Table Of Content

Vol. 45, No. 6, November—December 2008 2008 Journal of Spacecraft and Rockets Index How to Use the Index In the Subject Index, pages 1331-1336, each technical paper is listed under a maximum of three appropriate headings. Note the locating number in boldface type preceding each paper title, and use that number to find the paper in the Chronological Index. The Author Index, pages 1337—1338, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1339-1343, also lists all papers by their locating numbers. This listing contains titles, authors and their affiliations, and volume, issue number, and page where the paper appeared. It also gives the AIAA paper number, if any, on which the article was based. 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 2008, that paper also will appear in both the Subject and Chronological Indexes. Authors of Comments also are listed in the Author Index. Subject Index AIRCRAFT TECHNOLOGY, A08-130 Surface Direct Current Discharge for A08-027 Discrete-Roughness Transition for Hy- CONVENTIONAL, STOL/VTOL Hypersonic Flow Control personic Flight Vehicles A08-034 Numerical Aerodynamic Investigations A08-024 Boundary-Layer Transition and Hyper- Aerodynamics on Missile Yawing Control Using Nose-Mounted sonic Flight Testing Flow Effectors A08-025 Effects of Roughness on Hypersonic A08-102 Time-Accurate Numerical Prediction of Free-Flight Aerodynamics of a Finned Projectile Fuels and Fuel Systems Boundary-Layer Transition A08-026 Transition Experiments on Blunt Bodies A08-042 Design, Analysis and Testing of Mars A08-072 Eccentric Drain Port to Prevent Vortex- with Distributed Roughness in Hypersonic Free Tumbleweed Rover Concepts ing During Draining from Cylindrical Tanks Flight A€8-057 Integration of Actuator Performance for Noise A08-121 Aerothermodynamic Testing and Boun- Guiding Supersonic Projectiles A08-054 X-43A Flight-Test-Determined Aero- A08-066 Adaptive Collocated Feedback for dary-Layer Trip Sizing of the HIFiIRE Flight | dynamic Force and Moment Characteristics at Noise Absorption in Payload Fairings Vehicle A08-124 Ground Test Studies of the HIFiRE-! Mach 7.0 Testing, Flight and Ground 408-047 Quasi-One-Dimensional Numerical Transition Experiment Part 2: Computational Analysis of Payload Venting of Satellite Launch A08-079 Simulation of a Flush Air-Data System Analysis Vehicle for Transatmospheric Vehicles A08-120 Effect of Freestream Noise on Rough- A08-055 Separation Motion of Strap-On Boosters A08-073 Development of Hypersonic Quiet ness-Induced Transition for the X-51A Forebody with Base Flow and Turbulence Effects Tunnels A08-028 Boundary-Layer Stability Analysis of A08-034 Numerical Aerodynamic Investigations the Hypersonic International Flight Research on Missile Yawing Control Using Nose-Mounted COMPUTING, INFORMATION, Transition Experiments Flow Effectors AND COMMUNICATION A08-021 Transition Issues for Atmospheric Entry A08-119 Summary of Hypersonic Boundary- Aerospace Plane Autonomous Systems Layer Transition Experiments on Blunt Bodies A08-079 Simulation of a Flush Air-Data System A08-066 Adaptive Collocated Feedback for with Roughness for Transatmospheric Vehicles Noise Absorption in Payload Fairings A08-125 Receptivity of a Hypersonic Flat-Plate 408-023 Hypersonic Boundary-Layer Transi- Boundary Layer to Three-Dimensional Surface tion: Application to High-Speed Vehicle Design FLUID DYNAMICS Roughness A08-122 Boundary-Layer Stability Calculations Configuration Design Boundary Layers and Heat Transfer- for the Hypersonic International Flight Research 408-105 Knowledge Discovery for Flyback- Turbulent Experimentation Transition Experiment Booster Aerodynamic Wing Using Data Mining A08-096 Experimental Study on Aerothermal Deceleration Systems Heating Caused by Jet-Hypersonic Crossflow Computational Fluid Dynamics Interaction 408-086 Static Aeroelastic Analysis of Thin-Film 408-048 Turbulent Aeroheating Testing of Mars 408-086 Static Aeroelastic Analysis of Thin-Film Clamped Ballute for Titan Aerocapture Science Laboratory Entry Vehicle Clamped Ballute for Titan Aerocapture 408-031 Flow Control over a Backward-Facing Flight Mechanics Boundary-Layer Stability and Transition Step with Application of a Magnetic Field 408-102 Time-Accurate Numerical Prediction of A08-073 Development of Hypersonic Quiet A08-102 Time-Accurate Numerical Prediction of Free-Flight Aerodynamics of a Finned Projectile Tunnels Free-Flight Aerodynamics of a Finned Projectile A08-054 X-43A Flight-Test-Determined Aero- A08-126 Nonparallel Flow Effects on Rough- 408-048 Turbulent Aeroheating Testing of Mars dynamic Force and Moment Characteristics at ness-Induced Perturbations in Boundary Layers Science Laboratory Entry Vehicle Mach 7.0 A08-123 Ground Test Studies of the HIFIRE-! 408-053 Numerical Investigation of a Spiked Transition Experiment Part 1: Experimental Blunt Nose Cone at Hypersonic Speeds Flow Control Results A08-077 Transient Modeling of High-Altitude A08-099 Bow Shock Wave Mitigation by Laser- A08-022 Influence of Laminar Boundary-Layer Rocket-Stage Separation Plasma Energy Addition in Hypersonic Flow Transition on Entry Vehicle Designs 408-115 Damping Behavior of Sioshing Liquid A08-057 Integration of Actuator Performance for A08-023 Hypersonic Boundary-Layer Transi- in Laterally Excited Cylindrical Propellant Guiding Supersonic Projectiles tion: Application to High-Speed Vehicle Design Vessels 1331 1332 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX 408-124 Ground Test Studies of the HIFiRE-1 A08-124 Ground Test Studies of the HIFiRE-1 A08-032 Free-Molecule-Microresistojet Per- Transition Experiment Part 2: Computational Transition Experiment Part 2: Computational formance Using Water Propellant for Nano- Analysis Analysis satellite Applications 408-047 Quasi-One-Dimensional Numerical A08-120 Effect of Freestream Noise on Rough- Analysis of Payload Venting of Satellite Launch ness-Induced Transition for the X-51A Forebody Supersonic Flow Vehicle A08-028 Boundary-Layer Stability Analysis of A08-045 Reducing the Numerical Viscosity in 408-028 Boundary-Layer Stability Analysis of the Hypersonic International Flight Research Nonstructured Three-Dimensional Finite Vol- the Hypersonic International Flight Research Transition Experiments umes Computations Transition Experiments A08-021 Transition Issues for Atmospheric Entry A08-078 Viscous Effects on Performance of Two- 408-055 Separation Motion of Strap-On Boosters A08-129 Stability Analysis of Beagle2 in the Dimensional Supersonic Linear Micronozzles with Base Flow and Turbulence Effects Free-Molecular and Transition Regimes A08-031 Flow Control over a Backward-Facing 408-034 Numerical Aerodynamic Investigations A08-130 Surface Direct Current Discharge for Step with Application of a Magnetic Field on Missile Yawing Control Using Nose-Mounted Hypersonic Flow Control A08-008 Improvement of High Heat Flux Flow Effectors A08-125 Receptivity of a Hypersonic Flat-Plate Measurement Using a Null-Point Calorimeter 408-101 Detached Eddy Simulations and Rey- Boundary Layer to Three-Dimensional Surface nolds-Averaged Navier- Stokes Calculations of a Roughness Unsteady Flows Spinning Projectile A08-119 Summary of Hypersonic Boundary- A08-101 Detached Eddy Simulations and Rey- 408-125 Receptivity of a Hypersonic Flat-Plate Layer Transition Experiments on Blunt Bodies nolds-Averaged Navier- Stokes Calculations of a Boundary Layer to Three-Dimensional Surface with Roughness Spinning Projectile Roughness A08-128 Multiscale Particle-Continuum Simula- A08-107 Sensitivity Analysis for the Dynamic A08-076 Forebody Strake Effects on Rocket tions of Hypersonic Flow over a Planetary Probe Aeroelasticity of a Launch Vehicle Aerodynamic Characteristics at High Angles of A08-096 Experimental Study on Aerothermal Attack Heating Caused by Jet-Hypersonic Crossflow Vortices Interaction A08-072 Eccentric Drain Port to Prevent Vortex- ing During Draining from Cylindrical Tanks Hypersonic Flow Inlet, Nozzle, Diffuser, and Channel A08-076 Forebody Strake Effects on Rocket 408-123 Ground Test Studies of the HIFiRE-| Flows Aerodynamic Characteristics at High Angles of Transition Experiment Part i: Experimental 408-078 Viscous Effects on Performance of Two- Attack Results Dimensional Supersonic Linear Micronozzles 408-074 Evaluation of Kineiic/Continuum Solv- Wave Motion and Sloshing er for Hypersonic Nozzle-Plume Flow Jets, Wakes, and Viscid-Inviscid Flow A08-088 Low-Gravity Slosh Analysis for Cylin- 408-073 Development of Hypersonic Quiet Interactions drical Tanks with Hemiellipsoidal Top and Tunnels 408-077 Transient Modeling of High-Altitude Bottom 408-131 Analysis of an Electromagnetic Miti- Rocket-Stage Separation A08-115 Damping Behavior of Sloshing Liquid gation Scheme for Reentry Telemetry Through in Laterally Excited Cylindrical Propellant Plasma Plasmadynamics and MHD Vessels 408-087 Mechanical Actuators for Guidance of a 408-131 Analysis of an Electromagnetic Miti- A08-112 Slosh Analysis for Teardrop Tank Supersonic Projectile gation Scheme for Reentry Telemetry Through 408-023 Hypersonic Boundary-Layer Transi- Plasma GUIDANCE, CONTROL, AND tion: Application to High-Speed Vehicle Design 408-051 Electromagnetic Reduction of Plasma 408-027 Discrete-Roughness Transition for Hy- Density During Atmospheric Reentry and Hyper- DYNAMICS TECHNOLOGY personic Flight Vehicles sonic Flights 408-053 Numerical Investigation of a Spiked 408-031 Flow Control over a Backward-Facing Astrodynamics Blunt Nose Cone at Hypersonic Speeds Step with Application of a Magnetic Field 408-092 Satellite Constellation Design for Com- 408-022 Influence of Laminar Boundary-Layer 408-030 Kinetic and Continuum Simulations of plex Coverage Transition on Entry Vehicle Designs Electromagnetic Control of a Simulated Reentry 408-005 Deep Impact Navigation System Per- 408-054 X-43A Flight-Test-Determined Aero- Flow formance dynamic Force and Moment Characteristics at 408-130 Surface Direct Current Discharge for 408-061 Autonomous Orbit Determination from Mach 7.0 Hypersonic Flow Control Lunar Halo Orbits Using Crosslink Range 408-051 Electromagnetic Reduction of Plasma 408-098 Numerical Analysis of Reentry Trajec- 408-038 Orbital Dynamics of Solar Sails for Density During Atmospheric Reentry and Hyper- tory Coupled with Magnetohydrodynamics Flow Geomagnetic Tail Exploration sonic Flights Control A08-039 Optimal Deployment/Retrieval of Teth- 408-026 Transition Experiments on Blunt Bodies 408-050 Magnetohydrodynamics Interaction ered Satellites with Distributed Roughness in Hypersonic Free Over an Axisymmetric Body in a Hypersonic Flight Flow Autonomous Vehicles 408-049 Evolutionary Algorithm Shape Optimi- A08-005 Deep Impact Navigation System Per- zation of a Hypersonic Flight Experiment Nose Rarefied Flows formance Cone A08-074 Evaluation of Kinetic/Continuum Solv- 408-042 Design, Analysis and Testing of Mars 408-050 Magnetohydrodynamics Interaction er for Hypersonic Nozzle-Plume Flow Tumbleweed Rover Concepts Over an Axisymmetric Body in a Hypersonic 408-077 Transient Modeling of High-Altitude A08-061 Autonomous Orbit Determination from Flow Rocket-Stage Separation Lunar Halo Orbits Using Crosslink Range 408-024 Boundary-Layer Transition and Hyper- 408-030 Kinetic and Continuum Simulations of sonic Flight Testing Electromagnetic Control of a Simulated Reentry Control System Design 408-025 Effects of Roughness on Hypersonic Flow A08-139 Electric Propulsion and Controller Boundary-Layer Transition 408-104 Improved Atomic Oxygen Quantifica- Design for Drag-Free Spacecraft Operation 408-070 Locating Sudden Changes in Heat Flux tion Within the Earth’s Upper Atmosphere A08-114 Fault-Tolerant Stabilization of a Teth- Using Higher Temporal Derivatives of Temper- Through Numerical Corrections ered Satellite System Using Offset Control ature A08-128 Multiscale Particle-Continuum Simula- A08-121_ Aerothermodynamic Testing and Boun- tions of Hypersonic Flow over a Planetary Probe Control System Effectors dary-Layer Trip Sizing of the HIFiRE Flight | A08-129 Stability Analysis of Beagle2 in the A08-087 Mechanical Actuators for Guidance of a Vehicle Free-Molecular and Transition Regimes Supersonic Projectile J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX 1333 Dynamics A08-074 Evaluation of Kinetic/Continuum Solv- A08-081 Optimal Design of Hypersonic Turbojet A08-038 Orbital Dynamics of Solar Sails for er for Hypersonic Nozzle-Plume Flow Engines for Two-Stage-to-Orbit Spaceplane Geomagnetic Tail Exploration A08-037 Improving Lunar Return Entry Range Reliability, Maintainability, and Logistics Capability Using Enhanced Skip Trajectory Flight Mechanics Guidance Support A08-037 Improving Lunar Return Entry Range A08-013 Navigation Solutions for the Repeated- A08-044 Spacecraft Reliability-Based Design Capability Using Enhanced Skip Trajectory Intercept Mission with Constrained Maneuver Optimization Under Uncertainty Including Dis- Guidance Time crete Variables A08-135 Entry, Descent, and Landing Operations A08-039 Optimal DeploymenvRetrieval of Teth- A08-068 Egalitarian Peer-to-Peer Satellite Refu- Analysis for the Stardust Entry Capsule ered Satellites eling Strategy Launch Vehicle Dynamics State Estimation Safety A08-033 Improved Aerodynamics for Configura- A08-061 Autonomous Orbit Determination from A08-110 Hazard Analysis for Uncontrolled Space tions with Boattails Lunar Halo Orbits Using Crosslink Range Vehicle Reentry A08-137 Active Vibroacoustic Device for Noise A08-035 Autonomous Optical Navigation at Sensor Systems Reduction in Launch Vehicles Jupiter: A Linear Covariance Analysis A08-083 Engineering Model of Temperature- Missile Dynamics Structural Control Induced Pneumatic Sensor Pressure Gradients for A08-087 Mechanical Actuators for Guidance of a A08-064 Active Vibration Control of a Deploy- Rarefied Flow Conditions Supersonic Projectile able Optical Telescope A08-070 Locating Sudden Changes in Heat Flux A08-103 New Method to Predict Nonlinear Roll System Identification Using Higher Temporal Derivatives of Temper- Damping Moments ature A08-064 Active Vibration Control of a Deploy- A08-056 New Methods to Predict Nonlinear Pitch able Optical Telescope Damping Moments LAUNCH VEHICLE AND A08-075 2009 Version of the Aeroprediction Trajectory Optimization MISSILE (LV/M) TECHNOLOGY Code: APO9 A08-039 Optimal Deployment/Retrieval of Teth- Missile Guidance and Control ered Satellites Aerodynamics A08-018 Optimized Low-Thrust Orbit Transfer A08-033 Improved Aerodynamics for Configura- A08-053 Numerical Investigation of a Spiked for Space Tugs tions with Boattails Blunt Nose Cone at Hypersonic Speeds A08-014 Electric Sail Performance Analysis A08-132 Stage-Separation Aerodynamics of Navigation Two-Stage Space Transport Systems Part 1: A08-035 Autonomous Optical Navigation at INTERDISCIPLINARY TOPICS Steady-State Simulations Jupiter: A Linear Covariance Analysis A08-133 Stage-Separation Aerodynamics of A08-036 In Situ Navigation of Spacecraft Aerospace Management Two-Stage Space Trarsport Systems Part 2: Formations in High-Altitude and Extraterrestrial A08-091 Technology Readiness Level, Schedule Unsteady Simulation Orbits Risk, and Slippage in Spacecraft Design A08-047 Quasi-One-Dimensional Numerical 408-059 Real-Time Navigation for Mars Mis- Analysis of Payload Venting of Satellite Launch sions Using the Mars Network Aerospace Technology Utilization Vehicle A08-005 Deep Impact Navigation System Per- 408-067 Utilization of Space Stations: 1971- A08-105 Knowledge Discovery for Flyback- formance 2006 Booster Aerodynamic Wing Using Data Mining Optimization Techniques A08-091 Technology Readiness Level, Schedule A08-049 Evolutionary Algorithm Shape Optimi- Risk, and Slippage in Spacecraft Design zation of a Hypersonic Flight Experiment Nose A08-018 Optimized Low-Thrust Orbit Transfer Analytical and Numerical Methods Cone for Space Tugs 408-104 Improved Atomic Oxygen Quantifica- A08-105 Knowledge Discovery for Flyback- 408-062 Space Event Detection Method tion Within the Earth’s Upper Atmosphere Booster Aerodynamic Wing Using Data Mining A08-110 Hazard Analysis for Uncontrolled Space Through Numerical Corrections Vehicle Reentry Redundancy Management A08-075 2009 Version of the Aeroprediction Atmospheric and Space Sciences Code: APO9 A08-044 Spacecraft Reliability-Based Design Optimization Under Uncertainty Including Dis- 408-062 Space Event Detection Method A08-103 New Method to Predict Nonlinear Roll crete Variables A08-138 Mission Results from FORMOSAT-3/ Damping Moments COSMIC Constellation System A08-107 Sensitivity Analysis for the Dynamic Signal Processing A08-058 Atmospheric Modeling Using Acceler- Aeroelasticity of a Launch Vehicle A08-079 Simulation of a Flush Air-Data System ometer Data During Mars Reconnaissance Orbiter A08-134 Projectile Aerodynamics Overtaking ¢ for Transatmospheric Vehicles Aerobraking Operations Shock Wave 408-041 Parametric Processing for Two-Dimen- A08-076 Forebody Strake Effects on Rocket sional Digital Sun Sensors: Algorithms, Model- Lasers and Laser Applications Aerodynamic Characteristics at High Angles of ling, and Testing A08-099 Bow Shock Wave Mitigation by Laser- Attack Plasma Energy Addition in Hypersonic Flow Spacecraft Dynamics Configuration Design Multidisciplinary Design Optimization A08-114 Fault-Tolerant Stabilization of a Teth- 408-010 Low Recurring Cost, Partially Reusable ered Satellite System Using Offset Control A08-049 Evolutionary Algorithm Shape Optimi- Heavy Lift Launch Vehicle A08-007 Sloshsat Spacecraft Calibration at Sta- zation of a Hypersonic Flight Experiment Nose 408-056 New Methods to Predict Nonlinear Pitch tionary Spin Rates Cone Damping Moments A08-062 Space Event Detection Method A08-065 Evaluating Technology Projections and A08-075 2009 Version of the Aeroprediction Weight Prediction Method Uncertainty of Future Code: APO9 Spacecraft Guidance and Control Launch Vehicles Launch Vehicle and Sounding Rocket A08-046 Expected Maneuver and Maneuver A08-044 Spacecraft Reliability-Based Design Covariance Models Optimization Under Uncertainty Including Dis- Systems A08-036 In Situ Navigation of Spacecraft crete Variables A08-133 Stage-Separation Aerodynamics of Formations in High-Altitude and Extraterrestrial A08-080 Design Optimization of a Space Launch Two-Stage Space Transport Systems Part 2: Orbits Vehicle Using a Genetic Algorithm Unsteady Simulation 1334 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX A08-066 Adaptive Collocated Feedback for Thermal Protection Systems A08-090 Explosive-Hazard Analysis for Reuse- Noise Absorption in Payload Fairings A08-052 Influence of Particles on Radiative Base able Launch Vehicles in On-Pad Environments A08-065 Evaluating Technology Projections and Heating from the Rocket Exhaust Plume Weight Prediction Method Uncertainty of Future A08-111 Dynamic Impact Tolerance of Shuttle Solar Power Launch Vehicles Orbiter Wing Leading-Edge Panels A08-093 Prediction of Center of Pressure for 408-132 Stage-Separation Aerodynamics of A08-127 Nonequilibrium Stagnation-Line Radi- Deformed Solar Sails Two-Stage Space Transport Systems Part |: ative Heating for Fire II Solid Rocket Motors Steady-State Simulations A08-010 Low Recurring Cost, Partially Reusable A08-109 Radiative Heat Transfer Analysis with Heavy Lift Launch Vehicle PROPULSION Molten Al203 Dispersion in Solid Rocket Motors 408-009 Determination of Allowable Hydrogen A08-080 Design Optimization of a Space Launch Permeation Rates for Launch Vehicle Propellant Advanced Space Propulsion Vehicle Using a Genetic Algorithm Tanks 408-038 Orbital Dynamics of Solar Sails for A08-052 Influence of Particles on Radiative Base 408-056 New Methods to Predict Nonlinear Pitch Geomagnetic Tail Exploration Heating from the Rocket Exhaust Plume Damping Moments A08-019 Photonic Laser Propulsion: Proof-of- Supersonic Combustion A08-103 New Method to Predict Nonlinear Roll Concept Demonstration Damping Moments A08-011 Numerical Investigation of Jet Inter- Detonation A08-137 Active Vibroacoustic Device for Noise action in a Supersonic Freestream Reduction in Launch Vehicles A08-089 Method for Crew-Escape Risk-Enve- 408-055 Separation Motion of Strap-On Boosters lope Assessment During Ascent SPACE TECHNOLOGY with Base Flow and Turbulence Effects 408-090 Explosive-Hazard Analysis for Reuse- able Launch Vehicles in On-Pad Environments A08-080 Design Optimization of aS pace Launch Aerobraking Configurations/ Vehicle Using a Genetic Algorithm Electric Propulsion Aerothermodynamics A08-018 Optimized Low-Thrust Orbit Transfer 408-086 Static Aeroelastic Analoyf sThiin-sFil m Missile Systems for Space Tugs Clamped Ballute for Titan Aerocapture A08-033 Improved Aerodynamics for Configura- 408-084 Hall Thruster Plume Model for Space- A08-030 Kinetic and Continuum Simulations of tions with Boattails craft Impingement Torque: Development and Electromagnetic Control of a Simulated Reentry Validation Flow Mission Studies and Economics A08-100 Solar Array Plasma Interaction: Infl- A08-069 Ballute Entry Systems for Lunar Return 408-010 Low Recurring Cost, Partially Reusable uence of Interconnect Shape on Primary Arc and Low-Earth-Orbit Return Missions Heavy Lift Launch Vehicle Parameters A08-083 Engineering Model of Temperature- A08-139 Electric Propulsion and Controller Induced Pneumatic Sensor Pressure Gradients for Propulsion and Propellant Systems Design for Drag-Free Spacecraft Operation Rarefied Flow Conditions 408-085 Comparative Assessment of Lunar 408-032 Free-Molecule-Microresistojet Per- A08-058 Atmospheric Modeling Using Acceler- Propellant Options formance Using Water Propellant for Nano- ometer Data During Mars Reconnaissance Orbiter 408-108 Correlation of Hybrid Rocket Propellant satellite Applications Aerobraking Operations Regression Measurements with Enthalpy-Balance Gas Turbine Engines Aerobraking Flight Mechanics Model Predictions 408-009 Determination of Allowable Hydrogen 408-011 Numerical Investigation of Jet Inter- 408-071 Enceladus Mission Architecture Using Permeation Rates for Launch Vehicle Propellant action in a Supersonic Freestream Titan Aerogravity Assist for Orbital Capture Tanks Hybrid Rocket Engines About Saturn 408-019 Photonic Laser Propulsion: Proof-of- 408-058 Atmospheric Modeling Using Acceler- 408-108 Correlation of Hybrid Rocket Propellant Concept Demonstration ometer Data During Mars Reconnaissance Orbiter Regression Measurements with Enthalpy-Balance Aerobraking Operations Model Predictions Simulation Global Positioning System Hypersonic Propulsion A08-132 Stage-Separation Aerodynamics of 408-036 In Situ Navigation of Spacecraft Two-Stage Space Transport Systems Part | 408-099 Bow Shock Wave Mitigation by Laser- Formations in High-Altitude and Extraterrestrial Steady-State Simulations Plasma Energy Addition in Hypersonic Flow Orbits A08-133 Stage-Separation Aerodynamics of 408-081 Optimal Design of Hypersonic Turbojet Two-Stage Space Transport Systems Part 2 Engines for Two-Stage-to-Orbit Spaceplane Humans in Space/Life Support Systems, Unsteady Simulation 408-011 Numerical Investigation of Jet Inter- EVA 408-108 Correlation of Hybrid Rocket Propellant action in a Supersonic Freestream 408-097 Review of Seal Designs on the Apollo Regression Measurements with Enthalpy-Balance Liquid Rocket Engines Spacecraft Model Predictions 408-089 Method for Crew-Escape Risk-Enve- 408-043 Lunar Lander Concepts for Human International Space Station lope Assessment During Ascent Exploration 408-090 Explosive-Hazard Analysis for Reuse- 408-072 Eccentric Drain Port to Prevent Vortex- A08-113 Systems Analysis and Structural Design able Launch Vehicles in On-Pad Environments ing During Draining from Cylindrical Tanks of an Unpressurized Cargo Delivery Vehicle A08-067 Utilization of Space Stations: 1971- 408-101 Detached Eddy Simulations and Rey- Micro Propulsion and Power 2006 nolds-Averaged Navier- Stokes Calculations of a 408-019 Photonic Laser Propulsion: Proof-of- Spinning Projectile Landers Concept Demonstration A08-078 Viscous Effects on Performance of Two- A08-060 Entry, Descent, and Landing Commu- Testing, Flight and Ground Dimensional Supersonic Linear Micronozzles nications for the 2007 Phoenix Mars Lander A08-096 Experimental Study on Aerothermal A08-032 Free-Molecule-Microresistojet Per- A08-135 Entry, Descent, and Landing Operations Heating Caused by Jet-Hypersonic Crossflow formance Using Water Propellant for Nano- Analysis for the Stardust Entry Capsule Interaction satellite Applications A08-003 Entry, Descent, and Landing Operations A08-024 Boundary-Layer Transition and Hyper- Analysis for the Genesis Entry Capsule sonic Flight Testing Propulsion Hazards A08-004 Reconstruction of the Genesis Entry A08-020 Enthalpy Measurement of Inductively A08-089 Method for Crew-Escape Risk-Enve- A08-043 Lunar Lander Concepts for Human Heated Airflow lope Assessment During Ascent Exploration J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX 1335 Mission Design and Analysis A08-085 Comparative Assessment of Lunar A08-097 Review of Seal Designs on the Apollo A08-135 Entry, Descent, and Landing Operations Propellant Options Spacecraft Analysis for the Stardust Entry Capsule A08-110 Hazard Analysis for Uncontrolled Space A08-113 Systems Analysis and Structural Design A08-035 Autonomous Optical Navigation at Vehicle Reentry of an Unpressurized Cargo Delivery Vehicle Jupiter: A Linear Covariance Analysis A08-015 Extension of Traditional Entry, Descent, A08-017 Accuracy Analysis of the Reflective A08-015 Extension of Traditional Entry, Descent, and Landing Technologies for Human Mars Surface of the Umbrella-Type Antenna and Landing Technologies for Human Mars Exploration Exploration A08-016 Analysis of the UNISAT-3 Solar Array Spacecraft Test and Evaluation A08-060 Entry, Descent, and Landing Commu- In-Orbit Performance A08-012 Qualification of Spacecraft Equipment: nications for the 2007 Phoenix Mars Lander A08-069 Ballute Entry Systems for Lunar Return Random-Vibration Response Based on Impe- A08-040 Multibody Orbit Architectures for Lunar and Low-Earth-Orbit Return Missions dance/Mobility Techniques South Pole Coverage A08-092 Satellite Constellation Design for Com- A08-084 Hall Thruster Plume Model for Space- A08-043 Lunar Lander Concepts for Human plex Coverage craft Impingement Torque: Development and Exploration A08-114 Fault-Tolerant Stabilization of a Teth- Validation A08-014 Electric Sail Performance Analysis ered Satellite System Using Offset Control A08-141 Global Static Testing and Model A08-069 Ballute Entry Systems for Lunar Return A08-091 Technology Readiness Level, Schedule Validation of Stiffened Thin-Film Polyimide and Low-Earth-Orbit Return Missions Risk, and Slippage in Spacecraft Design Panels A08-071 Enceladus Mission Architecture Using A08-138 Mission Results from FORMOSAT-3/ A08-106 Aeroelastic Response and Protection of Titan Aerogravity Assist for Orbital Capture COSMIC Constellation System Space Shuttle External Tank Cable Trays About Saturn A08-113 Systems Analysis and Structural Design A08-007 Sloshsat Spacecraft Calibration at Sta- A08-092 Satellite Constellation Design for Com- ofa n Unpressurized Cargo Delivery Vehicle tionary Spin Rates plex Coverage Spacecraft Attitude Determination A08-003 Entry, Descent, and Landing Operations Spacecraft Thermal Management A08-083 Engineering Model of Temperature- Analysis for the Genesis Entry Capsule A08-082 Enhancement of Emissive Properties for Induced Pneumatic Sensor Pressure Gradients for A08-004 Reconstruction of the Genesis Entry In-Space High-Temperature Radiator Materials Rarefied Flow Conditions A08-037 Improving Lunar Return Entry Range A08-041 Parametric Processing for Two-Dimen- Capability Using Enhanced Skip Trajectory sional Digital Sun Sensors: Algorithms, Model- STRUCTURAL MECHANICS Guidance ling, and Testing AND MATERIALS A08-140 Preliminary Design of Superorbital A08-093 Prediction of Center of Pressure for Earth Entry Flight Experiment Using the Volna Launcher Deformed Solar Sails Aeroelasticity and Control 408-139 Electric Propulsion and Controller Spacecraft Communication A08-107 Sensitivity Analysis for the Dynamic Design for Drag-Free Spacecraft Operation A08-060 Entry, Descent, and Landing Commu- Aeroelasticity of a Launch Vehicle A08-136 Modeling a Low-Energy Ballistic Lunar A08-106 Aeroelastic Response and Protection of nications for the 2007 Phoenix Mars Lander Transfer Using Dynamical Systems Theory A08-131 Analysis of an Electromagnetic Miti- Space Shuttle External Tank Cable Trays gation Scheme for Reentry Telemetry Through Mission Trajectories (Earth and Flexible and Active Structures Plasma Interplanetary) A08-042 Design, Analysis and Testing of Mars A08-071 Enceladus Mission Architecture Using Spacecraft Contamination/Sterilization Tumbleweed Rover Concepts Titan Aerogravity Assist for Orbital Capture A08-006 Thruster Plumes: Sources for High A08-064 Active Vibration Control of a Deploy- About Saturn Pressure and Contamination at the Payload able Optical Telescope A08-040 Multibody Orbit Architectures for Lunar Location A08-001 Systematically Creased Thin-Film South Pole Coverage Membrane Structures A08-014 Electric Sail Performance Analysis Spacecraft Power A08-141 Global Static Testing and Model A08-046 Expected Maneuver and Maneuver A08-100 Solar Array Plasma Interaction: Infl- Validation of Stiffened Thin-Film Polyimide Covariance Models uence of Interconnect Shape on Primary Arc Panels A08-129 Stability Analysis of Beagle2 in the Parameters A08-063 Folding Large Antenna Tape Spring Free-Molecular and Transition Regimes A08-016 Analysis of the UNISAT-3 Solar Array A08-136 Modeling a Low-Energy Ballistic Lunar In-Orbit Performance Structural Composite Materials Transfer Using Dynamical Systems Theory Spacecraft Propulsion System Integration A08-063 Folding Large Antenna Tape Spring A08-013 Navigation Solutions for the Repeated- A08-009 Determination of Allowable Hydrogen Intercept Mission with Constrained Maneuver A08-100 Solar Array Plasma Interaction: Infl- Permeation Rates for Launch Vehicle Propellant uence of Interconnect Shape on Primary Arc Time Tanks Parameters Space Experiments A08-085 Comparative Assessment of Lunar Structural Design Propellant Options A08-067 Utilization of Space Stations: 1971- A08-063 Folding Large Antenna Tape Spring 2006 Spacecraft Sensor Systems Structural Dynamics and A08-016 Analysis of the UNISAT-3 Solar Array A08-041 Parametric Processing for Two-Dimen- In-Orbit Performance sional Digital Sun Sensors: Algorithms, Model- Characterization A08-007 Sloshsat Spacecraft Calibration at Sta- ling, and Testing A08-106 Aeroelastic Response and Protection of tionary Spin Rates Space Shuttle External Tank Cable Trays A08-006 Thruster Plumes: Sources for High Spacecraft Structural Configuration, A08-111 Dynamic Impact Tolerance of Shuttle Pressure and Contamination at the Payload Design, and Analysis Orbiter Wing Leading-Edge Panels Location A08-111 Dynamic Impact Tolerance of Shuttle A08-138 Mission Results from FORMOSAT-3/ Orbiter Wing Leading-Edge Panels Structural Finite Elements COSMIC Constellation System A08-012 Qualification of Spacecraft Equipment: A08-141 Global Static Testing and Model Random-Vibration Response Based on Impe- Validation of Stiffened Thin-Film Polyimide Space Systems dance/Mobility Techniques Panels A08-068 Egalitarian Peer-to-Peer Satellite Refu- A08-093 Prediction of Center of Pressure for A08-002 Effective Modulus of Creased Thin eling Strategy Deformed Solar Sails Membranes 1336 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX Structural Modeling A08-098 Numerical Analysis of Reentry Trajec- Nonintrusive Diagnostics A08-012 Qualification of Spacecraft Equipment: tory Coupled with Magnetohydrodynamics Flow A08-020 Enthalpy Measurement of Inductively Random-Vibration Response Based on Impe- Control Heated Airflow dance/Mobility Techniques A08-121 Aerothermodynamic Testing and Boun- A08-001 Systematically Creased Thin-Film dary-Layer Trip Sizing of the HIFiIRE Flight | Radiation in Participating Media Membrane Structures Vehicle A08-109 Radiative Heat Transfer Analysis with A08-048 Turbulent Aeroheating Testing of Mars Molten Al203 Dispersion in Solid Rocket Motors Structural Stability Science Laboratory Entry Vehicle A08-094 Spectrum Modeling for Air Shock- A08-001 Systematically Creased Thin-Film A08-128 Multiscale Particle-Continuum Simula- Layer Radiation at Lunar-Return Conditions Membrane Structures tions of Hypersonic Flow over a Planetary Probe A08-052 Influence of Particles on Radiative Base A08-095 Non-Boltzmann Modeling for Air Heating from the Rocket Exhaust Plume Shock-Layer Radiation at Lunar-Return Con- THERMOPHYSICS AND HEAT ditions Radiation Interchange Between Surfaces TRANSFER A08-127 Nonequilibrium Stagnation-Line Radi- A08-082 Enhancement of Emissive Properties for ative Heating for Fire II In-Space High-Temperature Radiator Materials Ablation, Pyrolysis, Thermal A08-119 Summary of Hypersonic Boundary- Decomposition and Degradation Layer Transition Experiments on Blunt Bodies Thermal Control with Roughness A08-082 Enhancement of Emissive Properties for A08-029 Performance of aL ow Density Ablative A08-140 Preliminary Design of Superorbital In-Space High-Temperature Radiator Materials Heat Shield Material Earth Entry Flight Experiment Using the Volna Thermal Modeling and Analysis Aerothermodynamics/Thermal Protection Launcher A08-097 Review of Seal Designs on the Apollo A08-029 Performance of aL ow Density Ablative A08-027 Discrete-Roughness Transition for Hy- Spacecraft Heat Shield Material personic Flight Vehicles A08-022 Influence of Laminar Boundary-Layer Computational Heat Transfer Thermochemistry and Chemical Kinetics Transition on Entry Vehicle Designs A08-095 Non-Boltzmann Modeling for Air A08-095 Non-Boltzmann Modeling for Air A08-020 Enthalpy Measurement of Inductively Shock-Layer Radiation at Lunar-Return Con- Shock-Layer Radiation at Lunar-Return Con- Heated Airflow ditions ditions A08-008 Improvement of High Heat Flux 408-127 Nonequilibrium Stagnation-Line Radi- A08-094 Spectrum Modeling for Air Shock- Measurement Using a Null-Point Calorimeter ative Heating for Fire I] Layer Radiation at Lunar-Return Conditions 408-029 Performance of a Low Density Ablative Heat Shield Material Heat Conduction Thermophysical Properties 408-025 Effects of Roughness on Hypersonic A08-070 Locating Sudden Changes in Heat Flux A08-094 Spectrum Modeling for Air Shock- Boundary-Layer Transition Using Higher Temporal Derivatives of Temper- Layer Radiation at Lunar-Return Conditions A08-026 Transition Experiments on Blunt Bodies ature A08-123 Ground Test Studies of the HIFiRE-1 with Distributed Roughness in Hypersonic Free 405-008 Improvement of High Heat Flux Transition Experiment Part 1: Experimental Flight Measurement Using a Null-Point Calorimeter Results J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX Author Index Abdel-jawad, Madhat M., A08-129 Chioma, Vincent J., A08-013, Gimelshein, Sergey F., A08-074, Kim, Chongam, A08-055 Abe, Takashi, A08-030 A08-046 A08-077 Kim, H. D., A08-134 Alba, Christopher, A08-028, Cho, Ju Hyeong, A08-052 Godard, A08-114 Kim, Man Young, A08-052 A08-121, A08-122 Chocron, Sidney, A08-090 Goldstein, H. E., A08-029, Kim, Minkwan, A08-051, A08-131 Allen, Jeffrey B., A08-104 Christian, John A., A08-015 A08-029E, A08-029EE Kimmel, Roger, A08-121 Altwegg, Kathrin, A08-006 Chu, Vicky, A08-138 Goldsworthy, Mark J., A08-129 Knapp, Andreas, A08-020 Antol, Jeffrey, A08-042, A08-113 Clark, lan G., A08-069 Gowda, B.H. Lakshmana, A08-072 Ko, Soon-Heum, A08-055 Arakawa, Yoshihiro, A08-020 Cline, Jason, A08-077 Graf, Stephan, A08-006 Kobayashi, Hiroaki, A08-081 Arimilli, Rao V., A08-070 Collier, Arnold S., A08-048 Grebow, Daniel J., A08-040 Kolobov, Vladimir, A08-074 Arndt, Tim O., A08-115 Corey, Ronald L., A08-084 Greene, Frank A., AO8-121 Komurasaki, Kimiya, A08-020 Arslanbekov, Robert, A08-074 Corriveau, Daniel, A08-034 Griffin, Steven, A08-137 Koppenwallner, G., A07-117- Auweter-Kurtz, Monika, A08-020 Couzi, Jacques, A08-008 Guelhan, Ali, A08-096 A07-124TC Babuska, Vit, A08-064 Covington, M. A., A08-029, Hajos, Gregory, A08-042 Kornfeld, Richard P., A08-060 Bae, Young K., A08-019 A08-029E, A08-029EE Hanes, Stephen, A08-064 Kumar, Krishna Dev, A08-114 Baek, Seung Wook, A08-052 Craig, Lynn E., A08-060 Hardy, Robin C., A08-111 Kuntz, David W., A08-024 Bairstow, S. H., A08-037 Creasy, M. Austin, A08-066 Harris, Steven, A08-042 Kuo, Ying-Hwa, A08-138 Balboni, J. A., A08-029, A08-029E, Cristofolini, Andrea, A08-050 Hartfield, Roy J., A08-080 Lacy, Seth L., A08-064 A08-029EE Crossley, William, A08-044 Hassan, Rania, A08-044 Lafleur, Jarret M., A08-015 Balsiger, Hans, A08-006 Cruz, Jonathan N., A08-113 Hauser, Thomas, A08-104 Lane, Steven A., A08-064, A08-137 Bartels, Robert E., A08-106 Daniels, Christopher C., A08-097 Hay, Frank, A08-087 Laschka, Boris, A08-132, A08-133 Bartkowicz, Matthew D., A08-122 Davis, Mark C., A08-054 Heinemann, J. M., A08-029, Lasserre, Jean-Pierre, A08-008 Barton, G. H., A08-037 Davis, Roger, A08-076 A08-029E, A08-029EE Lau, Kei Y., A08-023 Battaglia, Jean-Luc, A08-008 Deepak, Narayan R., A08-049 Herdrich, Georg, A08-020 Lazzaro, Anthony, A08-137 Bauer, A. M., A08-032 DeJarnette, Fred R., A08-042 Hill, Keric A., AO8-061 Lee, Riki H., A08-032 Bayley, Douglas J., A08-080 Demetriou, Michael A., A08-139 Hitt, Darren L., A08-078 Leifer, Jack, AO8-141 Behrens, John W., A08-043 Desai, Prasun N., A08-003, Hoffmann, Klaus A., A08-031 Leo, Donald J., A08-066 Bemis, Eammon, A08-058 A08-004, A08-135 Holden, Michael, A08-028, Li, Chris, A08-041 Berger, Karen T., A08-121, Donahue, Benjamin B., A08-010, A08-123, A08-124 Lightsey, E. Glenn, A08-036, A08-122 A08-043 Hollis, Brian R., A08-048, A08-094, A08-059 Berry, Scott A., AO8-027 Doraiswamy, Sriram, A08-101 A08-095, A08-127 Likar, Justin J., A08-100 Bhat, Ramachandra S., A08-005 Dreyer, Michael E., A08-115 Holt, Greg N., A08-036 Lilly, Taylor C., A08-032 Black, Jonathan T., A08-141 Dubos, Gregory F., A08-091 Horvath, Thomas J., A08-027 Lin, Tony C., A08-022 Blandino, John J., A08-139 Duncan, Courtney, A08-059 Hough, S., A08-058 Liou, Yuei-An, A08-138 Bochsler, Peter, A08-006 Duncan, John A., A08-032 Howard, Phil, A08-063 Logan, William, A08-076 Bogdanoff, David W., A08-026 Dunlap, Patrick H., A08-097 Howell, Kathleen C., A08-040 Léhle, Stefan, A08-008 Bogorad, Alexander L., A08-100 Dutta, Atri, A08-068 Hrbud, Ivana A., A08-082 Lopatin, Alexander, A08-017 Borg, Matthew P., A08-120 Ebrahimi, Houshang B., A08-011 Huang, Cheng-Yung, A08-138 Louisos, William F., A08-078 Borghi, Carlo A., A08-050 Edwards, John W., A08-106 Igawa, Hirotaka, A08-093 Lyle, Karen H., AO8-111 Born, George H., A08-061, A08-136 Eilers, Shannon D., A08-108 Ishikawa, Motoo, A08-098 Lyne, James Evans, A08-071 Boyce, Russell R., A08-049 Elaskar, Sergio A., A08-045 Ivanco, Thomas G., A08-106 Lyons, Daniel T., A08-003, A08-135 Boyd, lain D., A08-051, A08-128, Ellsworth, Joel C., A08-079 Jackson, Karen E., A08-111 MacLean, Matthew, A08-028, AO8-131 Ely, Todd A., A08-059 Janhunen, Pekka, A08-014 A08-123, A08-124 Braun, Robert D., A08-015, Enright, John, A08-041 Jaslikowski, Adam, A08-018 Macrossan, Michael N., A08-129 408-037, A08-069, A08-086, Eramya, Allen, A08-077 Jenkins, Christopher H., A08-002, Malone, Shane P., A08-084 A08-091 Falcinelli, Oscar, A08-045 A08-093 Marchetti, Paul, A08-139 Braunstein, Matthew, A08-077 Fantoni, Gabriele, A08-050 Jenkins, Rhonald M., A08-080 Markov, Alexander V., A08-067 Breitsamter, Christian, A08-132, Farinholt, Kevin M., A08-066 Johnson, Heath, A08-028, A08-121, Martinez, E. R., A08-029, A08-133 Farrington, Phiilip A., A08-065 A08-122, AO8-124 A08-029E, A08-029EE Brewster, M. Quinn, A08-109 Fasanella, Edwin L., A08-111 Johnston, Christopher O., A08-094, Martinez, Roland, A08-085 Brickler, Angela, A08-058 Fiethe, Bjérn, A08-006 A08-095, A08-127 Massey, Kevin C., A08-057, Brown, Shaun, A08-058 Finkbeiner, Joshua R., A08-097 Jones, Lisa E., A@8-111 A08-087 Burkhalter, John F., A08-080 Folta, David C, A08-040 Josyula, Eswar, 408-074 Mastroddi, Franco, A08-107 Burkhart, P. Daniel, A08-059 Fong, Chen-Joe, A08-138 Ju, Myoung-Gun, A08-072 Mastrodemos, Nickolaos, A08-005 Burton, Rodney L., A08-018 Forbes, Jeffrey M., A07-117- Jullien, Pierre, A08-008 Matsuda, Atsushi, A08-030 Butman, Stan, A08-060 A07-124R Jung, Jy-Yun, A08-109 Matsui, Makoto, A08-020 Candler, Graham V., A08-028, Frankel, Jay 1., A08-070 Kangas, Julie, A08-135 Maulsby, Curtis, A08-043 A08-101, AO8-122 Fravenholz, Raymond B., A08-005 Katsurayama, Hiroshi, A08-030 Mazzoleni, Andre P., A08-042 Caplin, Glenn, A08-043 Freitas, Christopher J., A08-089, Kawamura, Masaaki, A08-030 Mcllwain, Stuart, A08-034 Carney, Kelly S., A08-111 A08-090 Keating, Gerald, A08-058 McMichael, Jim, A08-087 Chanes Jr., Jose B., A08-099 Fuentes, Robert, A08-064 Keedy, Ryan M., A08-089 Mehta, Rakhab Chandra, A08-047 Chang, Keun Shik, A08-140 Fujino, Takayasu, A08-098 Keidar, Michael, A08-051, A08-131 Melis, Matthew E., A08-111 Chen, Suzhen, A08-034 Gantovnik, Vladimir, AO8-017 Kellas, Sotiris, AO8-111 Mengali, Giovanni, A08-014 Chen, Y.-K., A08-029, A08-029E, Garcia, Mark D., A08-060 Keller, Donald F., A08-106 Minucci, Marco A., A08-099 A08-029EE Gauer, Markus, A08-053 Ketsdever, Andrew D., A08-032 Moelyadi, Mochammad A.., Chesley, Steven R., A08-005 Geller, David K., A08-035 Keyhani, Majid, A08-070 A08-132, A08-133 Chi, Sien, A08-138 Gholston, Sampson E., A08-065 Khan, Ovais U., A08-031 Mogensen, Andreas E., A08-059 Chiba, Kazuhisa, A08-105 Giangi, Marilena, A08-107 Killingsworth, Miles D., A08-032 Montagnon, Elsa, A08-006 1338 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX Moore, Frank G.. A08-033, Piergentili, Fabrizio, A08-016, Schrader, Karl, A08-064 Toro, Paulo G. P., A08-099 A08-056, A08-075, A08-103 A08-016E Schuette, Gerrit, A08-096 Tsiotras, Panagiotis, A08-068 Moore, James D., A08-093 Polli, Gian Mario, A08-107 Schuster, David M., A08-106 Tumin, Anatoli, A08-126 Moore, Linda Y., A08-033, Potter, Donald L., A08-024 Schwartzentruber, Thomas E., Ulybyshev, Yuri, A08-092 408-056, A08-075, A08-103 Prabhu, Dinesh K., A08-026 A08-128 Utsumi, Masahiko, A08-088, Mundy, E., A08-123 Price, Xenophon, A08-084 Setoguchi, T., A08-134 A08-112 Muylaert, Jean, A08-140 Pukniel, Andrew, A08-018 Shang, J. S., A08-130 van Ootegem, Bruno, A08-008 Myrabo, Leik N.. A08-099 Putnam, Z. R., A08-037 Shidner, Jeremy D., A08-058 Verges, Amanda, A08-015 Na, Jae Jeong, AO8-140 Qualls, Garry D., A08-004 Signori, Gina M., A08-060 Vreeburg, Jan P.B., A08-007 Nagamatsu, H. T., A08-099 Quarta, Alessandro A., A08-014 Silton, Sidra 1., A08-057 Wadhams, Timothy, A08-028, Nandurkar, Kuldeep, A08-002 Rajesh, G., A08-134 Smith, David B., A08-043 A08-123, A08-124 Nerem, R. Steven, A007-117- Ramsey, Philip, A08-071 Smith, Suzanne Weaver, A08-141 Wang, Xiaowen, A08-125 A07-124R Randolph, Thomas M., A08-084 Snyder, John Steven, A08-084 Warnock, Tyler, A08-087 Neretti, Gabriele, A08-050 Rausch, Russ D., A08-106 Sohn, Chang-Hyun, A08-072 Weldon, Vince A., A08-010 Notter, Michael, A08-063 Ray, Taprabata, A08-049 Sorokin, Igor V., A08-067 Wells, Grant, A08-015 Obayashi, Shigeru, A08-105 Reda, Daniel C., A08-026 Soykasap, Omer, A08-063 White, John Terry, A08-054 Olejniczak, J., A08-029, A08-029E, Reshotko, Eli, A08-021 Stahl, Bernhard, A08-096 Whitmore, Stephen A., A08-079, A08-029EE Robinson, Michael J., A08-009 Stanley, Douglas Oliver, A08-085 A08-083, A08-108 Oliveira, Antonio Carlos, A08-099 Rodrigues, Gongalo, A08-012 Stastny, Nathan Bohus, A08-035 Wilder, Michael C., A08-026 Omura, Yoshiharu, A08-038 Rohrschneider, Reuben R.., Steinetz, Bruce M., A08-097 Wilhite, Alan W., A08-065 Owen, Jr, William M., A08-005 A08-086 Stella, Fulvio, A08-107 Williams, Paul, A08-039 Oyama, Teppei, A08-038 Rutkovskaya, Marina, A08-017 Strickland, Christopher, A08-042 Wilson, Jamie L., A08-042 Ozimek, Martin T, A08-040 Ryne, Mark S., A08-005 Sutton, Erik K., AO7-117—A07-124R Woo, Kyeongsik, A08-002, A08-093 Paganucci, Fabrizio, A08-050 Sahu, Jubaraj, A08-102 Sutton, Kenneth, A08-094, A08-095, Wu, Jie, A08-070 Papa, Alessandro, A08-001 Saleh, Joseph H., A08-091 A08-127 Wu, K. Chauncey, A08-113 Paris, Steve W., A08-010 Santiago-Prowald, Julian, A08-012 Suzuki, Hirokazu, A08-081 Yam, Albert, A08-041 Park, Chul, A08-140 Santoni, Fabio, A08-016, A08-016E Swain, James J., A08-065 Yamakawa, Hiroshi, A08-038 Parker, Jeffrey S., AO8-136 Sarigul-Klijn, Marti, A08-076 Tamagno, Jose P., A08-045 Yen, Nick, A08-138 Passaro, Andrea, A08-050 Sarigul-Klijn, Nesrin, A08-076 Tan, Bo, A08-114 Yoshino, Tomoyuki, A08-098 Patera, Russell P., A08-062, Sasamoto, Washito A., A08-113 Terrazas-Salinas, I., A08-029, Yu, Myoung Jong, A08-052 A08-110 Scalabrin, Leonardo C., A08-128 A08-029E, A08-029EE Zaleski, Kristina, A08-058 Paull, Allan, A08-053 Scher, Michael, A08-058 Thomas, Paige, A08-058 Zhong, Xiaolin, AO8-125 Pellegrino, Sergio, A08-001, Schneider, Steven P., A08-025, Titus, Nathan A., A08-013, A08-046 A08-063 408-073, A08-119, A08-120 Tolson, Robert H., A08-058 Piatak, David J., AO8-106 Schoenenberger, Mark D., A08-004 Tooley, Jeff, A08-135 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX Chronological Index A07-117-A07-124 Special Section: New Perspectives on the Sat- A08-014 Electric Sail Performance Analysis. Giovanni Mengali and ellite Drag Environments of Earth Mars and Venus. Sean L. Alessandro A. Quarta, University of Pisa, ltaly: and Pekka Janhunen, Finnish Bruinsma, Centre d'Etudes Spatiales, France; Jeffrey M. Forbes, University Meteorological Institute, Finland (45, |, p. 122) Article of Colorado, Frank G. Lemoine, NASA Goddard Space Flight Center; et al. (44, 6, p. 1154) A08-015 Extension of Traditional Entry, Descent, and Landing Technical Comment by G. Koppenwallner, Hypersonic Technology Technologies for Human Mars Exploration. John A. Christian, Grant Goettingen, Germany (45, 6, p. 1324) Wells, Jarret M. Lafleur, Amanda Verges, and Robert D. Braun, Georgia Reply by Erik K. Sutton, R. Steven Nerem, and Jeffrey M. Forbes, Instofi Tetchnuolotgy e(4 5, |, p. 130) Article basedo n AIAA Paper 2006-7427 University of Colorado (45, 6, p. 1328) A08-016 Analysis of the UNISAT-3 Solar Array In-Orbit Perform- A08-001 Systematically Creased Thin-Film Membrane Structures. ance. Fabio Santoni, University of Rome “La Sapienza,” Italy; and Fabrizio Alessandro Papa and Sergio Pellegrino, University of Cambridge, United Piergentili, University of Bologna, Italy (45, 1, p. 142) Article Kingdom (45, 1, p. 10) Article based on AIAA Paper 2005-1975 A08-002 Effective Modulus of Creased Thin Membranes. Kyeongsik A08-016E Erratum on “Analysis of the UNISAT-3 Solar Array In- Woo, Chungbuk National University, Republic of Korea; Kuldeep Nandurkar Orbit Performance.” Fabio Santoni, University of Rome “La Sapienza,” and Christopher H. Jenkins, Montana State University (45, 1, p. 19) Article Italy; and Fabrizio Piergentili, University of Bologna, Italy (45, 2, p. 415) based on AIAA Paper 2006-1798 Erratum A08-003 Entry, Descent, and Landing Operations Analysis for the A08-017 Accuracy Analysis of the Reflective Surface of the Genesis Entry Capsule. Prasun N. Desai, NASA Langley Research Center: Umbrella-Type Antenna. Alexander V. Lopatin and Marina A. and Daniel T. Lyons, Jet Propulsion Laboratory, California Institute of Rutkovskaya, Siberian State Aerospace University, Russia; and Vladimir B. Technology (45, 1, p. 27) Article Gantovnik, Universofi Ntoryt h Caroatl Chairlonttea ( 45, 1, p. 149) Technical Note A08-004 Reconstruction of the Genesis Entry. Prasun N. Desai, Garry D. Qualls, and Mark Schoenenberger, NASA Langley Research Center (45, |, p. 33) Article A08-018 Optimized Low-Thrust Orbit Transfer for Space Tugs. Andrew Pukniel, Rodney L. Burton, and Adam Jaslikowski, University of A08-005 Deep Impact Navigation System Performance. Raymond B. Illinois at Urbana—Champaign (45, 1, p. 151) Technical Note Frauenholz, Ramachandra S. Bhat, Steven R. Chesley, Nickolaos Mastrodemos, William M. Owen Jr., and Mark S. Ryne, Jet Propulsion A08-019 Photonic Laser Propulsion: Proof-of-Concept Demonstra- Laboratory, California Institute of Technology (45, 1, p. 39) Article based on tion. Young K. Bae, Bae Institute (45, 1, p. 153) Technical Note AIAA Paper 06-173 A08-020 Enthalpy Measurement of Inductively Heated Airflow. A08-006 Thruster Plumes: Sources for High Pressure and Makoto Matsui, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Contanination at the Payload Location. S. Graf, K. Altwegg, H. Balsiger, Tokyo, Japan; Andreas Knapp and Georg Herdrich, University of Stuttgart, and P. Bochsler, University of Bern, Switzerland; B. Fiethe, Technische Germany; and Monika Auweter-Kurtz, University of Hamburg, Germany (45, Universitdt, Germany; and E. Montagnon, ESA, Germany (45, |, p. 57) Article 1, p. 155) Technical Note based on AIAA Paper 2007-4408 A08-007 Sloshsat Spacecraft Calibration at Stationary Spin Rates. Jan P. B. Vreeburg, Leiden, The Netherlands (45, |, p. 65) Article A08-021 Transition Issues for Atmospheric Entry. Eli Reshotko, Case Western Reserve University (45, 2, p. 161) Article based on AIAA Paper 2007- A08-008 Improvement of High Heat Flux Measurement Using a Null- 0304 Point Calorimeter. Stevan Léhle and Jean-Luc Battaglia, Université de Bordeaux 1, France, Pierre Jullien and Bruno van Ootegem, European A08-022 Influence of Laminar Boundary-Layer Transition on Entry Aeronautical Defense and Space Academy, France; Jacques Couzi and Jean- Vehicle Designs. T. C. Lin, Northrop-Grumman Corporation (45, 2, p. 165) Pierre Lasserre, Commissariat a l'Energie Atomique/Centre d'Etudes Article based on AIAA Paper 2007-0309 Scientifiques et Techniques d'Aquitaine, France (45, |, p. 76) Article A08-023 Hypersonic Boundary-Layer Transition: Application to A08-009 Determination of Allowable Hydrogen Permeation Rates High-Speed Vehicle Design. Kei Y. Lau, The Boeing Company (45, 2. p. 176) for Launch Vehicle Propellant Tanks. Michael J. Robinson, The Boeing Article based on AIAA Paper 2007-310 Company (45, 1, p. 82) Article based on AIAA Paper 2006-2018 A08-010 Low Recurring Cost, Partially Reusable Heavy Lift Launch A08-024 Boundary-Layer Transition and Hypersonic Flight Testing. Vehicle. Benjamin B. Donahue, Boeing Advanced Systems; Vince A. Weldon David W. Kuntz and Donald L. Potter, Sandia National Laboratories (45, 2, p. and Steve W. Paris, Boeing Phantom Works (45, |, p. 90) Article based on 184) Article based on AIAA Paper 2007-0308 AIAA Paper 2004-4064 A08-025 Effects of Roughness on Hypersonic Boundary-Layer A08-011 Numerical Investigation of Jet Interaction in a Supersonic Transition. Steven P. Schneider, Purdue University (45, 2, p. 193) Article Freestream. Houshang B. Ebrahimi, ATA, Inc. (43, 1, p. 95) Article based on based on AIAA Paper 2007-0305 AIAA Paper 2005-4866 A08-026 Transition Experiments on Blunt Bodies with Distributed A08-012 Qualification of Spacecraft Equipment: Random-Vibration Roughness in Hypersonic Free Flight. D. C. Reda and M. C. Wilder, NASA Response Based on Impedance/Mobility Techniques. G. Rodrigues, Free Ames Research Center; D. W. Bogdanoff and D. K. Prabhu, Eloret University of Brussels, Belgium; and J. Santiago-Prowald, ESA, The Corporation (45, 2, p. 210) Article based on AIAA Paper 2007-0306 Netherlands (45, |, p. 104) Article A08-013 Navigation Solutions for the Repeated-Intercept Mission A08-027 Discrete-Roughness Transition for Hypersonic Flight with Constrained Maneuver Time. Vincent J. Chioma and Nathan A. Titus, Vehicles. Scott A. Berry and Thomas J. Horvath, NASA Langley Research U.S. Air Force Institute of Technology (45, 1, p. 116) Article Center (45, 2, p. 216) Article based on AIAA Paper 2007-307 1340 J. SPACECRAFT, VOL. 45, NO. 6: 2008 INDEX A08-028 Boundary-Layer Stability Analysis of the Hypersonic A08-040 Multibody Orbit Architectures for Lunar South Pole International Flight Research Transition Experiments. Heath B. Johnson, Coverage. Daniel J. Grebow, Martin T. Ozimek, and Kathleen C. Howell, Chris R. Alba, and Graham V. Candler, University of Minnesota; Matthew Purdue University; and David C. Folta, NASA Goddard Space Flight Center MacLean, Timothy Wadhams, and Michael Holden, Calspan—University at (45, 2, p. 344) Article Buffalo Research Center (45, 2, p. 228) Article based on AIAA Paper 2007- 311 A08-041 Parametric Processing for Two-Dimensional Digital Sun Sensors: Algorithms, Modeling, and Testing. John Enright, Albert Yam, A08-029 Performance of a Low Density Ablative Heat Shield and Chris Li, Ryerson University, Canada (45, 2, p. 359) Article Material. M. A. Covington and J. M. Heinemann, Eloret Corporation; H. E. Goldstein, Research Institute for Advanced Computer Science; Y .-K. Chen, lL. A08-042 Design, Analysis, and Testing of Mars Tumbleweed Rover Terrazas-Salinas, J. A. Balboni, J. Olejniczak, and E. R. Martinez, NASA Ames Concepts. Jamie L. Wilson, Andre P. Mazzoleni, and Fred R. DeJarnette, Research Center (45, 2, p. 237) Article based on AIAA Paper 2004-2273 North Carolina State University; Jeffrey Antol and Gregory A. Hajos, NASA Langley Research Center, and Christopher V. Strickland, NASA Wallops A08-029E Erratum on “Performance of a Low Density Ablative Heat Flight Facility (45, 2, p. 370) Article Shield Material.” M. A. Covington and J. M. Heinemann, Eloret Corporation, H. E. Goldstein, Research Institute for Advanced Computer A08-043 Lunar Lander Concepts for Human Exploration. Benjamin Science; Y.-K. Chen, I. Terrazas-Salinas, J. A. Balboni, J. Olejniczak, and E. B. Donahue, Glenn N. Caplin, David B. Smith, John Behrens, and Curtis R. Martinez, NASA Ames Research Center (45, 4, p. 854) Erratum Maulsby, Boeing Advanced Systems (45, 2, p. 383) Article based on AIAA Paper 2006-7443 A08-029EE Erratum on “Erratum on ‘Performance of a Low Density Ablative Heat Shield Material.’ M. A. Covington and J. M. Heinemann, A08-044 Spacecraft Reliability-Based Design Optimization Under Eloret Corporation, H. E. Goldstein, Research Institute for Advanced Uncertainty Including Discrete Variables. Rania Hassan and William Computer Science, Y.-K. Chen, |. Terrazas-Salinas, J. A. Balboni, J. Crossley, Purdue University (45, 2, p. 394) Article Olejniczak, and E. R. Martinez, NASA Ames Research Center (45, 6, p. 1330) Erratum A08-045 Reducing the Numerical Viscosity in Nonstructured Three- Dimensional Finite Volume Computations. Oscar A. Falcinelli, Sergio A. A08-030 Kinetic and Continuum Simulations of Electromagnetic Elaskar, and Jose P. Tamagno, National University of Cordoba, Argentina (45, Control of a Simulated Reentry Flow. Hiroshi Katsurayama, Masaaki 2, p. 406) Technical Note Kawamura, Atsushi Matsuda, and Takashi Abe, Japan Aerospace Exploration Agency, Japan (45, 2, p. 248) Article based on AIAA Paper 2007-1439 A08-046 Expected Maneuver and Maneuver Covariance Models. Vincent J. Chioma and Nathan A. Titus, U.S. Air Force Institute of Technology A08-031 Flow Control over a Backward-Facing Step with (45, 2, p. 409) Technical Note Application of a Magnetic Field. Ovais U. Khan and Klaus A. Hoffmann, Wichita State University (45, 2, p. 255) Article based on AIAA Paper 2006- A08-047 Quasi-One-Dimensional Numerical Analysis of Payload 3237 Venting of Satellite Launch Vehicle. R. C. Mehta, Vikram Sarabhai Centre, India (45, 2, p. 412) Technical Note A08-032 Free-Molecule-Microresistojet Performance Using Water Propellant for Nanosatellite Applications. R. H. Lee, A. M. Bauer, M. D. A08-048 Turbulent Aeroheating Testing of Mars Science Laboratory Killingsworth, T. C. Lilly, and J. A. Duncan, University of Southern Entry Vehicle. Brian R. Hollis, NASA Langley Research Center; and Amold California, Los Angeles; A. D. Ketsdever, U.S. Air Force Research S. Collier, Arnold Engineering Development Center (45, 3, p. 417) Article Laboratory (45, 2, p. 264) Article based on AIAA Paper 2007-5185 based on AIAA Paper 2007-1198 A08-033 Improved Aerodynamics for Configurations with Boattails. A08-049 Evolutionary Algorithm Shape Optimization of a Hyper- F. G. Moore and L. Y. Moore, Aeroprediction, Inc. (45, 2, p. 270) Article sonic Flight Experiment Nose Cone. N. R. Deepak, T. Ray, and R. R. Boyce, University of New South Wales, Australian Defence Force Academy, Australia A08-034 Numerical Aerodynamic Investigations on Missile Yawing (45, 3, p. 428) Article based on AIAA Paper 2006-7998 Control Using Nose-Mounted Flow Effectors. S. Chen, National Research Council Canada, Canada; D. Corriveau, Defence Research and Development A08-050 Magnetohydrodynamics Interaction Over an Axisymmet- Canada—Valcartier, Canada, and Stuart Mcllwain, National Research ric Body in a Hypersonic Flow. Andrea Cristofolini, Carlo A. Borghi, and Council Canada, Canada (45, 2, p. 282) Article Gabriele Neretti, University of Bologna, Italy; Andrea Passaro and Gabriele Fantoni, Alta Societa per Azioni, Italy; and Fabrizio Paganucci, University of A08-035 Autonomous Optical Navigation at Jupiter: A Linear Pisa, Italy (45, 3, p. 438) Article based on AIAA Paper 2006-8008 Covariance Analysis. Nathan B. Stastny and David K. Geller, Utah State University (45, 2, p. 290) Article based on AIAA Paper 2006-6680 A08-051 Electromagnetic Reduction of Plasma Density During Atmospheric Reentry and Hypersonic Flights. Michael Keidar, George A08-036 In Situ Navigation of Spacecraft Formations in High- Washington University; Minkwan Kim and lain Boyd, Universityo fM ichigan Altitude and Extraterrestrial Orbits. Greg N. Holt and E. Glenn Lightsey, (45, 3, p. 445) Article University of Texas at Austin (45, 2, p. 299) Article based on AIAA Paper 2007-6755 A08-052 Influence of Particles on Radiative Base Heating from the Rocket Exhaust Plume. Man Young Kim, Chonbuk National University, A08-037 Improving Lunar Return Entry Range Capability Using Republic of Korea; Myoung Jong Yu, Korea Aerospace Research Institute, Enhanced Skip Trajectory Guidance. 7. R. Putnam, Georgia Institute of Republic of Korea; Ju Hyeong Cho, Korea Institute of Machinery and Technology, S. H. Bairstow, Charles Stark Draper Laboratory; R. D. Braun, Materials, Republic of Korea; and Seung Wook Baek, Korea Advanced Georgia Institute of Technology, and G. H. Barton, Charles Stark Draper Institute of Science and Technology, Republic of Korea (45, 3, p. 454) Article Laboratory (45, 2, p. 309) Article based on ALAA Paper 2006-7438 A08-053 Numerical Investigation of a Spiked Blunt Nose Cone at A08-038 Orbital Dynamics of Solar Sails for Geomagnetic Tail Hypersonic Speeds. M. Gauer and A. Paull, University of Queensland, Exploration. Teppei Oyama, Hiroshi Yamakawa, and Yoshiharu Omura, Australia (45, 3, p. 459) Article Kyoto University, Japan (45, 2, p. 316) Article A08-054 X-43A Flight-Test-Determined Aerodynamic Force and A08-039 Optimal Deployment/Retrieval of Tethered Satellites. Paul Moment Characteristics at Mach 7.0. Mark C. Davis and John T. White, Williams, Balwyn North, Australia (45, 2, p. 324) Article based on AIAA NASA Dryden Flight Research Center (45, 3, p. 472) Article based on AIAA Paper 2005-4291 Paper 2006-8028