Table Of Content

JOURNAL OF SPACECRAFT AND ROCKETS Vol. 34, No. 6, November—December 1997 1997 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 853-857, each technical paper is listed under a maximum of three 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, pages 857 and 858, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 859-863, lists all papers by their unique code numbers. This list- ing 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 “CP” or conference volume 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 1997, that paper also will appear in the Chronological Index. Authors of Comments also are listed in the Author Index. The Book Review Index, page 864, lists the books reviewed during 1997, the author, publisher, and reviewer, and the volume, issue number, and page on which the review appeared. Subject Index Aircraft Technology, Conventional, Cabin Environment, Crew Training, and Life Fluid Dynamics STOL/VTOL Support Aeroacoustics Aerodynamics Air-Quality Monitoring and Detection of Air Contamination in an Enclosed Environment Unsteady Flowfield and Cavity Acoustics of the Rarefied-Flow Transition Regime Orbiter Aero- A97-079 Stratospheric Observatory for Infrared Astron- dynamic Acceleration Flight Measurements omy A97-057 Configuration Design A97-001 Boundary Layers and Heat Transfer—Laminar Three-Dimensional Aerodynamic Shape Optimi- Three-Dimensional Aerodynamic Shape Optimi- zation Using Genetic and Gradient Search Al- zation Using Genetic and Gradient Search Al- Comparison Between Numerical and Experi- gorithms A97-005 gorithms A97-005 mental Results on Different Hermes Elevon Large-Scale Roughness Influence on Turbulent Shapes A97-042 Hypersonic Boundary Layers Approaching Flight Mechanics Three-Dimensional Hypersonic Laminar Bound- Compression Corners A97-010 ary-Layer Computations for Transition Exper- Computational Fluid Dynamics Simulation of Effects of Severed Tethers in Space A97-034 iment Design A97-065 Improved Matched Asymptotic Solutions for Turbulent Waverider Flowfield with Sideslip A97-011 Three-Dimensional Atmospheric Skip Trajec- Boundary Layers and Heat Transfer— Numerical Analysis of a Swept-Fin Missile tories A97-076 Turbulent Calculation of Pitch Damping for a Flared Pro- A97-021 jectile A97-086 Large-Scale Roughness Influence on Turbulent Effects of Severed Tethers in Space Hypersonic Boundary Layers Approaching A97-034 Flight Operations Compression Corners A97-010 Unsteady Flowfield and Cavity Acoustics of the Comparison Between Numerical and Experi- Stratospheric Observatory for Infrared Astron- Effects of Severed Tethers in Space A97-034 mental Results on Different Hermes Elevon omy A97-057 Aerodynamic Characteristics Evaluation of Hy- Performance Shapes A97-042 personic Flight Experiment Vehicle Based on Mission Performance and Design Sensitivities of Boundary-Layer Stability and Transition Flight Data A97-072 Air-Breathing Hypersonic Launch Vehicles Navier-Stokes Computations of Finned Kinetic A97-022 Three-Dimensional Hypersonic Laminar Bound- Energy Projectile Base Flow A97-073 ary-Layer Computations for Transition Exper- Calculation of Pitch Damping for a Flared Pro- Simulation iment Design A97-065 jectile A97-086 Effect of Isolated Roughness Elements on Bound- Computational Analysis and Validation for Lat- Extreme Value Flight Duration Analysis of Four- ary-Layer Transition for Shuttle Orbiter eral Jet Controlled Missiles A97-091 Engine Spacecraft A97-063 A97-067 Analysis of Flowfields over Four-Engine DC-X Development of a Flight Article for a Hypersonic STOL/VTOL/STOVL Rockets A97-096 Boundary-Layer Experiment A97-094 Base Cavity Effects on the Aerodynamic Charac- Simulation of an Aerospace Vehicle Pitch-Over Enthalpy Effects on Hypervelocity Boundary- teristics of a Hypersonic Flared Projectile Maneuver A97-037 Layer Transition: Ground Test and Flight Data A97-115 A97-095 Aerospace Plane Energy Computational Fluid Dynamics Mission Performance and Design Sensitivities of Conservation Rarefied-Flow Transition Regime Orbiter Aero- Air-Breathing Hypersonic Launch Vehicles dynamic Acceleration Flight Measurements Thermal Sensitivity Analysis of Spacecraft Bat- A97-022 tery A97-059 A97-001 Periodic Optimal Cruise for a Hypersonic Vehi- Computational Fluid Dynamics Simulation of cle with Constraints A97-023 Photovoltaic Power Turbulent Waverider Flowfield with Sideslip Aerodynamic Characteristics Evaluation of Hy- A97-011 personic Flight Experiment Vehicle Based on Model of Plasma Contactor Performance Damped Oscillations of a Liquid/Gas Surface Flight Data A97-072 A97-128 upon Step Reduction in Gravity A97-015 853 854 J. SPACECRAFT, VOL. 34, NO.6: 1997 INDEX Numerical Analysis of a Swept-Fin Missile Experimental Rarefied Aerodynamic Forces at Zero-Lift Drag Characteristics of Afterbodies A97-021 Hypersonic Conditions over 70-Degree Blunt- with a Square Base A97-045 Structure of a Supersonic Three-Dimensional ed Cone A97-112 Structure of a Supersonic Three-Dimensional Cylinder/Offset-Flare Turbulent Interaction Experimental Rarefied Heat Transfer at Hyper- Cylinder/Offset-Flare Turbulent Interaction A97-046 sonic Conditions over 70-Degree Blunted A97-046 Three-Dimensional Hypersonic Laminar Bound- Cone A97-113 ary-Layer Computations for Transition Exper- Control Effectiveness of a Jet-Slender Body Shock Waves and Detonations iment Design A97-065 Combination at Hypersonic Speeds Fin Leading-Edge Sweep Effect on Shock—Shock Fluid Dynamics of Hypersonic Forward-Facing A97-118 Interaction at Mach 6 A97-066 Cavity Flow A97-068 Experimental Study of Cone-Derived Waverid- Experimental Study of Cone-Derived Waverid- Inlet, Nozzle, Diffuser, and Channel Flows ers at Mach 5.5 A97-069 ers at Mach 5.5 A97-069 High-Enthalpy Aerothermodynamics of a Mars Fluid Dynamics of Hypersonic Forward-Facing Supersonic Flow Entry Vehicle Part 1: Experimental Results Cavity Flow A97-068 A97-070 Flow Confluence Past a Jet-On Axisymmetric Numerical Investigation of Supersonic Base High-Enthalpy Aerothermodynamics of a Mars Afterbody A97-092 Flow with Base Bleed A97-009 Entry Vehicle Part 2: Computational Results Turbulent Flow Structure Characterization of A97-071 Jets, Wakes, and Viscid-Inviscid Flow Angled Injection into a Supersonic Crossflow Navier-Stokes Computations of Finned Kinetic Interactions A97-029 Energy Projectile Base Flow A97-073 Structure of a Supersonic Three-Dimensional Transonic Flow Simulation for a Bulbous Heat Numerical Investigation of Supersonic Base Cylinder/Offset-Flare Turbulent Interaction Shield A97-084 Flow with Base Bleed A97-009 A97-046 Calculation of Pitch Damping for a Flared Pro- Computational Fluid Dynamics Simulation of Optimization of a Dual-Mixture-Ratio Hydro- jectile A97-086 Turbulent Waverider Flowfield with Sideslip gen-Fuel Rocket A97-089 High-Fidelity Thermal Protection System Sizing A97-011 Flow Confluence Past a Jet-On Axisymmetric of Reusable Launch Vehicle A97-090 Turbulent Flow Structure Characterization of Afterbody A97-092 Computational Analysis and Validation for Lat- Angled Injection into a Supersonic Crossflow Transonic Flow eral Jet Controlled Missiles A97-091 A97-029 Analysis of Flowfields over Four-Engine DC-X Effect of Riblets on Axisymmetric Base Pressure Zero-Lift Drag Characteristics of Afterbodies Rockets A97-096 A97-038 with a Square Base A97-045 Validation Database for Propulsion Computa- Fin Leading-Edge Sweep Effect on Shock—Shock Transonic Flow Simulation for a Bulbous Heat tional Fluid Dynamics A97-099 Interaction at Mach 6 A97-066 Shield A97-084 Hypersonic Thermal Environment of a Proposed Navier-Stokes Computations of Finned Kinetic Single-Stage-to-Stage-Orbit Vehicle A97-109 Energy Projectile Base Flow A97-073 Unsteady Flows Base Cavity Effects on the Aerodynamic Charac- teristics of a Hypersonic Flared Projectile Plasmadynamics and MHD Hammerhead Wake Effects on Elastic Vehicle Dynamics A97-020 A97-115 Navier-Stokes Predictions of Pitch Damping for Plasma and Aerothermal Measurements on a Hy- Simulation of an Aerospace Vehicle Pitch-Over Axisymmetric Projectiles A97-117 pervelocity Re-Entry Vehicle A97-093 Maneuver A97-037 Unsteady Flowfield and Cavity Acoustics of the Hydrodynamics Rarefied Flows Stratospheric Observatory for Infrared Astron- omy A97-057 Damped Oscillations of a Liquid/Gas Surface Rarefied-Flow Transition Regime Orbiter Aero- Fluid Dynamics of Hypersonic Forward-Facing dynamic Acceleration Flight Measurements upon Step Reduction in Gravity A97-015 Cavity Flow A97-068 A97-001 Hypersonic Flow Monte Carlo Modeling and Analysis of Pressure Vortices Sensor Measurements During Suborbital Flight Three-Dimensional Aerodynamic Shape Optimi- A97-012 Zero-Lift Drag Characteristics of Afterbodies zation Using Genetic and Gradient Search Al- Aerodynamic Forces and Moments for a Re-Entry with a Square Base A97-045 gorithms A97-005 Module A97-025 Aerodynamic Forces and Moments for a Re-Entry Nocilla Model Parameters Obtained from Forces Wave Motion and Sloshing Module A97-025 Exerted on Surfaces by Molecular Beams Damped Oscillations of a Liquid/Gas Surface Comparison Between Numerical and Experi- A97-058 mental Results on Different Hermes Elevon Optimal Properties of Bodies of Revolution in upon Step Reduction in Gravity A97-015 Shapes A97-042 Continuum and Free Molecular Regimes Optimal Properties of Bodies of Revolution in A97-062 Guidance, Control, and Dynamics Continuum and Free Molecular Regimes Method of Basic Projectiles for Calculating Technology A97-062 Force Coefficients A97-083 Fin Leading-Edge Sweep Effect on Shock-Shock Aerodynamic Flight Measurements and Rar- Aircraft Dynamics Interaction at Mach 6 A97-066 efied-Flow Simulations of Mars Entry Vehi- Effect of Isolated Roughness Elements on Bound- cles A97-108 Method of Basic Projectiles for Calculating ary-Layer Transition for Shuttle Orbiter Experimental Rarefied Density Flowfields at Hy- Force Coefficients A97-083 A97-067 personic Conditions over 70-Degree Blunted Experimental Study of Cone-Derived Waverid- Cone A97-111 Astrodynamics ers at Mach 5.5 A97-069 Experimental Rarefied Aerodynamic Forces at Exact Design of Partial Coverage Satellite Con- Aerodynamic Characteristics Evaluation of Hy- Hypersonic Conditions over 70-Degree Blunt- stellations over Oblate Earth A97-004 personic Flight Experiment Vehicle Based on ed Cone A97-112 Trajectory Options to Pluto via Gravity Assists Flight Data A97-072 Experimental Rarefied Heat Transfer at Hyper- from Venus, Mars, and Jupiter A97-053 Method of Basic Projectiles for Calculating sonic Conditions over 70-Degree Blunted Improved Matched Asymptotic Solutions for Force Coefficients A97-083 Cone A97-113 Three-Dimensional Atmospheric Skip Trajec- Plasma and Aerothermal Measurements on a Hy- tories A97-076 pervelocity Re-Entry Vehicle A97-093 Separated Flows Navigating Galileo at Jupiter Arrival | A97-077 Enthalpy Effects on Hypervelocity Boundary- Layer Transition: Ground Test and Flight Data Numerical Investigation of Supersonic Base Dynamics A97-095 Flow with Base Bleed A97-009 Hypersonic Thermal Environment of a Proposed Hammerhead Wake Effects on Elastic Vehicle Individual Components of the Yaw Damping Single-Stage-to-Stage-Orbit Vehicle Dynamics A97-020 Sum: Implementation for Tumbling Bodies A97-109 Effect of Riblets on Axisymmetric Base Pressure A97-087 Experimental Rarefied Density Flowfields at Hy- A97-038 Damped Gyroscopic Modes of Spinning Teth- personic Conditions over 70-Degree Blunted Wind-Tunnel Test of Flow Through Mars Path- ered Space Vehicles with Flexible Booms Cone A97-111 finder Lander A97-041 A97-102 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX 855 Engine Control Structural Control Launch Vehicle and Missile (LV/M) Technology Mixture-Ratio Control to Improve Hydrogen- Symmetric Motion Control for Adaptive Struc- Fuel Rocket Performance A97-030 ture Based Construction of Large Space Struc- Aerodynamics Optimization of a Dual-Mixture-Ratio Hydro- tures A97-016 gen-Fuel Rocket A97-089 Aerodynamics for a Winged, Circular-Body, Sin- System Identification gle-Stage-to-Orbit Spacecraft Configuration Flight Mechanics A97-006 Air-Quality Monitoring and Detection of Air New Semiempirical Model for Wing-Tail Inter- Aerodynamic Considerations for Kinetic Energy Contamination in an Enclosed Environment ference A97-007 Projectiles A97-040 A97-079 Nonlinear Aeroprediction Methodology for Roll Six-Degree-of-Freedom Entry Dispersion Anal- Position of 45 Degrees A97-008 ysis for the METEOR Recovery Module Trajectory Optimization Large-Scale Roughness Influence on Turbulent A97-051 Hypersonic Boundary Layers Approaching Periodic Optimal Cruise for a Hypersonic Vehi- Flight Control Augmentors for Aft-Center-of- Compression Corners A97-010 cle with Constraints A97-023 Gravity Launch Vehicles A97-075 Numerical Analysis of aS wept-Fin Missile Aerodynamic Considerations for Kinetic Energy Navier-Stokes Predictions of Pitch Damping for A97-021 Axisymmetric Projectiles A97-117 Projectiles A97-040 Optimal Properties of Bodies of Revolution in Extracting Meteorological Data from Projectile Six-Degree-of-Freedom Entry Dispersion Anal- Continuum and Free Molecular Regimes ysis for the METEOR Recovery Module Trajectory A97-119 A97-062 A97-051 Transonic Flow Simulation for a Bulbous Heat Launch Vehicle Guidance and Control Six-Degree-of-Freedom Trajectory Targeting and Shield A97-084 Optimization for Titan Launch Vehicles Methods for Distributing Semiempirical, Nonlin- Six-Degree-of-Freedom Trajectory Targeting and A97-052 ear, Aerodynamic Loads on Missile Compo- Optimization for Titan Launch Vehicles Heliospheric Boundary Exploration Using lon nents A97-116 A97-052 Propulsion Spacecraft A97-056 Navier-Stokes Predictions of Pitch Damping for Maximum-Payload Transfers to Geosynchronous Axisymmetric Projectiles A97-117 Missile Dynamics Orbit Using Arcjet Thrusters A97-064 Control Effectiveness of a Jet-Slender Body Extracting Meteorological Data from Projectile Combination at Hypersonic Speeds Aerodynamic Considerations for Kinetic Energy Projectiles A97-040 Trajectory A97-119 A97-118 Configuration Design Navigation Interdisciplinary Topics Nonlinear Aeroprediction Methodology for Roll Navigating Galileo at Jupiter Arrival Aerospace Technology Utilization Position of 45 Degrees A97-008 A97-077 Mission Performance and Design Sensitivities of Efficient Approach for International Space Station Development and Operation of a Microgravity Air-Breathing Hypersonic Launch Vehicles Global Positioning System Multipath Analysis Furnace System for Sintering Experiments A97-022 A97-132 A97-014 Payload Capability of Kerosene-Fueled Mini Optimization Techniques Shuttle A97-107 Analytical and Numerical Methods Methods for Distributing Semiempirical, Nonlin- Periodic Optimal Cruise for a Hypersonic Vehi- ear, Aerodynamic Loads on Missile Compo- cle with Constraints A97-023 Collaborative Approach to Launch Vehicle De- nents A97-116 sign A97-074 Collaborative Approach to Launch Vehicle De- sign A97-074 Efficient Calculation of a Jitter/Stability Metric Launch Vehicle and Sounding Recket Systems A97-082 Hammerhead Wake Effects on Elastic Vehicle Pointing Systems Individual Components of the Yaw Damping Dynamics A97-020 Sum: Implementation for Tumbling Bodies Performance of Diamond-Coated Silicon Nitride A97-087 Six-Degree-of-Freedom Trajectory Targeting and Bearings A97-106 Optimization for Titan Launch Vehicles A97-052 Atmospheric and Space Sciences Spacecraft Dynamics Collaborative Approach to Launch Vehicle De- sign A97-074 Planning Spiral Motions of Nonholonomic Free- Experimental Investigation of Spacecraft In- Flight Control Augmentors for Aft-Center-of- Flight Disturbances and Dynamic Response Flying Space Robots A97-019 Gravity Launch Vehicles A97-075 A97-028 Experimental Investigation of Spacecraft In- Analysis of Flowfields over Four-Engine DC-X Flight Disturbances and Dynamic Response Contamination Experiments in the Midcourse Rockets A97-096 A97-028 Space Experiment A97-031 Tripropellant Engine Option Comparison for Preflight Testing and Flight Performance of the Aerodynamic Flight Measurements and Rar- Single Stage to Orbit A97-098 OEDIPUS-C Tether Force Sensor A97-080 efied-Flow Simulations of Mars Entry Vehi- Payload Capability of Kerosene-Fueled Mini Efficient Calculation of a Jitter/Stability Metric cles A97-108 Shuttle A97-107 A97-082 Modeling the Multiphase Atmospheric Chemis- Computational Comparison of Debris Cloud try of Launch Clouds A97-121 Missile Systems Models A97-100 Damped Gyroscopic Modes of Spinning Teth- Reliability, Maintainability, and Logistics New Semiempirical Model for Wing-Tail Inter- ered Space Vehicles with Flexible Booms Support ference A97-007 Nonlinear Aeroprediction Methodology for Roll A97-102 Extreme Value Flight Duration Analysis of Four- Position of 45 Degrees A97-008 Spacecraft Guidance and Control Engine Spacecraft A97-063 Preliminary Design of aH ybrid Propulsion Mul- Some Correlation Techniques for Environmcii- timission Missile System A97-026 Planning Spiral Motions of Nonholonomic Free- tally Induced Anomalies Analysis Computational Analysis and Validation for Lat- Flying Space Robots A97-019 A97-103 eral Jet Controlled Missiles A97-091 Efficient Calculation of a Jitter/Stability Metric Methods for Distributing Semiempirical, Nonlin- A97-082 Research Facilities and Instrumentation ear, Aerodynamic Loads on Missile Compo- Computational Comparison of Debris Cloud nents A97-116 Models A97-100 Steady-State and Frequency Response of a Thin- Film Heat Flux Gauge A97-123 Propulsion and Propellant Systems State Estimation Sensor Systems Mixture-Ratio Control to Improve Hydrogen- Air-Quality Monitoring and Detection of Air Fuel Rocket Performance A97-030 Contamination in au Enclosed Environment Steady-State and Frequency Response of a Thin- Functional Performance of Pyrovalves A97-079 Film Heat Flux Gauge A97-123 A97-060 856 J. SPACECRAFT, VOL. 34, NO.6: 1997 INDEX Tripropellant Engine Option Comparison for Aerodynamic Flight Measurements and Rar- Space Experiments Single Stage to Orbit A97-098 efied-Flow Simulations of Mars Entry Vehi- Payload Capability of Kerosene-Fueled Mini cles A97-108 Radiation-Induced Anomalies in Satellites Shuttle A97-107 Experimental Rarefied Density Flowfields at Hy- A96-142 personic Conditions over 70-Degree Blunted Monte Carlo Modeling and Analysis of Pressure Testing, Flight and Ground Cone A97-111 Sensor Measurements During Suborbital Flight Experimental Rarefied Aerodynamic Forces at A97-012 Functional Performance of Pyrovalves Hypersonic Conditions over 70-Degree Blunt- Flight Data Analysis for the Photovoltaic Array A97-060 ed Cone A97-112 Space Power Plus Diagnostics Experiment Experimental Rarefied Heat Transfer at Hyper- A97-013 Thermal Protection Systems sonic Conditions over 70-Degree Blunted Development and Operation of a Microgravity Cone A97-113 Furnace System for Sintering Experiments Film Cooling Effect of Hydrogen on Cylinder in A97-014 Supersonic Airflow A97-044 Aerobraking Flight Mechanics Low-Earth-Orbit Micrometeoroid and Debris In- vestigations A97-017 Propulsion Mars-Jupiter Aerogravity Assist Trajectories for Astronaut-Induced Disturbances in Microgravity High-Energy Missions A97-002 A97-036 Improved Matched Asymptotic Solutions for Cassini/Huygens Science Instruments, Space- Electric and Advanced Space Propulsion Three-Dimensional Atmospheric Skip Trajec- craft, and Mission A97-078 Life Extension Strategies for Shuttle-Deployed tories A97-076 Transient Potential Modification of Large Space- Small Satellites Using Pulsed Plasma Thrust- craft Due to Electron Emissions A97-101 ers A97-122 Humans in Space/Life Support Systems, EVA Neutral Orbital Altitude Density Effects on the Model of Plasma Contactor Performance International Space Station A97-127 Astronaut-Induced Disturbances in Microgravity A97-128 A97-036 Space Processing Engine Performance Internal Effects Model for Spacecraft Modules Perforated by Orbital Debris A97-050 Development and Operation of a Microgravity Extreme Value Flight Duration Analysis of Four- International Space Station Electromagnetic En- Furnace System for Sintering Experiments Engine Spacecraft A97-063 vironment A97-131 A97-014 Optimization of a Dual-Mixture-Ratio Hydro- Some Correlation Techniques for Environmen- gen-Fuel Rocket A97-089 Landers tally Induced Anomalies Analysis Tripropellant Engine Option Comparison for A97-103 Single Stage to Orbit A97-098 Aerodynamics for a Winged, Circular-Body, Sin- gle-Stage-to-Orbit Spacecraft Configuration Space Systems Environmental Effects A97-006 Wind-Tunnel Test of Flow Through Mars Path- Radiation-Induced Anomalies in Satellites Solid Rocket Motor Exhaust Model for Alumina finder Lander A97-041 A96-142 Particles in the Stratosphere A97-047 Lunar Landing Craft for the Reusable Launch Flight Data Analysis for the Photovoltaic Array Predicted Optical Characteristics of Solid Rocket Vehicle and Shuttle Vehicles A97-085 Space Power Plus Diagnostics Experiment Motor Exhaust in the Stratosphere A97-013 A97-048 Mission Design and Analysis Low-Earth-Orbit Micrometeoroid and Debris In- Effects of Launch Vehicle Emissions in the vestigations A97-017 Stratosphere A97-120 Exact Design of Partial Coverage Satellite Con- Cassini/Huygens Science Instruments, Space- stellations over Oblate Earth A97-004 craft, and Mission A97-078 Hybrid Rocket Engines Trajectory Options to Pluto via Gravity Assists Evolution of Secondary Electron Emission Char- from Venus, Mars, and Jupiter A97-053 acteristics of Spacecraft Surfaces A97-088 Preliminary Design of aH ybrid Propulsion Mul- Heliospheric Boundary Exploration Using lon Transient Potential Modification of Large Space- timission Missile System A97-026 Propulsion Spacecraft A97-056 craft Due to Electron Emissions A97-101 Maximum-Payload Transfers to Geosynchronous Systems Engineering Trades for the IRIDIUM® Injector Design and Characterization Orbit Using Arcjet Thrusters A97-064 Constellation A97-104 Validation Database for Propulsion Computa- Cassini/Huygens Science Instruments, Space- Cost per Billable Minute Metric for Comparing tional Fluid Dynamics A97-099 craft, and Mission A97-078 Satellite Systems A97-130 Lunar Landing Craft for the Reusable Launch Liquid Rocket Motors and Missile Systems Vehicle and Shuttle Vehicles A97-085 Spacecraft Attitude Determination Computational Comparison of Debris Cloud Mixture-Ratio Control to Improve Hydrogen- Models A97-100 Moon-Sun Attitude Sensor A97-055 Performance of Diamond-Coated Silicon Nitride Fuel Rocket Performance A97-030 Systems Engineering Trades for the IRIDIUM® Bearings A97-106 Constellation A97-104 Solid Rocket Motors and Missile Systems Life Extension Strategies for Shuttle-Deployed Position of Propellant in Teardrop Tank Sys- tems A97-124 Small Satellites Using Pulsed Plasma Thrust- Solid Rocket Motor Exhaust Model for Alumina Neutral Orbital Altitude Density Effects on the ers A97-122 Particles in the Stratosphere A97-047 International Space Station A97-127 Neutral Orbital Altitude Density Effects on the Predicted Optical Characteristics of Solid Rocket International Space Station A97-127 Efficient Approach for International Space Station Motor Exhaust in the Stratosphere Cost per Billable Minute Metric for Comparing Global Positioning System Multipath Analysis A97-048 A97-132 Satellite Systems A97-130 Validation Database for Propulsion Computa- tional Fluid Dynamics A97-099 Mission Trajectories (Earth and Spacecraft Communication Interplanetary) Systems Engineering Trades for the IRIDIUM® Space Technology Constellation A97-104 Mars-Jupiter Aerogravity Assist Trajectories for International Space Station Electromagnetic En- Aerobraking Configurations/ High-Energy Missions A97-002 vironment A97-131 Aerothermodynamics Advanced Propulsion for Geostationary Orbit In- Efficient Approach for International Space Sta- sertion and North-South Station Keeping tion Global Positioning System Multipath Aerodynamic Forces and Moments for a Re-Entry A97-003 Module A97-025 Trajectory Options to Pluto via Gravity Assists Analysis A97-132 High-Enthalpy Aerothermodynamics of a Mars from Venus, Mars, and Jupiter A97-053 Spacecraft Contamination/Sterilization Entry Vehicle Part 1: Experimental Results Heliospheric Boundary Exploration Using lon A97-070 Propulsion Spacecraft A97-056 Contamination Experiments in the Midcourse High-Enthalpy Aerothermodynamics of a Mars Maximum-Payload Transfers to Geosynchronous Space Experiment A97-031 Entry Vehicle Part 2: Computational Results Orbit Using Arcjet Thrusters A97-064 Evolution of Secondary Electron Emission Char- A97-071 Navigating Galileo at Jupiter Arrival | A97-077 acteristics of Spacecraft Surfaces A97-088 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX 857 Spacecraft Data Sensing, Processing, and Damped Gyroscopic Modes of Spinning Teth- Dynamic Model for Global Positioning System Transmission ered Space Vehicles with Flexible Booms Block IIR Space Vehicle A97-054 A97-102 Moon—Sun Attitude Sensor A97-055 Spacecraft Launch Depressurization Loads Structural Finite Elements A97-125 Spacecraft Power Dynamic Model for Global Positioning System Spacecraft Test and Evaluation Block IIR Space Vehicle A97-054 Flight Data Analysis for the Photovoltaic Array Development of a Flight Article for a Hypersonic Space Power Plus Diagnostics Experiment Dynamic Model for Global Positioning System Boundary-Layer Experiment A97-094 A97-013 Block IIR Space Vehicle A97-054 Model of Plasma Contactor Performance Deployment Test Methods for a Large Deploy- Structural Optimization A97-128 able Mesh Reflector A97-126 U-Groove Aluminum Weld Strength Improve- Spacecraft Propulsion System Integration Spacecraft Thermal Management ment A97-018 Functional Performance of Pyrovalves High-Fidelity Thermal Protection System Sizing A97-060 of Reusable Launch Vehicle A97-090 Thermophysics and Heat Transfer Lunar Landing Craft for the Reusable Launch Vehicle and Shuttle Vehicles A97-085 Ablation, Pyrolysis, Thermal Decomposition Life Extension Strategies for Shuttle-Deployed Structural Mechanics and Materials and Degradation Small Satellites Using Pulsed Plasma Thrust- Flexible and Active Structures Galileo Probe Heat Shield Ablation Experiment ers A97-122 A97-110 Position of Propellant in Teardrop Tank Sys- Symmetric Motion Control for Adaptive Struc- tems A97-124 ture Based Construction of Large Space Struc- Aerothermodynamics/Thermal Protection tures A97-016 Spacecraft Radiation Protection Trajectory-Based Validation of the Shuttle Heat- Radiation-Induced Anomalies in Satellites Materials Structural Properties ing Environment A97-024 Film Cooling Effect of Hydrogen on Cylinder in A96-142 U-Groove Aluminum Weld Strength Improve- Supersonic Airflow A97-044 Some Correlation Techniques for Environmen- ment A97-018 Effect of Isolated Roughness Elements on Bound- tally Induced Anomalies Analysis —_A97-103 Cracking Characteristics of Dual-Wall Structures ary-Layer Transition for Shuttle Orbiter International Space Station Electromagnetic En- Following Simulated Orbital Debris Particle A97-067 vironment A97-131 Impact A97-049 High-Enthalpy Aerothermodynamics of a Mars Spacecraft Sensor Systems Structural Design Entry Vehicle Part 1: Experimental Results A97-070 Experimental Investigation of Spacecraft In- U-Groove Aluminum Weld Strength Improve- High-Enthalpy Aerothermodynamics of a Mars Flight Disturbances and Dynamic Response ment A97-018 Entry Vehicle Part 2: Computational Results A97-028 Cracking Characteristics of Dual-Wall Structures A97-071 Contamination Experiments in the Midcourse Following Simulated Orbital Debris Particle High-Fidelity Thermal Protection System Sizing Space Experiment A97-031 Impact A97-049 of Reusable Launch Vehicle A97-090 Wind-Tunnel Test of Flow Through Mars Path- Development of a Flight Article for a Hypersonic Enthalpy Effects on Hypervelocity Boundary- finder Lander A97-041 Boundary-Layer Experiment A97-094 Layer Transition: Ground Test and Flight Data Moon-Sun Attitude Sensor A97-055 Deployment Test Methods for a Large Deploy- A97-095 Preflight Testing and Flight Performance of the able Mesh Reflector A97-126 Hypersonic Thermal Environment of a Proposed OEDIPUS-C Tether Force Sensor _A97-080 Single-Stage-to-Stage-Orbit Vehicle Structural Durability (Including Fatigue, A97-109 Spacecraft Structural Configuration, Design, Fracture, and Environmental Degradation) Galileo Probe Heat Shield Ablation Experiment and Analysis A97-110 Influence of X-Ray Solar Flare Radiation on Simulation of an Aerospace Vehicle Pitch-Over Degradation of Teflon® in Space Thermal Control Maneuver A97-037 A97-081 Cracking Characteristics of Dual-Wall Structures Thermal Sensitivity Analysis of Spacecraft Bat- Following Simulated Orbital Debris Particle Structural Dynamics and Characterization tery A97-059 Impact A97-049 Influence of X-Ray Solar Flare Radiation on Internal Effects Model for Spacecraft Modules Astronaut-Induced Disturbances in Microgravity Degradation of Teflon® in Space Perforated by Orbital Debris A97-050 A97-036 A97-081 Author Index Adam, Philippe H., A97-095 Berry, Scott A., A97-066 Caram, Jose M., A97-067 Cornelison, Joni, A97-096 Adelfang, S. I., A97-127 Berthoud, L., A97-017 Casalino, Lorenzo, A97-030, Crowther, R., A97-100 Adolphsen, J. N., A96-142 Bertin, John J., A97-067 A97-089 Curran, Francis M., A97-003 Agiiero, Victor M., A97-101 Bhatt, Hemanshu D., A97-123 Castellano, Timothy P., A97-041 Da Forno, R., A97-034 Allégre, J., A97-025, A97-111, Bilén, Sven G., A97-101 Cate, Hans ten, A97-035 Davies, R. E., A97-088 A97-112, A97-113 Bisch, D., A97-111, A97-112, Chadwick, Kenneth M., A97-093 De Filippis, F., A97-042 Angrilli, F., A97-034 A97-113 Chandrashaker, R., A97-102 Délery, Jean, A97-092 Antreasian, P. G., A97-077 Blanchard, Robert C., A97-001, Cho, Christopher S., A97-123 Dennison, J. R., A97-088 Ayuso-Barea, Antonio, A97-125 A97-108 Chobotov, V. A., A97-033 Desai, Prasun N., A97-051 Babinsky, H., A97-010 Boies, M. T., A97-031 Chpoun, A., A97-025 Dick, Jason N., A97-043 Barret, Chris, A97-075 Boltz, Frederick W., A97-107 Christensen, Carissa Bryce, Donahue, Benjamin B., A97-085 Barrows, S. P., A97-100 Borrelli, Salvatore, A97-061 A97-035 Dreyer, M., A97-015 Barth, J., A96-142 Bouslog, Stanley A., A97-067 Chuang, C.-H., A97-023 Drory, M. D., A97-106 Beiting, Edward J., A97-047, Bowersox, R. D. W., A97-029, Colasurdo, Guido, A97-030 Dubinsky, A., A97-062, A97-083 A97-048 A97-114 Cole, T. R., A97-054 Dulikravich, George S., A97-005 Bement, Laurence J., A97-060 Brady, B. B., A97-120, A97-121 Comstock, Douglas A., A97-035 Dunn, Michael J., A97-030 Benson, R. C., A97-031 Braun, R. D., A97-051, A97-074 Cook, Steven R., A97-058 Dupuis, A., A97-086, J97-115 Beran, Philip S., A97-021 Brucker, G. J., A96-142 Cooper, Gene R., A97-119 Ebrahimi, Houshang B., Bergmans, John L., A97-080 Buter, T. A., A97-114 Corbel, Bernard, A97-092 A97-099 858 J. SPACECRAFT, VOL. 34, NO.6: 1997 INDEX Edwards, J. A., A97-010, A97-086, Jongeward, G. A., A97-128 Moss, James N., A97-108 Sims, J. D., A97-026 A97-115 Jovic, Srba, A97-041 Myers, R. M., A97-128 Sims, Jon Andrew, A97-053 Edwards, J. R., A97-046 Katti, R. A., A97-059 Myers, Roger M., A97-003 Skliar, Mikhail, A97-079 Ellis, S., A97-087 Katz, I., A97-128 Nakagawa, Jun, A97-126 Smith, James E., Jr., A97-014 Elperin, T., A97-062, A97-083 Kawakami, Yoichi, A97-126 Nakamura, Y., A97-019 Smith, O. E., A97-127 Engblom, W. A., A97-068 Kimmel, Roger L., A97-065 Newman, Dava J., A97-036 Smith, R. E., A97-127 Engelund, Walter C., A97-006, Kleb, William L., A97-037 Nicholson, F. T., A97-077 Soldi, James D., A97-013 A97-051 Klein, Mark A., A97-065 Noojin, Steven L., A97-014 Spores, Ronald A., A97-122 Ericsson, L. E., A97-020 Kluever, Craig A., A97-003, Nowak, Robert J., A97-066 Srinivasan, G. R., A97-057 Erlandson, R. E., A97-012, A97-031 A97-056, A97-064 Ohta, T., A97-069 Srivastava, B., A97-091 Fansler, Kevin S., A97-119 Kontis, K., A97-118 Oleson, Steven R., A97-003 Stassinopolous, E. G., A96-142 Fanti, G., A97-034 Krishnan, V., A97-038 Olynick, D. R., A97-024, A97-090 Staugler, Andrew James, A97-053 Foster, Norman F., A97-005 Kroo, I. M., A97-074 Onoda, Junjiro, A97-016 Stetson, Kenneth F., A97-067 Fournier, E. Y., A97-115 Kuo, Zeal-Sain, A97-076 Oskay, Vural, A97-119 Stollery, J. L., A97-118 Fralick, Gustave C., A97-123 Ladoon, D., A97-068 Palmer, G. E., A97-090 Sturek, Walter B., A97-117 Frederick, R. A., Jr., A97-026 Lai, Shu T., A97-129 Panneton, Robert J., A97-131, Sugimoto, Toshio, A97-126 Gaitonde, Datta, A97-046 Lang, V. I., A97-120 A97-132 Sun, H. S., A97-105 Galica, G. E., A97-031 Lay, Richard R., A97-028 Pastrone, Dario, A97-030 Suresha, S., A97-059 Gardner, B. M., A97-128 LeBeau, Gerald J., A97-001 Patil, S. R., A97-045 Sutter, Brian M., A97-052 Garrison, T. P., A97-104 Lengrand, J. C., A97-025, A97-111, Patterson, M., A97-128 Suzuki, T., A97-019 Gatsonis, N. A., A97-012 A97-112, A97-113 Perkins, John N., A97-070, Swan, P. A., A97-104 Gell, David A., A97-028 Lesho, J. F., A97-031 A97-071 Swinerd, G. G., A97-100 Giesy, Daniel P., A97-082 Levack, Daniel J. H., A97-098 Phillips, W. Pelham, A97-006 Takahashi, Shinei, A97-097 Gilchrist, Brian E., A97-101 Levadou, Frangois, A97-081 Pizzicaroli, J., A97-104 Takita, Kenichi, A97-044 Gnoffo, P. A., A97-109 Lin, C. S., A97-054 Powell, Richard W., A97-051 Tam, Tim, A97-024 Goldstein, D. B., A97-068 Lin, Sheam-Chyun, A97-039 Qin, N., A97-086 Tang, J. R., A97-105 Gomez, Susan F., A97-132 Liu, L. Y., A97-105 Raffin, M., A97-025 Tartabini, Paul V., A97-051 Goracke, B. David, A97-098 Liu, Yung-Wha, A97-039 Raitt, W. John, A97-101 Tilley, Dennis L., A97-122 Graat, E. J., A97-077 Lohar, Fayyaz A., A97-002 Ramirez, W. Fred, A97-079 Tilmann, C. P., A97-114 Greene, F. A., A97-109 Longdon, L. W., A97-087 Rao, Prabhakara P., A97-052 Townsend, John S., A97-027 Guidice, Donald, A97-013 Longuski, James Michael, Rath, H. J., A97-015 Guidos, Bernard J., A97-073 A97-053 Ravachol, M., A97-042 TTrriybfootn,i dJi.s ,P .,M iAc9h7a-i0l4,2 A97-036 Guillot, Martin J., A97-043 Lovell, Robert R., A97-130 Ray, Kevin, A97-013 Gumbert, Cary C., A97-130 Lovell, T. Alan, A97-022 Reccanello, F., A97-034 Tsunoda, Hiroaki, A97-126 Gupta, S. C., A97-059 Ludlow, D. K., A97-086 Reijasse, Philippe, A97-092 Tyc, G., A97-080, A97-102 Utashima, Masayoshi, A97-032 Hamilton, H. H., Il, A97-109 Ma, Der-Ming, A97-004 Reinecke, William G., A97-043 Utsumi, Masahiko, A97-124 Hardy, David, A97-013 Maa, Scott, A97-041 Ren, F., A97-105 Uy, O. Manuel, A97-031 Hariu, Ken-ichi, A97-126 Mandell, M. J., A97-128 Rhew, Ray D., A97-080 Van Eesbeek, Marc, A97-081 Harper, Tim, A97-081 Mandeville, J.C. 497-017 Richards, W. Lance, A97-094 Hastings, Daniel E., A97-013, Marini, M., A97-042 Riehl, John P., A97-003 van Schoor, Marthinus C., A97-130 Martin, L. R., A97-120, A97-121 Riley, C. J., A97-109 A97-036 Haw, R. J., A97-077 Maryniak, Gregg, A97-035 Rivell, Thomas, A97-041 Vandegrift, John G., A97-014 Heavey, Karen R., A97-009 Mateescu, Dan, A97-002 Rudrakumar, S., A97-038 Vaughan, R., A97-018 Henline, W. D., A97-090 Matsuzaki, R., A97-069 Ryan, Robert S., A97-027 Verderaime, V., A97-018 Herman, D. E., A97-033 Matunaga, Saburo, A97-016 Sahu, Jubaraj, A97-009 Vigneron, F. R., A97-080, A97-102 Herrell, Linda M., A97-078 Maynard, E. P., A97-012 Santiago-Prowald, Julian, Vinh, Nguyen X., A97-076 Hilgers. A., A97-103 McElrath, T. P., A97-077 A9T-125 0 Violet, Michael D., A97-130 Hoffbaer, Mark A., A97-058 Mclnville, R. M., A97-007, A97-008, Sanz-Andrés, Angel, A97-125 Viswanath, P. R., A97-038, A97-045 Hollis, Brian R., A97-070, A97-071 A97-116 Sarper, Hiiseyin, A97-063 Wang, Joseph, A97-129 Hollister, Walter M., A97-130 Mehta, R. C., A97-084 Sawada, Keisuke, A97-097 Wang, Ten-See, A97-096 Hong, Philip E., A97-052 Miles, John B., A97-011 Schettino, Antonio, A97-061 Watanabe, Shigeya, A97-072 Honrubia, F. J. Lopez, A97-103 Milintchouk, Andrei, A97-081 Schiff, Lewis B., A97-117 Weilmuenster, K. James, A97-109 Hornung, Hans G., A97-095 Milos, F. S., A97-090, A97-110 Schmidt, David K., A97-022 Weinacht, Paul, A97-117 Housh, Clint, A97-116 Misra, Arun K., A97-002 Schmidt, Edward M., A97-040 Weislogel, M. M., A97-015 Hsu, Wen-Chiang, A97-004 Miyagawa, T., A97-069 Schneider, S. P., A97-068 Whitehead, William R., A97-080 Huffman, R. E., Jr., A97-114 Miyoshi, Kazuo, A97-126 Schonberg, William P., A97-049, Williamsen, Joel E., A97-049, Hwu, Shian U., A97-131, A97-132 Mizobata, Kazuhide, A97-097 A97-050 A97-050 Ince, M., A97-104 Monaghan, Richard C., A97-094 Schwoerke, Stephen N., A97-065 Wilmoth, Richard G., A97-001, Isaac, Kakkattukuzhy, A97-011 Moore, A. A., A97-074 Seiff, Alvin, A97-041 A97-108 Ishimoto, Shinji, A97-072 Moore, F. G., A97-007, A97-008, Serpico, M., A97-042 Wilson, Gregory R., A97-041 Jablonski, A. M., A97-080, A97-102 A97-116 Serrano, John, A97-050 Wolk, G., A97-015 Jaffe, Leonard D., A97-078 Moran, Kenneth J., A97-021 Shang, J. S., A97-046 Woodard, Stanley E., A97-028 Jarnot, Robert F., A97-028 Morimoto, Hitoshi, A97-023 Shaw, S. T., A97-086 Wu, Z. Z., A97-105 Johnson, C. G., A97-033 Mortari, Daniele, A97-055 Shen, Ming-Chiou, A97-039 Yamamoto, Yukimitsu, A97-072 Johnson, Gary W., A97-098 Moss, G. M., A97-087 Shi, Yijian, A97-011 Zago, A., A97-034 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX Chronological Index A97-001 Rarefied-Flow Transition Regime Orbiter Aerody- Steven L. Noojin, and James E. Smith Jr., University ofA labama in namic Acceleration Flight Measurements. Robert C. Blanchard Huntsville (34, 1, p. 104) Article and Richard G. Wilmoth, NASA Langley Research Center, and Ger- ald J. LeBeau, NASA Johnson Spacé Center (34, 1, p. 8) Article A97-015 Damped Oscillations of a Liquid/Gas Surface upon based on AIAA Paper 96-2467 Step Reduction in Gravity. G. Wélk, M. Dreyer, and H. J. Rath, University of Bremen, Germany, and M. M. Weislogel, NASA A97-002 Mars-Jupiter Aerogravity Assist Trajectories for Lewis Research Center (34, 1, p. 110) Article High-Energy Missions. Fayyaz A. Lohar, Arun K. Misra, and Dan Mateescu, McGill University (34, 1, p. 16) Article based on AIAA A97-016 Symmetric Motion Control for Adaptive Structure Paper 95-0457 Based Construction of Large Space Structures. Saburo Ma- tunaga, Tokyo Institute of Technology, Japan; and Junjiro Onoda, A97-003 Advanced Propulsion for Geostationary Orbit Inser- Institute for Space and Astronautical Science, Japan (34, 1, p. 118) tion and North-South Station Keeping. Steven R. Oleson and Article Roger M. Myers, NYMA Inc.; Craig A. Kluever, University of Mis- souri—Columbia/Kansas City; and John P. Riehl and Francis M. A97-017. Low-Earth-Orbit Micrometeoroid and Debris Inves- Curran, NASA Lewis Research Center (34, 1, p. 22) Article tigations. L. Berthoud, European Space Agency, The Netherlands; and J. C. Mandeville, ONERA, France (34, 1, p. 125) Article A97-004 Exact Design of Partial Coverage Satellite Constella- tions over Oblate Earth. Der-Ming Ma and Wen-Chiang Hsu, A97-018 U-Groove Aluminum Weld Strength Improvement. V. Verderaime and R. Vaughan, NASA Marshall Space Flight Cen- Tamkang University, Taiwan, ROC (34, 1, p. 29) Article based on AIAA Paper 94-3721 CP9411 ter (34, 1, p. 133) Article A97-005 Three-Dimensional Aerodynamic Shape Optimiza- A97-019 Planning Spiral Motions of Nonholonomic Free-Fly- tion Using Genetic and Gradient Search Algorithms. Norman ing Space Robots. Y. Nakamura and T. Suzuki, University of To- F. Foster, Lockheed Martin Corporation; and George S. Dulikrav- kyo, Japan (34, 1, p. 137) Article ich, Pennsylvania State University (34, 1, p. 36) Article A97-020 Hammerhead Wake Effects on Elastic Vehicle Dy- namics. L. E. Ericsson, Lockheed Missiles and Space Company, A97-006 Aerodynamics for a Winged, Circular-Body, Single- Inc. (34, 2, p. 145) Article Stage-to-Orbit Spacecraft Configuration. W. Pelham Phillips and Walter C. Engelund, NASA Langley Research Center (34, 1, p. A97-021 Numerical Analysis of a Swept-Fin Missile. Kenneth 43) Article based on AIAA Paper 95-1848 CP955 J. Moran and Philip S. Beran, U.S. Air Force Institute of Technol- ogy (34, 2, p. 152) Article A97-007 New Semiempirical Model for Wing-Tail Interfer- ence. F. G. Moore and R. M. MclInville, U.S. Naval Surface War- A97-022 Mission Performance and Design Sensitivities of Air- fare Center (34, 1, p. 48) Article based on AIAA Paper 96-3393 Breathing Hypersonic Launch Vehicles. David K. Schmidt and CP967 T. Alan Lovell, University of Maryland (34, 2, p. 158) Article A97-008 Nonlinear Aeroprediction Methodology for Roll Posi- A97-023 Periodic Optimal Cruise for a Hypersonic Vehicle tion of 45 Degrees. F. G. Moore and R. M. Mclnville, U.S. Naval with Constraints. C.-H. Chuang and Hitoshi Morimoto, Georgia Surface Warfare Center (34, 1, p. 54) Article Institute of Technology (34, 2, p. 165) Article A97-009 Numerical Investigation of Supersonic Base Flow A97-024 Trajectory-Based Validation of the Shuttle Heating with Base Bleed. Jubaraj Sahu and Karen R. Heavey, U.S. Army Environment. Dave Olynick and Tim Tam, NASA Ames Research Research Laboratory (34, 1, p. 62) Article Center (34, 2, p. 172) Article A97-010 Large-Scale Roughness Influence on Turbulent Hy- A97-025 Aerodynamic Forces and Moments for a Re-Entry personic Boundary Layers Approaching Compression Cor- Module. J. Allégre, M. Raffin, and J. C. Lengrand, Centre Na- ners. H. Babinsky, Cranfield University, England, UK; and J. A. tional de la Recherche Scientifique, France, and A. Chpoun, Uni- Edwards, Defence Research Agency, England, UK (34, 1, p. 70) Ar- versité d’Evry, France (34, 2, p. 182) Article ticle based on AIAA Paper 95-0334 A97-026 Preliminary Design of a Hybrid Propulsion Multimis- A97-011 Computational Fluid Dynamics Simulation of Turbu- sion Missile System. J. D. Sims and R. A. Frederick Jr., University lent Waverider Flowfield with Sideslip. Yijian Shi and John B. of Alabama in Huntsville (34, 2, p. 186) Article Miles, University of Missouri-Columbia; and Kakkattukuzhy Isaac, University of Missouri-Rolla (34, 1, p. 76) Article A97-027 Fundamentals and Issues in Launch Vehicle Design. Robert S. Ryan and John S. Townsend, NASA Marshall Space A97-012 Monte Carlo Modeling and Analysis of Pressure Sen- Flight Center (34, 2, p. 192) Article based on AIAA Paper 96-1194 sor Measurements During Suborbital Flight. N. A. Gatsonis and CP964 E. P. Maynard, Worcester Polytechnic Institute, and R. E. Erland- son, Johns Hopkins University, Applied Physics Laboratory (34, 1, A97-028 Experimental Investigation of Spacecraft In-Flight p. 83) Article Disturbances and Dynamic Response. Stanley E. Woodard, NASA Langley Research Center, Richard R. Lay and Robert F. Jar- A97-013 Flight Data Analysis for the Photovoltaic Array not, Jet Propulsion Laboratory, Calfornia Institute of Technology, Space Power Plus Diagnostics Experiment. James D. Soldi and and David A. Gell, University of Michigan (34, 2, p. 199) Article Daniel E. Hastings, Massachusetts Institute of Technology, and David Hardy, Donald Guidice, and Kevin Ray, U.S. Air Force Phil- A97-029 Turbulent Flow Structure Characterization of An- lips Laboratory (34, 1, p. 92) Article gled Injection into a Supersonic Crossflow. Rodney D. W. Bow- ersox, U.S. Air Force Institute of Technology (34, 2, p. 205) Article A97-014 Development and Operation of a Microgravity Fur- nace System for Sintering Experiments. John G. Vandegrift, A97-030 Mixture-Ratio Control to Improve Hydrogen-Fuel 860 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX Rocket Performance. Guido Colasurdo, Dario Pastrone, and A97-045 Zero-Lift Drag Characteristics of Afterbodies with a Lorenzo Casalino, Politecnico di Torino, Italy (34, 2, p. 214) Square Base. P. R. Viswanath and S. R. Patil, National Aerospace Article Laboratories, India (34, 3, p. 290) Article Technical Comment by Michael J. Dunn, The Boeing Company (34, 5, p. 691) A97-046 Structure of a Supersonic Three-Dimensional Cylin- der/Offset-Flare Turbulent Interaction. Datta Gaitonde and J. S. Shang, U.S. Air Force Wright Laboratory, and J. R. Edwards, A97-051 Contamination Experiments in the Midcourse Space Experiment. O. Manuel Uy, R. C. Benson, R. E. Erlandson, M. T. North Carolina State University (34, 3, p. 294) Article Boies, and J. F. Lesho, Johns Hopkins University, Applied Physics A97-047 Solid Rocket Motor Exhaust Model for Alumina Par- Laboratory; G. E. Galica and B. D. Green, Physical Sciences, Inc.; ticles in the Stratosphere. Edward J. Beiting, The Aerospace Cor- B. E. Wood, Arnold Engineering Development Center, and D. F. poration (34, 3, p. 303) Article based on AIAA Paper 97-0532 Hall, The Aerospace Corporation (34, 2, p. 218) Article based on AIAA Paper 96-0219 A97-048 Predicted Optical Characteristics of Solid Rocket Motor Exhaust in the Stratosphere. Edward J. Beiting, The A97-032 Spacecraft Orbits Around Asteroids for Global Map- Aerospace Corporation (34, 3, p. 311) Article ping. Masayoshi Utashima, National Space Development Agency, Japan (34, 2, p. 226) Article A97-049 Cracking Characteristics of Dual-Wall Structures Following Simulated Orbital Debris Particle Impact. William A97-033 Collision and Debris Hazard Assessment for a Low- P. Schonberg, University ofA labama in Huntsville, and Joel E. Wil- Earth-Orbit Space Constellation. V. A. Chobotov, D. E. Her- liamsen, NASA Marshall Space Flight Center (34, 3, p. 318) Article man, and C. G. Johnson, The Aerospace Corporation (34, 2, p. 233) Article A97-050 Internal Effects Model for Spacecraft Modules Perfo- rated by Orbital Debris. William P. Schonberg and John Serrano, A97-034 Effects of Severed Tethers in Space. F. Angrilli, R. Da University of Alabama in Huntsville, and Joel E. Williamsen, NASA Forno, F. Reccanello, and A. Zago, University of Padua, Italy; and Marshall Space Flight Center (34, 3, p. 325) Article G. Fanti, University of Parma, Italy (34, 2, p. 239) Article A97-051 Six-Degree-of-Freedom Entry Dispersion Analysis A97-035 Methodology for Cost-Benefit Analysis of Space for the METEOR Recovery Module. Prasun N. Desai, Robert D. Launch Infrastructure. Douglas A. Comstock, Carissa Bryce Braun, Richard W. Powell, Walter C. Engelund, and Paul V. Tart- Christensen, Gregg Maryniak, and Hans ten Cate, Futron Corpora- abini, NASA Langley Research Center (34, 3, p. 334) Article based tion (34, 2, p. 246) Article on AIAA Paper 96-0903 A97-036 Astronaut-Induced Disturbances in Microgravity. A97-052 Six-Degree-of-Freedom Trajectory Targeting and Dava J. Newman, Michail Tryfonidis, and Marthinus C. van Optimization for Titan Launch Vehicles. Prabhakara P. Rao, Schoor, Massachusetts Institute of Technology (34, 2, p. 252) Engi- Brian M. Sutter, and Philip E. Hong, Lockheed Martin Astronautics neering Note (34, 3, p. 341) Article based on AIAA Paper 96-3776 A97-037. Simulation of an Aerospace Vehicle Pitch-Over Ma- A97-053 Trajectory Options to Pluto via Gravity Assists from neuver. William L. Kleb, NASA Langley Research Center (34, 2, Venus, Mars, and Jupiter. Jon Andrew Sims, Andrew James p. 254) Engineering Note based on AIAA Paper 96-0825 Staugler, and James Michael Longuski, Purdue University (34, 3, p. 347) Article A97-038 Effect of Riblets on Axisymmetric Base Pressure. A97-054 Dynamic Model for Global Positioning System Block V. Krishnan, P. R. Viswanath, and S. Rudrakumar, National Aerospace Laboratories, India (34, 2, p. 256) Engineering Note IIR Space Vehicle. C. S. Lin and T. R. Cole, The Aerospace Cor- poration (34, 3, p. 354) Article A97-039 Design of Hypersonic Waveriders with Wing—Body- A97-055 Moon—Sun Attitude Sensor. Daniele Mortari, Univer- Tail—Inlet Engine. Sheam-Chyun Lin, Yung-Wha Liu, and Ming- Chiou Shen, National Taiwan Institute of Technology, Taiwan, sity of Rome “La Sapienza,” Italy (34, 3, p. 360) Article based on AIAA Paper 96-3618 CP969 ROC (34, 2, p. 258) Engineering Note A97-056 Heliospheric Boundary Exploration Using Ion Pro- A97-040 Aerodynamic Considerations for Kinetic Energy pulsion Spacecraft. Craig A. Kluever, University of Missouri—Co- Projectiles. Edward M. Schmidt, U.S. Army Research Laboratory lumbia/Kansas City (34, 3, p. 365) Article (34, 2, p. 261) Engineering Note A97-057. Unsteady Flowfield and Cavity Acoustics of the A97-041 Wind-Tunnel Test of Flow Through Mars Pathfinder Stratospheric Observatory for Infrared Astronomy. G. R. Srin- Lander. Thomas Rivell, Alvin Seiff, Srba Jovic, Gregory R. Wil- ivasan, NASA Ames Research Center (34, 3, p. 372) Article based son, Scott Maa, and Timothy P. Castellano, NASA Ames Research on AIAA Paper 95-1862 CP955 Center (34, 3, p. 265) Article A97-058 Nocilla Model Parameters Obtained from Forces Ex- A97-042 Comparison Between Numerical and Experimental erted on Surfaces by Molecular Beams. Steven R. Cook and Results on Different Hermes Elevon Shapes. F. De Filippis, M. Mark A. Hoffbauer, Los Alamos National Laboratory (34, 3, p. Serpico, and M. Marini, Centro Italiano Ricerche Aerospaziali; and 379) Article J. P. Tribot and M. Ravachol, Dassault Aviation, France (34, 3, p. 272) Article based on AIAA Paper 96-2472 CP965 A97-059 Thermal Sensitivity Analysis of Spacecraft Battery. S. Suresha, Indian Space Research Organisation Satellite Centre, A97-043 Pressure Distribution on Sabots in Hypervelocity S. C. Gupta, Indian Institute of Science, and R. A. Katti, Indian Flight. Martin J. Guillot, Jason N. Dick, and William G. Reinecke, Space Research Organisation Satellite Centre (34, 3, p. 384) Arti- University of Texas at Austin (34, 3, p. 279) Article cle A97-044 Film Cooling Effect of Hydrogen on Cylinder in Su- A97-060 Functional Performance of Pyrovalves. Laurence J. personic Airflow. Kenichi Takita, Tohoku University, Japan (34, Bement, NASA Langley Research Center (34, 3, p. 391) Article 3, p. 285) Article based on AIAA Paper 96-2754 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX 861 A97-061 Numerical Correlations Between Flight and Plasma A97-076 Improved Matched Asymptotic Solutions for Three- Wind-Tunnel Tests. Salvatore Borrelli and Antonio Schettino, Dimensional Atmospheric Skip Trajectories. Zeal-Sain Kuo, Centro Italiano Ricerche Aerospaziali (34, 3, p. 397) Engineering Chung Cheng Institute of Technology, Taiwan, ROC; and Nguyen Note X. Vinh, University of Michigan (34, 4, p. 496) Article based on AIAA Paper 96-3596 CP969 A97-062 Optimal Properties of Bodies of Revolution in Con- tinuum and Free Molecular Regimes. A. Dubinsky and T. Elp- A97-077 Navigating Galileo at Jupiter Arrival. R. J. Haw, P. G. erin, Ben-Gurion University of the Negev, Israel (34, 3, p. 400) Antreasian, T. P. McElrath, E. J. Graat, and F. T. Nicholson, Jet Engineering Note Propulsion Laboratory, California Institute of Technology (34, 4, p. 503) Article A97-063 Extreme Value Flight Duration Analysis of Four-En- gine Spacecraft. Hiiseyin Sarper, University of Southern Colorado A97-078 Cassini/Huygens Science Instruments, Spacecraft, (34, 3, p. 402) Engineering Note and Mission. Leonard D. Jaffe and Linda M. Herrell, Jet Propul- sion Laboratory, California Institute of Technology (34, 4, p. 509) A97-064 Maximum-Payload Transfers to Geosynchronous Article Orbit Using Arcjet Thrusters. Craig A. Kluever, University of Missouri—Columbia/Kansas City (34, 3, p. 405) Engineering Note A97-079 Air-Quality Monitoring and Detection of Air Con- tamination in an Enclosed Environment. Mikhail Skliar, Univer- A97-065 Three-Dimensional Hypersonic Laminar Boundary- sity of Utah; and W. Fred Ramirez, University of Colorado (34, 4, Layer Computations for Transition Experiment Design. Roger p. 522) Article L. Kimmel and Mark A. Klein, U.S. Air Force Wright Laboratory, and Stephen N. Schwoerke, Lockheed Martin Corporation (34, 4, A97-080 Preflight Testing and Flight Performance of the OE- p. 409) Article based on AIAA Paper 96-2080 DIPUS-C Tether Force Sensor. Alexander M. Jablonski and Frank R. Vigneron, Canadian Space Agency; Ray D. Rhew, NASA A97-066 Fin Leading-Edge Sweep Effect on Shock-Shock In- Langley Research Center; John L. Bergmans, CFD Research Cor- teraction at Mach 6. Scott A. Berry and Robert J. Nowak, NASA poration; and William R. Whitehead and George Tyc, Bristol Aero- Langley Research Center (34, 4, p. 416) Article based on AIAA Pa- space Limited, Canada (34, 4, p. 533) Article per 96-0230 A97-081 Influence of X-Ray Solar Flare Radiation on Degra- A97-067 Effect of Isolated Roughness Elements on Boundary- dation of Teflon® in Space. Andrei Milintchouk, Marc Van Ees- beek, Francois Levadou, and Tim Harper, European Space Agency, Layer Transition for Shuttle Orbiter. John J. Bertin, U.S. Air Force Academy; Kenneth F. Stetson; Stanley A. Bouslog, Rohr In- The Netherlands (34, 4, p. 542) Article dustries, Inc.; and Jose M. Caram, NASA Johnson Space Center (34, 4, p. 426) Article A97-082 Efficient Calculation of a Jitter/Stability Metric. Daniel P. Giesy, Lockheed Martin Corporation (34, 4, p. 549) Ar- ticle A97-068 Fluid Dynamics of Hypersonic Forward-Facing Cav- ity Flow. W. A. Engblom and D. B. Goldstein, University of Texas A97-083 Method of Basic Projectiles for Calculating Force Co- at Austin; and D. Ladoon and S. P. Schneider, Purdue University efficients. A. Dubinsky and T. Elperin, Ben-Gurion University of (34, 4, p. 437) Article the Negev, Israel (34, 4, p. 558) Engineering Note A97-069 Experimental Study of Cone-Derived Waveriders at A97-084 Transonic Flow Simulation for a Bulbous Heat Mach 5.5. T. Ohta, T. Miyagawa, and R. Matsuzaki, Tokyo Metro- Shield. R. C. Mehta, Vikram Sarabhai Space Center, India (34, 4, politan Institute of Technology, Japan (34, 4, p. 445) Article p. 561) Engineering Note A97-070 High-Enthalpy Aerothermodynamics of a Mars En- A97-085 Lunar Landing Craft for the Reusable Launch Vehi- try Vehicle Part 1: Experimental Results. Brian R. Hollis and cle and Shuttle Vehicles. Benjamin B. Donahue, Boeing Defense John N. Perkins, North Carolina State University (34, 4, p. 449) Ar- and Space Group (34, 4, p. 564) Engineering Note based on AIAA ticle Paper 96-4459 A97-071 High-Enthalpy Aerothermodynamics of a Mars En- A97-086 Calculation of Pitch Damping for a Flared Projectile. try Vehicle Part 2: Computational Results. Brian R. Hollis and N. Qin, D. K. Ludlow, and S. T. Shaw, Cranfield College of Aero- John N. Perkins, North Carolina State University (34, 4, p. 457) Ar- nautics, England, UK; J. A. Edwards, Defence Research and Eval- ticle uation Agency, England, UK; and A. Dupuis, Defence Research Establishment, Valcartier, Canada (34, 4, p. 566) Engineering Note A97-072 Aerodynamic Characteristics Evaluation of Hyper- based on AIAA Paper 97-0405 sonic Flight Experiment Vehicle Based on Flight Data. Shigeya Watanabe, Shinji Ishimoto, and Yukimitsu Yamamoto, National A97-087 Individual Components of the Yaw Damping Sum: Aerospace Laboratory, Japan (34, 4, p. 464) Article based on Implementation for Tumbling Bodies. S. Ellis, L. W. Longdon, AIAA Paper 96-4527 and G. M. Moss, Cranfield University, England, UK (34, 4, p. 568) Engineering Note A97-073 Navier-Stokes Computations of Finned Kinetic En- ergy Projectile Base Flow. Bernard J. Guidos, U.S. Army Re- A97-088 Evolution of Secondary Electron Emission Charac- search Laboratory (34, 4, p. 471) Article based on AIAA Paper 95- teristics of Spacecraft Surfaces. R. E. Davies and J. R. Dennison, 3460 CP958 Utah State University (34, 4, p. 571) Engineering Note A97-074 Collaborative Approach to Launch Vehicle Design. A97-089 Optimization of a Dual-Mixture-Ratio Hydrogen- R. D. Braun and A. A. Moore, NASA Langley Research Center, and Fuel Rocket. Lorenzo Casalino, Politecnico di Torino, Italy (34, 4, I. M. Kroo, Stanford University (34, 4, p. 478) Article based on p. 574) Engineering Note AIAA Paper 96-4018 CP9611 A97-090 High-Fidelity Thermal Protection System Sizing of A97-075 Flight Control Augmentors for Aft-Center-of-Grav- Reusable Launch Vehicle. G. E. Palmer, W. D. Henline, D. R. ity Launch Vehicles. Chris Barret, NASA Marshall Space Flight Olynick, and F. S. Milos, NASA Ames Research Center (34, 5, p. Center (34, 4, p. 487) Article 577) Article based on AIAA Paper 95-2080 862 J. SPACECRAFT, VOL. 34, NO. 6: 1997 INDEX A97-091 Computational Analysis and Validation for Lateral A97-106 Performance of Diamond-Coated Silicon Nitride Jet Controlled Missiles. B. Srivastava, Raytheon Company (34, 5, Bearings. M. D. Drory, Crystallume (34, 5, p. 683) Engineering p. 584) Article Note A97-092. Flow Confluence Past a Jet-On Axisymmetric After- A97-107 Payload Capability of Kerosene-Fueled Mini Shuttle. body. Philippe Reijasse, Bernard Corbel, and Jean Délery, Frederick W. Boltz, NASA Ames Research Center (34, 5, p. 685) ONERA, France (34, 5, p. 593) Article based on AIAA Paper 96- Engineering Note 2449 CP965 A97-108 Aerodynamic Flight Measurements and Rarefied- Flow Simulations of Mars Entry Vehicles. Robert C. Blanchard, A97-093. Plasma and Aerothermal Measurements on a Hyper- velocity Re-Entry Vehicle. Kenneth M. Chadwick, Calspan SRL Richard G. Wilmoth, and James N. Moss, NASA Langley Research Center (34, 5, p. 687) Engineering Note Corporation (34, 5, p. 602) Article based on AIAA Paper 96-2322 A97-109 Hypersonic Thermal Environment of a Proposed Sin- A97-094 Development of a Flight Article for a Hypersonic gle-Stage-to-Stage-Orbit Vehicle. K. James Weilmuenster, P. A. Boundary-Layer Experiment. W. Lance Richards and Richard C. Gnoffo, F. A. Greene, C. J. Riley, and H. H. Hamilton II, NASA Monaghan, NASA Dryden Flight Research Center (34, 5, p. 609) Langley Research Center (34, 6, p. 697) Article Article A97-110 Galileo Probe Heat Shield Ablation Experiment. A97-095 Enthalpy Effects on Hypervelocity Boundary-Layer Frank S. Milos, NASA Ames Research Center (34 , 6, p. 705) Article Transition: Ground Test and Flight Data. Philippe H. Adam and Hans G. Hornung, California Institute of Technology (34, 5, p. 614) A97-111 Experimental Rarefied Density Flowfields at Hyper- Article sonic Conditions over 70-Degree Blunted Cone. J. Allégre, D. Bisch, and J. C. Lengrand, Centre National de la Recherche Scien- A97-096 Analysis of Flowfields over Four-Engine DC-X Rock- tifique, France (34, 6, p. 714) Article ets. Ten-See Wang and Joni Cornelison, NASA Marshall Space Flight Center (34, 5, p. 620) Article based on AIAA Paper 96-2953 A97-112 Experimental Rarefied Aerodynamic Forces at Hy- personic Conditions over 70-Degree Blunted Cone. J. Allégre, A97-097 Conceptual Study of a Two-Stage, Air-Breathing Re- D. Bisch, and J. C. Lengrand, Centre National de la Recherche Sci- usable Launch Vehicle. Shinei Takahashi, Kazuhide Mizobata, entifique, France (34, 6, p. 719) Article and Keisuke Sawada, Tohoku University, Japan (34, 5, p. 628) Ar- A97-113 Experimental Rarefied Heat Transfer at Hypersonic ticle based on AIAA Paper 97-0192 Conditions over 70-Degree Blunted Cone. J. Allégre, D. Bisch, A97-098 Tripropellant Engine Option Comparisca for Single and J. C. Lengrand, Centre National de la Recherche Scientifique, France (34, 6, p. 724) Article Stage to Orbit. B. David Goracke and Daniel J. H. Levack, The Boeing Company; and Gary W. Johnson, NASA Marshall Space A97-114 Experimental Investigation of the Flow Structure Flight Center (34, 5, p. 636) Article based on AIAA Paper 95-3609 Near a Single Wraparound Fin. C. P. Tilmann and R. E. Huffman Jr., U.S. Air Force Wright Laboratory, T. A. Buter, U.S. Air Force A97-099 Validation Database for Propulsion Computational Institute of Technology; and R. D. W. Bowersox, University of Ala- Fluid Dynamics. Houshang B. Ebrahimi, Sverdrup Technology, bama (34, 6, p. 729) Article Inc. (34, 5, p. 642) Article A97-115 Base Cavity Effects on the Aerodynamic Characteris- A97-100 Computational Comparison of Debris Cloud Models. tics of a Hypersonic Flared Projectile. E. Y. Fournier and A. D. S. P. Barrows, Smith System Engineering, Ltd., England, UK; G. G. Dupuis, Defence Research Establishment, Valcartier, Canada, and Swinerd, University of Southampton, England, UK; and R. J. A. Edwards, Defence Research Agency, England, UK (34, 6, p. Crowther, Defence Evaluation and Research Agency, England, UK 737) Article (34, 5, p. 650) Article A97-116 Methods for Distributing Semiempirical, Nonlinear, A97-101 Transient Potential Modification of Large Spacecraft Aerodynamic Loads on Missile Components. F. G. Moore and Due to Electron Emissions. Sven G. Bilén, Victor M. Agiiero, and R. M. Mclnville, U.S. Naval Surface Warfare Center, and Clint Brian E. Gilchrist, University of Michigan; and W. John Raitt, Utah Housh, U.S. Naval Air Warfare Center (34, 6, p. 744) Article State University (34, 5, p. 655) Article A97-117 Navier-Stokes Predictions of Pitch Damping for Axi- A97-102 Damped Gyroscopic Modes of Spinning Tethered symmetric Projectiles. Paul Weinacht and Walter B. Sturek, U.S. Space Vehicles with Flexible Booms. F. R. Vigneron and A. M. Army Research Laboratory; and Lewis B. Schiff, NASA Ames Re- Jablonski, Canadian Space Agency; R. Chandrashaker, Pratt and search Center (34, 6, p. 753) Article Whitney Canada; and G. Tyc, Bristol Aerospace, Ltd., Canada (34, A97-118 Control Effectiveness of a Jet-Slender Body Combi- 5, p. 662) Article nation at Hypersonic Speeds. K. Kontis and J. L. Stollery, Cran- field University, England, UK (34, 6, p. 762) Article based on A97-103 Some Correlation Techniques for Environmentally AIAA Paper 96-2470 CP965 Induced Anomalies Analysis. F. J. Lopez Honrubia and A. Hilg- ers, European Space Agency, The Netherlands (34, 5, p. 670) Arti- A97-119 Extracting Meteorological Data from Projectile Tra- cle jectory. Gene R. Cooper, Kevin S. Fansler, and Vural Oskay, U.S. Army Research Laboratory (34, 6, p. 769) Article based on AIAA A97-104 Systems Engineering Trades for the IRIDIUM® Con- Paper 95-3437 CP958 stellation. T. P. Garrison, M. Ince, J. Pizzicaroli, and P. A. Swan, Motorola Satellite Communications Group (34, 5, p. 675) Article A97-120 Effects of Launch Vehicle Emissions in the Strato- sphere. B. B. Brady, L. R. Martin, and V. I. Lang, The Aerospace A97-105 Analytical Formulation for Thermal Protection of Corporation (34, 6, p. 774) Article Active Cooling Nosetips. F. Ren and J. R. Tang, Chinese Academy of Sciences, PRC; and L. Y. Liu, Z. Z. Wu, and H. S. Sun, China A97-121_ Modeling the Multiphase Atmospheric Chemistry of Academy of Launch Vehicle Technology, PRC (34, 5, p. 681) Engi- Launch Clouds, B. B. Brady and L. R. Martin, The Aerospace neering Note Corporation (34, 6, p. 780) Article