems A99-030 A99-019 Radar and Optical Characterization of an Anom- Simple Analytical Model for Parametric Studies Computational Aeroheating Predictions for alous Orbital Debris Population of Hypersonic Waveriders X-34 A99-022 A99-093 A99-064 Thermostructural Analysis of X-34 Wing Lead- Surface Heating Effects of X-33 Vehicle Ther Mini/Micro Shuttles with Hypergolic Noncryo- ing-Edge Tile Thermal Protection System mal-Protection-System Panel Bowing genic Liquid Rocket Bipropellant A99-023 A99-109 A99-078 Analysis of Galileo Probe Heatshield Ablation Application of the 1998 Version of the Aeropre- Atmospheric and Space Sciences diction Code A99-081 and Temperature Data A99-036 Mars Pathfinder Entry Temperature Data, Performance Study of a Power Law Starbody Application of Accelerometer Data to Mars Glo- Aerothermal Heating, and Heatshield Mate- A99-082 bal Surveyor Aerobraking Operations rial Response A99-046 A99-039 Launch Vehicle and Sounding Rocket Systems Ablation and Thermal Response Program for Radar and Optical Characterization of an Anom- Spacecraft Heatshield Analysis alous Orbital Debris Population Preliminary Static Aeroelastic Analysis of Re- A99-057 A99-093 usable Launch Vehicle Stability and Control Surface Heating Effects of X-33 Vehicle Ther- Derivatives A99-006 mal-Protection-System Panel Bowing Research Facilities and Instrumentation Mini/Micro Shuttles with Hypergolic Noncryo- A99-109 genic Liquid Rocket Bipropellant Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Ther- Three-Stage Launch System with ScramjetA9s9 -078 Propulsion mography Method A99-020 Development of Pulsed Arc Heater for Small Hy- A99-086 Ducted Rocket Engines Two Options for Flight Testing Rocket-Based personic High-Enthalpy Wind Tunnel A99-091 LiqCuoimd biPnreopdu-lCsyicoln e LaEunngcihne sV ehicle ReliabiAi9l9t-y0 89in TwoC omObpitnieodn-sC yfcolre FlEingghit neTse sting RocketA-9B9a-s0e8d9 Closed Form A99-090 Safety Electric and Advanced Space Propulsion Missile Systems Quantifying and Reducing International Space Station Vulnerability Following Orbital De- Orbit Transfer with a Variable Thrust Hall Asymmetric Divert Jet Performance of a Super- bris Penetration A99-016 Thruster Under Drag A99-114 sonic Missile: Computational and Experimen- Sensor Systems tal Comparisons A99-080 Ignition and Ignitor Design Application of the 1998 Version of the Aeropre- Radar and Optical Characterization of an Anom- diction Code A99-081 Postfire Short Circuit Phenomena of Electroex- alous Orbital Debris Population High-Angle-of-Attack Aerodynamics of a Mis- plosive Initiators A99-074 A99-093 sile Geometry at Low Speed A99-100 Liquid Rocket Motors and Missile Systems Solid Rocket Motor Development for Land- Launch Vehicle and Missile (LV/M) Based Intercontinental Ballistic Missiles Liquid Propulsion Launch Vehicle Reliabiilty in Technology A99-116 Closed Form A99-090 Aerodynamics Propulsion and Propellant Systems Ramijets and Scramjets Aerothermodynamic Environment for a Generic Postfire Short Circuit Phenomena of Electroex- Effects of Shock Wave Impingement on Super- Missile A99-003 plosive Initiators A99-074 sonic Film Cooling A99-077 J. SPACECRAFT, VOL. 36, NO. 6: 1999 INDEX 929 Solid Rocket Motors and Missile Systems Mars Polar Lander Aerothermodynamic and En- Analysis of Spacecraft Anomalies due to the Ra- try Dispersion Analysis diation Environment Probability of Structural Failure of a Satellite A99-051 A99-117 Launching Motor: A Case Study Orbit Transfer with a Variable Thrust Hall Measuring Attitude Rates Through Angular Mo- A99-011 Thruster Under Drag A99-114 mentum Gyros A99-121 Space Technology Space Experiments Spacecraft Structural Configuration, Design, and Analysis Near Earth Asteroid Rendezvous (NEAR) Space- Aerobraking Configurations/ Aerothermodynamics craft Solar Conjunction Experiment Comment on “Spacecraft Launch Depressuriza- A99-009 tion Loads” A97-125 Mars Global Surveyor: Aerobraking Mission Interplanetary Meteoroid Environment Model Reply to R. C. Mehta A97-125 Overview A99-037 Update A99-015 Interplanetary Meteoroid Environment Model Rarefied Aerothermodynamic Predictions for Analysis of Pressure Measurements During Update A99-015 Mars Global Surveyor Cold-Gas Thruster Firings Onboard Suborbital Quantifying and Reducing International Space Spacecraft A99-088 A99-038 Analysis of Spacecraft Anomalies due to the Ra- Station Vulnerability Following Orbital De- Mars Pathfinder Rarefied Aerodynamics: Com- bris Penetration A99-016 diation Environment A99-117 putations and Measurements Fracture Control of Space Flight Structures and A99-040 Space Systems Pressure Vessels A99-067 Mars Polar Lander Aerothermodynamic and En- Paraboloidally Shaped Antenna Possessing try Dispersion Analysis Near-Polar Satellite Constellations for Continu- Pointing and Beam-Width Control A99-051 ous Global Coverage A99-010 A99-095 Low-Density Aerodynamics of the Stardust Sam- Design Optimization of Phased-Array-Fed Re- Model-Based Thruster Leakage Monitor for the ple Return Capsule A99-053 flector Antennas for Mobile Communication Cassini Spacecraft A99-096 Transition Effects on Heating in the Wake of a Satellites A99-012 Blunt Body A99-085 Analysis of Hubble Space Telescope Reaction Spacecraft Test and Evaluation Development of Pulsed Arc Heater for Small Hy- Wheel Lubricant A99-013 personic High-Enthalpy Wind Tunnel Direct Simulation of Space Debris Evolution Atmospheric Reentry Demonstrator Balloon A99-091 A99-014 Flight Test A99-062 Quantifying and Reducing International Space Automatic Landing Flight Experiment Flight Aerobraking Flight Mechanics Station Vulnerability Following Orbital De- Simulation Analysis and Flight Testing bris Penetration A99-016 A99-069 Mars Global Surveyor: Aerobraking Mission Mars Pathfinder Entry, Descent, and Landing Electrical Breakdown of Anodized Coatings in Overview A99-037 Reconstruction A99-043 Low-Density Plasmas A99-073 Application of Accelerometer Data to Mars Glo- Atmospheric Reentry Demonstrator Balloon Low-Speed Aerodynamics of a Planetary Entry bal Surveyor Aerobraking Operations Flight Test A99-062 Capsule A99-084 A99-039 Self-Assembling Transfer Vehicles for Human Utilization of Low-Speed Experiments in Tran- Mars Pathfinder Atmospheric Entry Navigation Mars Missions A99-076 sonic Capsule Stability Research Operations A99-042 Model-Based Thruster Leakage Monitor for the A99-101 Mars Pathfinder Entry, Descent, and Landing Cassini Spacecraft A99-096 Reconstruction A99-043 Spacecraft Thermal Management Mars Microprobe Entry-to-Impact Analysis Spacecraft Communication A99-050 Near Earth Asteroid Rendezvous (NEAR) Space- Flexible Heat Pipes for a Lightweight Spacecraft Mars Polar Lander Aerothermodynamic and En- Radiator A99-092 craft Solar Conjunction Experiment try Dispersion Analysis A99-051 Transient Thermal Sensitivity Analysis During A99-009 Solar Eclipse with Discontinuous Heat Load Design Optimization of Phased-Array-Fed Re- Landers flector Antennas for Mobile Communication A99-120 Mars Microprobe Entry-to-Impact Analysis Satellites A99-012 A99-050 Paraboloidally Shaped Antenna Possessing Structural Mechanics and Materials Pointing and Beam-Width Control Mission Design and Analysis A99-095 Aeroelasticity and Control Near-Polar Satellite Constellations for Continu- Spacecraft Contamination/Sterilization Preliminary Static Aeroelastic Analysis of Re- ous Global Coverage A99-010 usable Launch Vehicle Stability and Control Interplanetary Meteoroid Environment Model Particle Environment Surrounding the Mid- Derivatives A99-006 Update A99-015 course Space Experiment Spacecraft Aeroelastic Effects on the Roll Characteristics of Rarefied Aerothermodynamic Predictions for A99-070 a Wraparound Fin Projectile Mars Global Surveyor A99-038 Spacecraft Data Sensing, Processing, and A99-065 Mars Pathfinder Atmospheric Entry Navigation Transmission Operations A99-042 Flexible and Active Structures Mars Pathfinder Entry, Descent, and Landing Paraboloidally Shaped Antenna Possessing Reconstruction A99-043 Friction Model of a Revolute Joint for a Precision Pointing and Beam-Width Control Mars Microprobe Entry-to-Impact Analysis Deployable Spacecraft Structure A99-095 A99-050 A99-075 Self-Assembling Transfer Vehicles for Human Spacecraft Propulsion System Integration Nanometer Regularity in the Mechanics of a Pre- Mars Missions A99-076 cision Deployable Spacecraft Structure Joint Three-Stage Launch System with Scramjets Self-Assembling Transfer Vehicles for Human A99-098 A99-086 Mars Missions A99-076 Materials Structural Properties Mission Trajectories (Earth and Spacecraft Radiation Protection Interplanetary) In Situ Erosion Study of Kapton® Using a Novel Analysis of Spacecraft Anomalies due to the Ra- Hyperthermal Oxygen Atom Source Near-Polar Satellite Constellations for Continu- diation Environment A99-117 A99-007 ous Global Coverage A95-010 Mars Global Surveyor: Aerobraking Mission Spacecraft Sensor Systems Structural Design Overview A99-037 Navigation Flight Operations for Mars Pathfinder Model-Based Thruster Leakage Monitor for the Friction Model of a Revolute Joint for a Precision A99-041 Cassini Spacecraft A99-096 Deployable Spacecraft Structure A99-075 930 J. SPACECRAFT, VOL. 36, NO. 6: 1999 INDEX Structural Durability (Including Fatigue, Structural Stability Ceramics Catalysis Evaluation at High Tempera- Fracture, and Environmental Degradation) ture Using Thermal and Chemical Approaches High-Supersonic/Hypersonic Flutter of Prismat- A99-032 Errata on “Influence of X-Ray Solar Flare Radi- ic Composite Plate/Shell Panels Analysis of Galileo Probe Heatshield Ablation ation on Degradation of Teflon® in Space” A99-097 and Temperature Data A99-036 A97-081 Nonlinear Behavior of the Space Shuttle Super- Prediction and Validation of Mars Pathfinder In Situ Erosion Study of Kapton® Using a Novel lightweight Liquid-Oxygen Tank Under Pre- Hypersonic Aerodynamic Database Hyperthermal Oxygen Atom Source launch Loads A99-104 A99-044 A99-007 Modeling and Nonlinear Structural Analysis of a Mars Pathfinder Entry Temperature Data, Fracture Control of Space Flight Structures and Large-Scale Launch Vehicle Aerothermal Heating, and Heatshield Mate- Pressure Vessels A99-067 A99-105 rial Response A99-046 Effects of Welding-Induced Imperfections on Direct Simulation Monte Carlo Calculations of Structural Dynamics and Characterization Behavior of Space Shuttle Superlightweight Aerothermodynamics for Mars Microprobe Tank A99-106 Capsules A99-048 Elastic Response of Generic Space Vehicle Hav- Nonlinear Behavior of Space Shuttle Superlight- Aerothermodynamics of the Stardust Sample Re- ing Degraded Interstage Joints weight Tank Under Booster Ascent Loads turn Capsule A99-054 A99-058 A99-107 Ablation and Thermal Response Program for Payload Fairing Separation Dynamics Nonlinear Behavior of Space Shuttle Superlight- Spacecraft Heatshield Analysis A99-063 weight Tank Under End-of-Flight Loads A99-057 Friction Model of a Revolute Joint for a Precision A99-108 Power Law Shapes for Leading-Edge Blunting Deployable Spacecraft Structure with Minimal Shock Standoff Thermal Effects A99-075 A99-083 Nanometer Regularity in the Mechanics of a Pre- Ceramics Catalysis Evaluation at High Tempera- Transition Effects on Heating in the Wake of a cision Deployable Spacecraft Structure Joint ture Using Thermal and Chemical Approaches Blunt Body A99-085 A99-098 A99-032 Analysis of Linear Aerospike Plume-Induced X- Submicron Mechanical Stability of a Proto- Numerical Simulation of Metallic Thermal Pro- 33 Base-Heating Environment type Deployable Space Telescope Support tection System Panel Bowing A99-102 Structure A99-099 A99-110 Numerical Simulation of Metallic Thermal Pro- tection System Panel Bowing Structural Finite Elements A99-110 Thermophysics and Heat Transfer Fabrication and Testing of a Leading-Edge- Nonlinear Behavior of the Space Shuttle Super- Shaped Heat Pipe A99-122 lightweight Liquid-Oxygen Tank Under Pre- Ablation, Pyrolysis, Thermal Decomposition, launch Loads A99-104 and Degradation Computational Heat Transfer Modeling and Nonlinear Structural Analysis of a Analysis of Galileo Probe Heatshield Ablation Large-Scale Launch Vehicle Analysis of Linear Aerospike Plume-Induced X- and Temperature Data A99-036 A99-105 Mars Pathfinder Entry Temperature Data, 33 Base-Heating Environment Effects of Welding-Induced Imperfections on Aerothermal Heating, and Heatshield Mate- A99-102 Behavior of Space Shuttle Superlightweight rial Response A99-046 Tank A99-106 Aerothermodynamics oft he Stardust Sample Re- Heat Pipes Nonlinear Behavior of Space Shuttle Superlight- turn Capsule A99-054 Fabrication and Testing of Mo-—Re Heat Pipes weight Tank Under Booster Ascent Loads Ablation and Thermal Response Program for Embedded in Carbon/Carbon A99-107 Spacecraft Heatshield Analysis A99-008 Nonlinear Behavior of Space Shuttle Superlight- A99-057 Flexible Heat Pipes for a Lightweight Spacecraft weight Tank Under End-of-Flight Loads Aerothermodynamics/Thermal Protection Radiator A99-092 A99-108 Fabrication and Testing of a Leading-Edge- Computational Aerothermodynamic Design Is- Shaped Heat Pipe A99-122 Structural Modeling sues for Hypersonic Vehicles Probability of Structural Failure of a Satellite A99-002 Nonintrusive Diagnostics Fabrication and Testing of Mo—Re Heat Pipes Launching Motor: A Case Study Embedded in Carbon/Carbon Global Aeroheating Wind-Tunnel Measurements A%9-011 A99-008 Using Improved Two-Color Phosphor Ther- Nonlinear Behavior of the Space Shuttle Super- Global Aeroheating Wind-Tunnel Measurements mography Method A99-020 lightweight Liquid-Oxygen Tank Under Pre- Using Improved Two-Color Phosphor Ther- launch Loads A99-104 mography Method A99-020 Thermal Control Modeling and Nonlinear Structural Analysis of a X-34 Experimental Aeroheating at Mach 6 Large-Scale Launch Vehicle and 10 A99-021 Errata on “Influence of X-Ray Solar Flare Radi- A99-105 Computational Aeroheating Predictions for ation on Degradation of Teflon® in Space” Effects of Welding-Induced Imperfections on X-34 A99-022 497-081 Behavior of Space Shuttle Superlightweight Thermostructural Analysis of X-34 Wing Lead- Tank A99-106 ing-Edge Tile Thermal Protection System Thermal Modeling and Analysis Nonlinear Behavior of Space Shuttle Superlight- Heating Analysis of the Nosecap and LAe9a9d-i0n23g Characteristics of an Anomalous Orbital De- weight Tank Under Booster Ascent Loads Edges of the X-34 Vehicle bris Population Inferred from Theoretical A99-107 A99-024 Modeling A99-094 Nonlinear Behavior of Space Shuttle Superlight- Aeroheating Predictions for X-34 Using an Invis- Numerical Simulation of Metallic Thermal Pro- weight Tank Under End-of-Flight Loads cid Boundary-Layer Method tection System Panel Bowing A99-108 A99-025 A99-110 J. SPACECRAFT, VOL. 36, NO. 6: 1999 INDEX Author Index Alemdaroglu, N., A99-111 Ferrari, Marceilo A. S., Maymon, Giora, A99-011 Serpico, M., A99-029 Allasio, Andrea, A99-062 A99-060 Maynes, D., A99-100 Shane, R. W., A99-038 Alter, Stephen J., A99-022, Galica, Gary E., A99-070 McGhee, David, A99-006 Sherman, Brian, A99-109 A99-025 Galofaro, J. T., A99-073 Mclnville, R. M., A99-081 Shoki, Hiroki, A99-012 Appelbaum, G., A99-114 Gaposchkin, E. M., A99-093 Mee, David, A99-082 Sigal, Asher, A99-019 Ashkenazy, J., A99-114 Garrett, Henry B., A99-015 Mehta, R. C., A97-125 Silver, David M., A99-070 Azevedo, Joao L. F., A99-060 Gatsonis, Nikos A., A99-088 Merrigan, Michael A., A99-008, Silverberg, Larry M., A99-095 Badie, J. M., A99-032 Gebert, G. A., A99-100 A99-122 Snyder, D. B., A99-073 Bae, Jae-Sung, A99-004 Glass, Christopher, A99-021 Merski, N. Ronald, A99-020, Spencer, D. A., A99-041, A99-042, Balat, M. J. H., A99-032 Glass, David E., A99-008, A99-092, A99-021 A99-043 Beavers, W., A99-093 A99-122 Mikhail, Ameer G., A99-030 Squire, T. H., A99-023, A99-036 Beerer, Joseph G., A99-037 Gnoffo, Peter A., A99-002, Milintchouk, Andrei, A97-081 Sridharan, R., A99-093, A99-094 Benson, Richard C., A99-070 A99-022, A99-044 Milos, F. S., A99-023, A99-036, Srivastava, B., A99-080 Berry, Scott A., A99-021 Goodson, Troy D., A99-113 A99-046, A99-057 Stanley, Robert J., A99-095 Bertin, John J., A99-003 Green, B. David, A99-070 Mitcheltree, R. A., A99-044, Stansbery, E., A99-093 Bertrand, P. A., A99-013 Greene, F. A., A99-047, A99-052 A99-047, A99-049, A99-050, Stark, John P. W., A99-014 Biagioni, Leonardo, A99-091 Grossman, Eitan, A99-007 A99-052, A99-053, A99-055 Starkey, Ryan P., A99-064 Blacklock, Kevin, A99-016 Guelman, M., A99-114 Miyazawa, Yoshikazu, Starnes Jr., James H., A99-104, Blanchard, Robert C., A99-040, Gupta, Anurag, A99-061 A99-069 A99-106, A99-107, A99-108 A99-043 Gupta, S. C., A99-120 Moore, F. G., A99-081 Steele, C. R., A99-066 Boies, Mark T., A99-070 Guy, Thomas D., A99-016 Moore, William V., A99-009 Stevens, Jonathan C., A99-092 Bokulic, Robert S., A99-009 Hachkowski, M. Roman, Moss, J. N., A99-040, A99-047, Strauss, Daniel, A99-060 Boltz, Frederick W., A99-078 A99-075 A99-048, A99-053 Sturek, Walter B., A99-018 Borriello, Giorgio, A99-062 Hagiwara, Takanori, A99-103 Motoda, Toshikazu, A99-069 Suresha, S., A99-120 Boyd, Iain D., A99-071 Hamilton, H. Harris, II, Mount, Charles K., A99-007 Surzhikov, Sergey T., A99-118 Brauckmann, G. J., A99-027, A99-002 Nagatomo, Hideo, A99-028 Sutharshana, S., A99-067 A99-052 Hanson, John, A99-113 Nakamura, Yoshiaki, A99-087 Swaminathan, P. K., A99-088 Braun, R. D., A99-036, A99-040, Harper, Tim, A97-081 Nelson, H. F., A98-117 Takaki, Ryoji, A99-072 A99-041, A99-042, A99-043, Hegedus, Martin C., A99-079 Nemeth, Michael P., A99-104, Takasu, Norinao, A99-028 A99-044, A99-047, A99-049, Hillstrom, Derek G., A98-117 A99-106, A99-107, A99-108 Takita, Kenichi, A99-077 A99-050, A99-051, Hinkle, Jason D., A99-099 Neuwerth, G., A99-031 Tanahashi, Yoshiharu, Britt, Vicki O., A99-104 Hoflund, Gar B., A99-007 Nishio, Masatomi, A99-103 A99-087 _ Brunty, Joseph A., A99-006 Hollis, Brian R., A99-085 Noll, S. N., A99-039 Tanrikulu, Omer, A99-112 Bullock, Steven J., A99-098 Horvath, T. J., A99-021, O’Brien, Timothy F., A99-083 Tarhan, E., A99-111 Butler, Robert J., A99-003 A99-049 Ohara, Tsuyoshi, A99-087 Tauber, Michael E., A99-054 Caledonia, George E., A99-071 Hosken, R., A99-117 Oktay, E., A99-111 Taylor, Malcolm S., A99-018 Camarda, Charles J., A99-008, Huang, Zhaofeng, A99-090 Okumura, Minoru, A99-012 Teraoka, Ken, A99-072 A99-122 Hymer, T. C., A99-081 Olds, John R., A99-089 Thornton, Janine M., A99-046 Cancro, G. J., A99-039 Ishikawa, Kazutoshi, A99-069 Oliver, John P., A99-015 Thurman, Sam W., A99-043 Carlson, Henry A., A99-119 Ito, Takeshi, A99-072 Olynick, David R., A99-002, Tokunaga, Kyoko, A99-012 Carré, D. J., A99-013 Izumi, Tatsushi, A99-069 A99-054 Tolson, R. H., A99-039 Champigny, P., A99-111 Jacob, D., A99-031 Paek, Seung-Kil, A99-004, Towne, Matthew C., A99-003 Chang, J. B., A99-067 Johnston, M. Daniel, A99-037 A99-065 Tsunoda, Hiroaki, A99-012 Charbonnier, Jean-Marc, A99-084, Joshi, A., A99-058 Paganucci, Fabrizio, A99-091 Ulybyshev, Yuri, A99-010 A99-101 Josyula, Eswar, A99-005 Palmer, Grant, A99-024, A99-109, Uy, O. Manuel, A99-070 Cheatwood, F. M., A99-038, Kallemeyn, P. H., A99-041, A99-110 Vampola, A. L., A99-117 A99-047, A99-050, A99-051, A99-042, A99-043 Paris, Sebastien, A99-101 Van Eesbeek, Marc, A97-081 A99-052, A99-055 Kansky, J., A99-093 Park, Tae-Sang, A99-004 Vaughan, R. M., A99-041, Chen, Alice J., A99-003 Karatekin, Ozgiir, A99-084, Parker, J. S., A99-039 A99-042 Chen, Y.-K., A99-036, A99-046, A99-101 Paull, Allan, A99-082 Vavala, Raffaele, A99-062 A99-054, A99-057, A99-063 Karipides, Daniel P., A99-071 Peiter, U., A99-031 Vayner, B. V., A99-073 Chuang, Jason C. H., A99-113 Keating, G. M., A99-039 Perkins, John N., A99-085 Venkatapathy, Ethiraj, Ciucci, A., A99-029 Kechichian, Jean Albert, Perkins, Stanley C., Jr., A99-079 A99-002 Collins, Timothy J., A99-104, A99-068 Peterson, Lee D., A99-075, Wang, Frank Y., A99-084, A99-101 A99-106, A99-107, A99-108 Kennedy, W. S., A99-116 A99-098, A99-099 Wang, Liqun, A99-014 Congdon, William M., A99-046 Kimura, Toshiyuki, A99-086 Polites, Michael E., A99-033 Wang, S., A99-097 Cosentino, Orazio, A99-062 Kleb, William L., A99-022, Polsky, Susan, A99-024 Wang, Ten-See, A99-102 Czerniak, M., A99-032 A99-025 Porter, David, A99-017 Warren, Peter A., A99-099 d’Espiney, P., A99-111 Koga, R., A99-117 Powell, Richard W., A99-044, Weilmuenster, K. James, A99-002, De Giorgis, Maurizio, A99-062 Kontinos, Dean A., A99-109, A99-051 A99-044 de Divitiis, Nicola, A99-115 A99-110 Price, Joseph M., A99-048 Wessen, Randii R., A99-017 Decker, F., A99-031 Kovacic, S. M., A99-116 Queen, Eric M., A99-051 Wilkerson, B. L., A99-039 Desai, Prasun N., A99-055 Kumar, C. K., A99-088 Raitses, Y., A99-114 Willcockson, William H., DiFulvio, M., A99-049 Kwon, Jang Hyuk, A99-004 Raman, V. V., A99-092 A99-037, A99-045, A99-056 DiFulvio, Michael, A99-021 Lake, Mark S., A99-075 Rankin, Charles C., A99-105 Williamsen, Joel, A99-016 Dillenius, Marnix F. E., Lambour, R., A99-093, A99-094 Rault, D. F., A99-038 Wilmoth, R. G., A99-038, A99-079 Lauriente, M., A99-117 Rea, E. C., A99-116 A99-052 Donahue, Benjamin, A99-076 Lee, Allan Y., A99-096 Reid, Robert S., A99-122 Wilmoth, Richard C., A99-040, Doreswamy, C. V., A99-073 Lee, In, A99-004, A99-065 Riabov, Vladimir V., A99-035, A99-048, A99-053 Drouilhet, S. J., A99-015 Lesieutre, Daniel J., A99-079 A99-059 Wolan, John T., A99-007 Edquist, C. Thomas, A99-051 Lesieutre, Teresa O., A99-079 Riley, Christopher J., A99-025, Wood, William A., A99-022 Engelund, W. C., A99-038, Levadou, Francois, A97-081 A99-026 Wurster, Kathryn E., A99-026 A99-044 Leveugle, Thierry, A99-062 Ruffin, Stephen M., A99-061 Yamamoto, Satoru, A99-028 Erlandson, R. E., A99-088 Lewis, Mark J., A99-064, A99-082, Sabean, John W., A99-082 Yang, Lien C., A99-074 Esposito, Pasquale, A99-037 A99-083 Sanz-Andrés, Angel, A97-125 Young, Richard D., A99-104, Evans, Hilary J., A99-016 Lifshitz, Y., A99-007 Sawada, Keisuke, A99-086 A99-105, A99-106, A99-107, Evans, R. W., A99-015 Lin, T. C., A99-116 Schettino, A., A99-029 A99-108 Fabrizi, M., A99-029 Lou, M. C., A99-067 Schmidt, Edward M., A99-034 Zeiler, Thomas A., A99-006 Falconi, D., A99-029 Love, John F., A99-079 Schneider, Steven P., A99-001 Zhang, Hong-Hua, A99-121 Fay, J. P., A99-066 Lyons, Daniel T., A99-037 Scortecci, Fabrizio, A99-091 Zoby, E. Vincent, A99-026 Ferguson, D. C., A99-073 Masuya, Goro, A99-077 Sena, J. Tom, A99-008, A99-122 Zuber, Matthew E., A99-003 J. SPACECRAFT, VOL. 36, NO.6: 1999 INDEX Chronological Index A97-081 Influence of X-Ray Solar Flare Radiation on Degra- A99-011 Probability of Structural Failure of a Satellite dation of Teflon” in Space. Andrei Milintchouk, Marc Van Ees- Launching Motor: A Case Study. Giora Maymon, RAFAEL, beek, Francois Levadou, and Tim Harper, European Space Agency, Ministry of Defence, Israel (36, 1, p. 100) Article The Netherlands (34, 4, p. 542) Article Errata (36, 2, p. 296) A99-012 Design Optimization of Phased-Array-Fed Reflector Antennas for Mobile Communication Satellites. | Kyoko A97-125 Spacecraft Launch Depressurization Loads. Angel Tokunaga and Hiroaki Tsunoda, Advanced Space Communications Sanz-Andrés, Julian Santiago-Prowald, and Antonio Ayuso-Barea, Research Laboratory, Japan; and Hiroki Shoki and Minoru Oku- Universidad Politécnica de Madrid, Spain (34, 6, p. 805) Article mura, Toshiba Corporation, Japan (36, 1, p. 105) Article based on Technical Comment by R. C. Mehta, Vikram Sarabhai Space AIAA Paper 98-1223 ISBN 1-56347-264-3 Centre, India (36, |, p. 152) Reply (36, 1, p. 152) A99-013 Analysis of Hubble Space Telescope Reaction Wheel Lubricant. D. J. Carré and P. A. Bertrand, The Aerospace Corpo- 498-117 Aerodynamic Interference for Hypersonic Missiles at ration (36, 1, p. 109) Article Low Angle of Attack. H. F. Nelson and Derek G. Hillstrom, Uni- versity of Missouri-Rolla (35, 6, p. 749) Article based on AIAA Pa- A99-014 Direct Simulation of Space Debris Evolution. Liqun per 98-0680 Wang and John P. W. Stark, University of London, England, UK Errata (36, 6, p. 924) (36, 1, p. 114) Article A99-001 Flight Data for Boundary-Layer Transition at Hy- A99-015 Interplanetary Meteoroid Environment Model Up- personic and Supersonic Speeds. Steven P. Schneider, Purdue date. Henry B. Garrett, Jet Propulsion Laboratory, California In- University (36, 1, p. 8) Survey Paper stitute of Technology; S. J. Drouilhet, Moorhead State University; John P. Oliver, University of Florida; and R. W. Evans, OAO Cor- 499-002 Computational Aerothermodynamic Design Issues poration (36, 1, p. 124) Article based on AIAA Paper 98-1049 for Hypersonic Vehicles. Peter A. Gnoffo, K. James Weilmuen- ster, and H. Harris Hamilton II, NASA Langley Research Center, A99-016 Quantifying and Reducing International Space Sta- and David R. Olynick and Ethiraj Venkatapathy, NASA Ames Re- tion Vulnerability Following Orbital Debris Penetration. Joel search Center (36, 1, p. 21) Survey Paper Williamsen, NASA Marshall Space Flight Center, and Kevin Blacklock, Hilary J. Evans, and Thomas D. Guy, Sverdrup Tech- 499-003 Aerothermodynamic Environment for a Generic nology, Inc. (36, 1, p. 133) Article Missile. Matthew E. Zuber, Matthew C. Towne, Alice J. Chen, John J. Bertin, and Robert J. Butler, U.S. Air Force Academy (36, A99-017. Market-Based Approach for Manifesting Shuttle 1, p. 44) Article Secondary Payloads. Randii R. Wessen, Jet Propulsion Labora- tory, California Institute of Technology; and David Porter, Univer- 499-004 Computation of Roll Moment for Projectile with sity of Arizona (36, 1, p. 142) Article Wraparound Fins Using Euler Equation. Seung-Kil Paek, Tae- Sang Park, Jae-Sung Bae, In Lee, and Jang Hyuk Kwon, Korea Ad- A99-018 Statistical Comparison of Computed Surface Pres- vanced Institute of Science and Technology (36, |, p. 53) Article sure Predictions. Malcolm S. Taylor and Walter B. Sturek, U.S. Army Research Laboratory (36, 1, p. 148) Engineering Note 499-005 Computational Simulation Improvements of Super- sonic High-Angle-of-Attack Missile Flows. Eswar Josyula, U.S. A99-019 Study of Roll Stability Derivatives. Asher Sigal, Tech- Air Force Research Laboratory (36, 1, p. 59) Article based on nion—Israel Institute of Technology, Israel (36, 1, p. 150) Engi- AIAA Paper 98-0525 neering Note 499-006 Preliminary Static Aeroelastic Analysis of Reusable A99-020 Global Aeroheating Wind-Tunnel Measurements Launch Vehicle Stability and Control Derivatives. Thomas A. Using Improved Two-Color Phosphor Thermography Zeiler, University of Alabama; and David McGhee and Joseph A. Method. N. Ronald Merski, NASA Langley Research Center (36, Brunty, NASA Marshall Space Flight Center (36, 1, p. 67) Article 2, p. 160) Article 499-007 In Situ Erosion Study of Kapton” Using a Novel Hy- A99-021 X-34 Experimental Aeroheating at Mach 6 and 10. perthermal Oxygen Atom Source. Eitan Grossman and Y. Lif- Scott A. Berry, Thomas J. Horvath, Michael DiFulvio, Christopher shitz, Soreq NRC, Israel; and John T. Wolan, Charles K. Mount, Glass, and N. Ronald Merski, NASA Langley Research Center (36, and Gar B. Hoflund, University of Florida (36, 1, p. 75) Article 2, p. 171) Article 499-008 Fabrication and Testing of Mo—Re Heat Pipes Em- A99-022 Computational Aeroheating Predictions for X-34. bedded in Carbon/Carbon. David E. Glass, Analytical Services William L. Kleb, William A. Wood, and Peter A. Gnoffo, NASA and Materials, Inc.; Charles J. Camarda, NASA Johnson Space Langley Research Center, and Stephen J. Alter, Lockheed Engi- Center, and Michael A. Merrigan and J. Tom Sena, Los Alamos Na- neering and Sciences Company (36, 2, p. 179) Article based on tional Laboratory (36, |, p. 79) Article AIAA Paper 98-0879 499-009 Near Earth Asteroid Rendezvous (NEAR) Spacecraft 499-023. Thermostructural Analysis of X-34 Wing Leading- Solar Conjunction Experiment. Robert S. Bokulic, Johns Hop- Edge Tile Thermal Protection System. Frank S. Milos and Tho- kins University, Applied Physics Laboratory, and William V. mas H. Squire, NASA Ames Research Center (36, 2, p. 189) Article Moore, Jet Propulsion Laboratory, California Institute of Technol- ogy (36, 1, p. 87) Article A99-024 Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle. Grant Palmer, NASA Ames Research Center; A99-010 Near-Polar Satellite Constellations for Continuous and Susan Polsky, Thermosciences Institute (36, 2, p. 199) Article Global Coverage. Yuri Ulybyshev, Rocket-Space Corporation Energia,” Russia (36, |, p. 92) Article A99-025 Aeroheating Predictions for X-34 Using an Inviscid Errata (36, 4, p. 608) Boundary-Layer Method. Christopher J. Riley and William L. J. SPACECRAFT, VOL. 36, NO. 6: 1999 INDEX 933 Kleb, NASA Langley Research Center, and Steven J. Alter, Lock- A99-040 Mars Pathfinder Rarefied Aerodynamics: Computa- heed Engineering and Sciences Company (36, 2, p. 206) Article tions and Measurements. James N. Moss, Robert C. Blanchard, Richard C. Wilmoth, and Robert D. Braun, NASA Langley Re- A99-026 Engineering Aerothermal Analysis for X-34 Thermal search Center (36, 3, p. 330) Article based on AIAA Paper 98-0298 Protection System Design. Kathryn E. Wurster, Christopher J. Ri- ley, and E. Vincent Zoby, NASA Langley Research Center (36, 2, A99-041 Navigation Flight Operations for Mars Pathfinder. p. 216) Article Robin M. Vaughan, Pieter H. Kallemeyn Jr., and David A. Spen- cer, Jet Propulsion Laboratory, California Institute of Technol- A99-027 X-34 Vehicle Aerodynamic Characteristics. Gre- ogy; and Robert D. Braun, NASA Langley Research Center (36, 3, gory J. Brauckmann, NASA Langley Research Center (36, 2, p. p. 340) Article 229) Article A99-042 Mars Pathfinder Atmospheric Entry Navigation Op- A99-028 Numerical Investigation of Shock/Vortex Interaction erations. R. D. Braun, NASA Langley Research Center; and D. A. in Hypersonic Thermochemical Nonequilibrium Flow. Satoru Spencer, P. H. Kallemeyn, and R. M. Vaughan, Jet Propulsion Lab- Yamamoto and Norinao Takasu, Tohoku University, Japan; and oratory, California Institute of Technology (36, 3, p. 348) Article Hideo Nagatomo, Osaka University, Japan (36, 2, p. 240) Article based on AIAA Paper 97-3663 ISBN 1-56347-235-X A99-029 Base Flow Predictions for a Lightsat Launcher at Su- A99-043 Mars Pathfinder Entry, Descent, and Landing Re- personic Speeds. M. Serpico, A. Schettino, and A. Ciucci, Centro construction. David A. Spencer, Jet Propulsion Laboratory, Cal- Italiano Ricerche Aerospaziali, Italy; and D. Faiconi and M. Fab- ifornia Institute of Technology; Robert C. Blanchard and Robert D. rizi, Fiat Avio Comprensorio BPD, Italy (36, 2, p. 247) Article Braun, NASA Langley Research Center, and Pieter H. Kallemeyn and Sam W. Thurman, Jet Propulsion Laboratory, California Insti- A99-030 Grooves Effect on Lift: Data Correlation and Pre- tute of Technology (36, 3, p. 357) Article diction for Kinetic Energy Projectiles. Ameer G. Mikhail, U.S. Army Research Laboratory (36, 2, p. 255) Article based on AIAA A99-044 Prediction and Validation of Mars Pathfinder Hyper- Paper 98-0671 sonic Aerodynamic Database. Peter A. Gnoffo, Robert D. Braun, K. James Weilmuenster, Robert A. Mitcheltree, Walter C. Enge- A99-031 Reynolds Number Effects on Low-Speed Aerody- lund, and Richard W. Powell, NASA Langley Research Center (36, namics of a Hypersonic Configuration. G. Neuwerth, U. Peiter, 3, p. 367) Article based on AIAA Paper 98-2445 F. Decker, and D. Jacob, Technical University of Aachen, Germany (36, 2, p. 265) Article based on AIAA Paper 98-1578 ISBN 1- A99-045 Mars Pathfinder Heatshield Design and Flight Expe- 56347-266-X rience. William H. Willcockson, Lockheed Martin Astronautics A99-032 Ceramics Catalysis Evaluation at High Tempera- (36, 3, p. 374) Article ture Using Thermal and Chemical Approaches. M. J. H. A99-046 Mars Pathfinder Entry Temperature Data, Aerother- Balat, M. Czerniak, and J. M. Badie, Centre National de la Re- mal Heating, and Heatshield Material Response. Frank S. Mi- cherche Scientifique, France (36, 2, p. 273) Article based on los, and Y.-K. Chen, NASA Ames Research Center, William M. AIAA Paper 97-2589 Congdon, Applied Research Associates, Inc.; and Janine M. Thorn- A99-033 Technology of Automated Rendezvous and Capture ton, Lockheed Martin Astronautics (36, 3, p. 380) Article based on in Space. Michael E. Polites, NASA Marshall Space Flight Center AIAA Paper 98-268 1 (36, 2, p. 280) Article A99-047. Aerodynamics of the Mars Microprobe Entry Vehi- A99-034 Angular Motion Effects on Kinetic Energy Projectile cles. R. A. Mitcheltree, J. N. Moss, F. M. Cheatwood, F. A. Performance. Edward M. Schmidt, U.S. Army Research Labora- Greene, and R. D. Braun, NASA Langley Research Center (36, 3, p. tory (36, 2, p. 292) Engineering Note 392) Article based on AIAA Paper 97-3658 ISBN 1-56347-235-X A99-035 Numerical Study of Hypersonic Rarefied-Gas A99-048 Direct Simulation Monte Carlo Calculations of Aero- Flows About a Torus. Vladimir V. Riabov, University of New thermodynamics for Mars Microprobe Capsules. James N. Hampshire (36, 2, p. 293) Engineering Note based on AIAA Pa- Moss, Richard G. Wilmoth, and Joseph M. Price, NASA Langley per 98-0778 Research Center, (36, 3, p. 399) Article A99-036 Analysis of Galileo Probe Heatshield Ablation and A99-049 Aerothermal Heating Predictions for Mars Micro- Temperature Data. F. S. Milos, Y.-K. Chen, and T. H. Squire, probe. R. A. Mitcheltree, M. DiFulvio, T. J. Horvath, and R. D. NASA Ames Research Center, and R. A. Brewer, Lockheed Martin Braun, NASA Langley Research Center (36, 3, p. 405) Article based Missiles and Space Co. (36, 3, p. 298) Article based on AIAA Paper on AIAA Paper 98-0170 97-2480 A99-050 Mars Microprobe Entry-to-Impact Analysis. Robert A99-037. Mars Global Surveyor: Aerobraking Mission Over- D. Braun, Robert A. Mitcheltree, and F. McNeil Cheatwood, NASA view. Daniel T. Lyons, Joseph G. Beerer, Pasquale Esposito, and Langley Research Center (36, 3, p. 412) Article M. Daniel Johnston, Jet Propulsion Laboratory, California Insti- tute of Technology; and William H. Willcockson, Lockheed Martin A99-051 Mars Polar Lander Aerothermodynamic and Entry Astronautics (36, 3, p. 307) Article Dispersion Analysis. Eric M. Queen, F. McNeil Cheatwood, Ri- chard W. Powell, and Robert D. Braun, NASA Langley Research A99-038 Rarefied Aerothermodynamic Predictions for Mars Center; and C. Thomas Edquist, Lockheed Martin Astronautics (36, Global Surveyor. R. G. Wilmoth, D. F. Rault, F. M. Cheatwood, 3, p. 421) Article and W. C. Engelund, NASA Langley Research Center; and R. W. Shane, George Washington University (36, 3, p. 314) Article A99-052 Aerodynamics of the Stardust Sample Return Capsule. R. A. Mitcheltree, R. G. Wilmoth, F. M. Cheatwood, G. J. Brauck- A99-039 Application of Accelerometer Data to Mars Global mann, and F. A. Greene, NASA Langley Research Center (36, 3, p. Surveyor Aerobraking Operations. R. H. Tolson, G. M. Keating, 429) Article based on AIAA Paper 97-2304 ISBN 1-56347-232-5 G. J. Cancro, J. S. Parker, S. N. Noll, and B. L. Wilkerson, George Washington University and NASA Langley Research Center (36, 3, A99-053 Low-Density Aerodynamics of the Stardust Sample p. 323) Article Return Capsule. Richard G. Wilmoth, Robert A. Mitcheltree, and 934 J. SPACECRAFT, VOL. 36, NO.6: 1999 INDEX James N. Moss, NASA Langley Research Center (36, 3, p. 436) Ar- space Laboratory, Japan; and Tatsushi Izumi, National Space De- ticle based on AIAA Paper 97-2510 velopment Agency, Japan (36, 4, p. 554) Article A99-054 Aerothermodynamics of the Stardust Sample Return A99-070 Particle Environment Surrounding the Midcourse Capsule. Dave Olynick, Y.-K. Chen, and Michael E. Tauber, Space Experiment Spacecraft. Gary E. Galica, B. David Green, NASA Ames Research Center (36, 3, p. 442) Article based on AIAA and Mark T. Boies, Physical Sciences, Inc.; and O. Manuel Uy, Paper 98-0167 David M. Silver, and Richard C. Benson, Johns Hopkins Univer- sity, Applied Physics Laboratory (36, 4, p. 561) Article A99-055 Entry Dispersion Analysis for the Stardust Comet Sample Return Capsule. Prasun N. Desai, Robert A. Mitcheltree, A99-071 Detailed Simulation of Surface Chemistry Leading to and F. McNeil Cheatwood, NASA Langley Research Center (36, 3, p. Spacecraft Glow. Daniel P. Karipides and Iain D. Boyd, Cornell 463) Article based on AIAA Paper 97-3812 ISBN 1-56347-235-X University; and George E. Caledonia, Physical Sciences, Inc. (36, 4, p. 566) Article A99-056 Stardust Sample Return Capsule Design Experience. William H. Willcockson, Lockheed Martin Aeronautics (36, 3, p. A99-072 Plasma Electron Density Measurement Around Hy- 470) Article based on AIAA Paper 98-2854 personic Flight Experiment Vehicle. Takeshi Ito and Ryojji Takaki, National Aerospace Laboratory, Japan; and Ken Teraoka, A99-057 Ablation and Thermal Response Program for National Space Development Agency, Japan (36, 4, p. 573) Article Spacecraft Heatshield Analysis. Y.-K. Chen and Frank S. Mi- based on AIAA Paper 98-2480 los, NASA Ames Research Center (36, 3, p. 475) Article based on AIAA Paper 98-0273 A99-073 Electrical Breakdown of Anodized Coatings in Low- Density Plasmas. J. T. Galofaro, NASA Lewis Research Center, C. 499-058 Elastic Response of Generic Space Vehicle Having V. Doreswamy, Tuskegee University, B. V. Vayner, Ohio Aero- Degraded Interstage Joints. A. Joshi, /ndian Institute of Technol- space Institute, and D. B. Snyder and D. C. Ferguson, NASA Lewis ogy, India (36, 3, p. 484) Engineering Note Research Center (36, 4, p. 579) Article A99-059 Aerodynamics of a Spinning Cylinder in Rarefied A99-074 Postfire Short Circuit Phenomena of Electroexplo- Gas Flows. Vladimir V. Riabov, University of New Hampshire sive Initiators. Lien C. Yang, TRW Systems & Information Tech- (36, 3, p. 486) Engineering Note nology Group (36, 4, p. 586) Article A99-060 Viscous Multiblock Simulations of Axisymmetric A99-075 Friction Model of a Revolute Joint for a Precision De- Launch Vehicle Flows. Jodo L. F. Azevedo, /nstituto de Aerondu- pioyable Spacecraft Structure. M. Roman Hachkowski, Ray- tica e Espaco, Brazil; Daniel Strauss, Instituto Tecnoldgico de theon Optical Systems, Lee D. Peterson, University of Colorado; Aeronautica, Brazil; and Marcello A. S. Ferrari, Instituto de and Mark S. Lake, NASA Langley Research Center (36, 4, p. 591) Aeronautica e Espaco, Brazil (36, 4, p. 489) Article Article based on AIAA Paper 96-1472 ISBN 1-56347-209-0 499-061 Optimal Artificially Blunted Leading-Edge Airfoils A99-076 Self-Assembling Transfer Vehicles for Human Mars for Enhanced Aerothermodynamic Performance. Anurag Missions. Benjamin Donahue, Boeing Space Systems (36, 4, p. Gupta and Stephen M. Ruffin, Georgia Institute of Technology (36, 599) Engineering Note based on AIAA Paper 94-2761 4, p. 499) Article A99-077 Effects of Shock Wave Impingement on Supersonic 499-062 Atmospheric Reentry Demonstrator Balloon Flight Film Cooling. Kenichi Takita and Goro Masuya, Tohoku Univer- Test. Maurizio De Giorgis, Giorgio Borriello, Andrea Allasio, sity, Japan (36, 4, p. 602) Engineering Note and Raffaele Vavala, Alenia, Italy; Thierry Leveugle, Aerospa- tiale, France, and Orazio Cosentino, /talian Space Agency (36, 4, A99-078 Mini/Micro Shuttles with Hypergolic Noncryogenic p. 507) Article Liquid Rocket Bipropellant. Frederick W. Boltz, NASA Ames Re- search Center (36, 4, p. 605) Engineering Note 499-063 Payload Fairing Separation Dynamics. S-C. Cheng, The Aerospace Corporation (36, 4, p. 511) Article A99-079 Engineering-, Intermediate-, and High-Level Aero- dynamic Prediction Methods and Applications. Marnix F. E. 499-064 Simple Analytical Model for Parametric Studies of Dillenius, Daniel J. Lesieutre, Martin C. Hegedus, Stanley C. Per- Hypersonic Waveriders. Ryan P. Starkey and Mark J. Lewis, kins Jr., John F. Love, and Teresa O. Lesieutre, Nielsen Engineer- University of Maryland (36, 4, p. 516) Article ing and Research, Inc. (36, 5, p. 609) Survey Paper 499-065 Aeroelastic Effects on the Roll Characteristics of a A99-080 Asymmetric Divert Jet Performance of a Supersonic Wraparound Fin Projectile. Seung-Kil Paek and In Lee, Korea Missile: Computational and Experimental Comparisons. B. Advanced Institute of Science and Technology (36, 4, p. 524) Article Srivastava, Raytheon Company (36, 5, p. 621) Article 499-066 Forces for Rolling and Asymmetric Pinching of Pres- A99-081 Application of the 1998 Version of the Aeroprediction surized Cylindrical Tubes. J. P. Fay and C. R. Steele, Stanford Code . F.G. Moore, R. M. McInville, and T. C. Hymer, U.S. Naval University (36, 4, p. 531) Article Surface Warfare Center (36, 5, p. 633) Article 499-067 Fracture Control of Space Flight Structures and A99-082 Performance Study of a Power Law Starbody. John Pressure Vessels. S. Sutharshana, Angeles Crest Engineering, W. Sabean and Mark J. Lewis, University of Maryland; and David Inc.; J. B.C hang, The Aerospace Corporation, and M. C. Lou, Jet Mee and Allan Paull, University ofQ ueensland, Australia (36, 5, p. Propulsion Laboratory, California Institute of Technology (36, 4, 646) Article p. 538) Article A99-083 Power Law Shapes for Leading-Edge Blunting with 499-068 Low-Thrust Trajectory Optimization Based on Ep- Minimal Shock Standoff. Timothy F. O’Brien and Mark J. Lewis, och Eccentric Longitude Formulation. Jean Albert Kechichian, University of Maryland (36, 5, p. 653) Article The Aerospace Corporation (36, 4, p. 543) Article A99-084 Low-Speed Aerodynamics of a Planetary Entry Cap- 499-069 Automatic Landing Flight Experiment Flight Simu- sule. Frank Y. Wang, Ozgiir Karatekin, and Jean-Marc Charbon- lation Analysis and Flight Testing. Toshikazu Motoda, nier, von Karman Institute for Fluid Dynamics, Belgium (36, 5, p. Yoshikazu Miyazawa, and Kazutoshi Ishikawa, National Aero- 659) Article