Table Of Content

JOURNAL OF PROPULSION AND POWER lol. 25, No. 6, November—December 2009 2009 Journal of Propulsion and Power Index How to Use the Index In the Subject Index, pages 1363-1368, 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 1369-1370, lists all authors associated with a given technical paper. The locating numbers are identical to those in the Subject Index. The Chronological Index, pages 1371-1376, 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 2009, 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, Fuels and Fuel Systems ENERGY CONVENTIONAL, STOL/VTOL B09-111 Thermophysical Properties Mea {/ternate Fuels ments of Rocket Propellants RP-1 and RP-2 Aerodynamics B09-111 Thermophysical Properties Measure- B09-118 Comparison of Several Optimization Noise ments of Rocket Propellants RP-1 and RP-2 Strategies for Robust Turbine Blade Design B09-074 Design of Quiet Propeller fi Hydrogen and Unique Fuels B09-068 Experimental Investigations of Pressure Mini Unmanned Air Vehicle B09-147 Hardware-in-the-Loop Testing of a Fuel Distortions on the High-Pressure Compressor B09-021 Time Delay Analysis Cell Aircraft Powerplant Operating Behavior Engine Direct and Indirect Combustion B09-067 Development and Application of an Sources Laser Integration/Systems Arbitrary Lagrangian Eulerian Solver for Turbo B09-037 Combustion-Noise Chat B09-122 Comparative Study of Plastics as machinery Aeromechanics Turbofan Engine with a Spectra Propellants for Laser Ablation Plasma Thrusters B09-023 |R educed-Order Model for Combustion Method Viagnetohydrodynamic Power Generation Instability in a Two-Dimensional Duct with a Flameholdet Performance B09-008 Feasibility of an Onboard Surface Hall Magnetohydrodynamic Power Generator in B09-071 Experimental and Numerical Study of B09-027 Probabilistic Aspects of Reentry Flight Jet Mixing from a Shock-Containing Nozzle sign B09-099 Effect of Tabs on Rectangular Jet Plume B09-068 Experimental Investigations Vicrowaves Development Distortions on the High-Pressure B09-104 System-Level Feasibility Assessment of Operating Behavior Microwave Power Beaming for Small Satellites Aeroelasticity and Aeroservoelasticity B09-031 New Simulation Strategy for an Powerplant Integration Rotating Machinery Oscillating Cascade in Turbomachinery Using B09-148 Optimum Design of Turbopr B09-017 Aerothermal Analysis of a Partially Immersed-Boundary Method Using Genetic Algorithm Shrouded Axial Turbine Aerospace Plane Wind Power Propeller and Rotor Systems B09-134 Air-Hydrogen Heat Exchangers for B09-022 Shroud and Ejector Augmenters for Advanced Space Launchers B09-022 Shroud and Ejector Aug Subsonic Propulsion and Power Systems Subsonic Propulsion and Power Systems Air Transportation B09-074 Design of Quiet Propeller for FLUID DYNAMICS Mini Unmanned Air Vehicle B09-121_ Chemical Properties of Aircraft Engine Particulate Exhaust Emissions (eroacoustics Simulation B09-082 Passive Control of Pressure Oscillations Airframe-Propulsion Integration B09-023 Reduced-Order Model for Combi 1 Solid Rocket Motors: Cold-Flow Experiments B09-019 Experimental Investigation of Em Instability in a Two-Dimensional Duc B09-020 Computational Analyses of Offset- bedded Crossflow Fan for Airfoil Propulsion Flameholder Stream Nozzles for Noise Reduction Circulation Control B09-106 Bayesian Framework for Calibrati B09-021 Time Delay Analysis of Turbofan Gas Turbine Simulator Engine Direct and Indirect Combustion Noise Flow Control Testing, Flight and Ground Sources B09-019 Experimental Investigation of Em B09-037 Combustion-Noise Characterization bedded Crossflow Fan for Airfoil Propulsion Turbofan Engine with a Spectral Boundary Layers and Heat Transfer- Circulation Control Method Turbulent B09-070 Flow Characteristics of Tip Injection on B09-139 Computational Simulation of Cylindri- Compressor Rotating Spike via Time-Accurate Uninhabited and Unmanned Air Vehicles cal Film Hole with Jet Pulsation on Flat Plates Simulation B09-019 Experimental Investigation of En B09-116 Mitigation of Graphite Nozzle Erosion B09-099 Effect of Tabs on Rectangular Jet Plume bedded Crossflow Fan for Airfoil Propulsion by Boundary-Layer Control in Solid Propellant Development Circulation Control! Rocket Motors 1363 1364 J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX Computational Fluid Dynamics B09-071 Experimental and Numerical Study of B09-014 Pressure Measurements and Attenuation Jet Mixing from a Shock-Containing Nozzle in a Hybrid Multitube Pulse Detonation Turbine B09-137 Simulation of Supersonic Combustion B09-096 Effect of Chamber Backpressure on System in Three Dimensional Configurations Swirl Injector Fluid Mechanics B09-073 Compressible Flow Structures Interac- 809-080 Computational Analysis of the Oxidizer B09-098 Rotational Flowfields in Porous Chan- tion with a Two-Dimensional Ejector: A Cold- Preflow in an Upper-Stage Rocket Engine B09-020 Computational Analyses of Offset- nels with Arbitrary Headwall Injection Flow Study B09-091 Reaction Mechanism of Aluminum- Stream Nozzles for Noise Reduction Multiphase Flows Particle-Air Detonation B09-061 Mixing and Combustion Characteristics of Kerosene in a Model Supersonic Combustor B09-025 Spray Structure in Near-Injector Region Subsonic Flow B09-040 Numerical Study of Plasma Behavior in of Aerated Jet in Subsonic Crossflow a Magnetoplasmadynamic Thruster Around B09-080 Computational Analysis of the Oxidizer BS0u9b-s0o2n2i c SPhrroopuudl sioann d andE jePcotwoerr SAyusgtmeemnst ers for Critical Current Preflow in an Upper-Stage Rocket Engine B09-005 Large Eddy Simulation of Ftow Devel- B09-043 Comparison of Several Zero-Boil-Off Supersonic Flow opment in Chamber with Surface Mass Injection Pressure Control Strategies for Cryogenic Fluid B09-099 Effect of Tabs on Rectangular Jet Plume B09-004 Chemical Erosion of Refractory-Metal Storage in Microgravity Development Nozzle Inserts in Solid-Propellant Rocket Motors B09-091 Reaction Mechanism of Aluminum- B09-057 Experimental Study of aM ach 3 Bump- B09-070 Flow Characteristics of Tip Injection on Particle-Air Detonation Compression Flowfield Compressor Rotating Spike via Time-Accurate B09-097 Experimental Characterization of a B09-075 Thrust Measurement of the Hybrid Simulation Two-Phase Flowfield in a Solid Rocket Motor Electric Thruster TIHTUS by a Baffle Plate Model B09-061 Mixing and Combustion Characteristics Hydrodynamics of Kerosene in a Model Supersonic Combustor Plasmadynamics and MHD B09-018 Effects of Floating-Ring Seal Clearance B09-095 In-Stream Hypermixer Fueling Pylons B09-109 Operation of an Annular Helicon Plasma on the Pump Performance for Turbopumps in Supersonic Flow Source B09-002 Effect of Recess in High-Pressure B09-039 Langmuir Probe Studies of Magnetic Transonic Flow Liquid Oxygen/Methane Coaxial Injection and Confinement in an lon Thruster Discharge Plasma B09-069 Shock/Boundary-Layer/Tip-Clearance Combustion B09-008 Feasibility of an Onboard Surface Hall Interaction in a Transonic Rotor Blade B09-096 Effect of Chamber Backpressure on Magnetohydrodynamic Power Generator in Swirl Injector Fluid Mechanics Unsteady Flows Reentry Flight B09-056 Wall-Propelled, In-Tube Propulsion B09-067 Development and Application of an Inlet, Nozzle, Diffuser, and Channel with Repetitive-Pulse Laser Ablation Arbitrary Lagrangian Eulerian Solver for Turbo- Flows B09-040 Numerical Study of Plasma Behavior in machinery Aeromechanics B09-144 Numerical Investigation of Roll Torque a Magnetoplasmadynamic Thruster Around B09-086 Buzz Instability in a Mixed-Compres- Induced by Solid Rocket Motor Internal Flow Critical Current sion Air Intake B09-030 Influence of Heat Capacity Ratio on B09-145 Single-Phase Internal Flowfield Valida- Pressure and Nozzle Flow of a Scramjets Rarefied Flows tion with an Experimental Solid Rocket Motor B09-026 Measurement of Flow Properties and B09-075 Thrust Measurement of the Hybrid Model Thrust on Scramjet Nozzle Using Pressure- Electric Thruster TIHTUS by a Baffle Plate B09-141 Transient Three-Dimensional Side- Sensitive Paint Load Analysis of a Film-Cooled Nozzle B09-057 Experimental Study of aM ach 3 Bump- Reacting Flows and Combustion B09-071 Experimental and Numerical Study of Compression Flowfield B09-089 Liquid Monopropellant Combustion in Jet Mixing from a Shock-Containing Nozzle B09-086 Buzz Instability in a Mixed-Compres- Mesoscale Vortex Chamber B09-031 New Simulation Strategy for an sion Air Intake B09-124 Vortical Structure of Reacting Flow ina Oscillating Cascade in Turbomachinery Using B09-013 Oscillatory Flows of Rectangular Hy- Sudden-Expansion Combustor with Solid Fuel Immersed-Boundary Method personic Inlet Unstart Caused by Downstream B09-137 Simulation of Supersonic Combustion B09-073 Compressible Flow Structures Interac- Mass-Flow Choking in Three Dimensional Configurations tion with a Two-Dimensional Ejector: A Cold- B09-072 Optimization of Second Throat Ejectors B09-007 Diffusion Flame Calculations for Com- Flow Study for High-Altitude Test Facility posite Propellants Using a Vorticity-Velocity B09-113 Study of Restricted Shock Separation B09-098 Rotational Flowfields in Porous Chan- Formulation Phenomena in a Thrust Optimized Parabolic nels with Arbitrary Headwall Injection B09-032 Reacting Mixing-Layer Computations Nozzie B09-073 Compressible Flow Structures Interac- in a Simulated Turbine-Stator Passage Vortices tion with a Two-Dimensional Ejector: A Cold- B09-061 Mixing and Combustion Characteristics Flow Study of Kerosene in a Model Supersonic Combustor B09-098 Rotational Flowfields in Porous Chan- B09-081 Performance Characteristics of an B09-088 Condensation-Induced Surface Boiling nels with Arbitrary Headwall Injection Annular Conical Aerospike Nozzle with Free- of Alcohol Fuel Droplets in Combustion B09-145 Single-Phase Internal Flowfield Valida stream Effect Chambers tion with an Experimental Solid Rocket Motor B09-020 Computational Analyses of Offset- Model Stream Nozzles for Noise Reduction Separated Flows B09-095 In-Stream Hypermixer Fueling Pylons B09-120 Infrared Thermography and Pitot Pres- B09-113 Study of Restricted Shock Separation in Supersonic Flow sure Measurements of a Scramjet Nozzle Phenomena in a Thrust Optimized Parabolic B09-097 Experimental Characterization of a Flowfield Nozzle Two-Phase Flowfield in a Solid Rocket Motor B09-113 Study of Restricted Shock Separation Model B09-141 Transient Three-Dimensional Side- Phenomena in a Thrust Optimized Parabolic Load Analysis of a Film-Cooled Nozzle B09-124 Vortical Structure of Reacting Flow in a Nozzle Sudden-Expansion Combustor with Solid Fuel B09-015 Analytic Model for Single-Cycle Deto- Shock Waves and Detonations nation Tube with Diverging Nozzles B09-090 Review of Recent Developments in GUIDANCE, CONTROL, AND Wave Rotor Combustion Technology DYNAMICS TECHNOLOGY Jets, Wakes, and Viscid-Inviscid Flow B09-141 Transient Three-Dimensional Side- Interactions Load Analysis of a Film-Cooled Nozzle Artificial Intelligence B09-119 Vane Clocking in a _ Three-Stage B09-142 Thrust Measurement of a Multicycle B09-033 Gas Turbine Fault Diagnosis Using Compressor: Frequency Domain Data Analysis Partially Filled Pulse Detonation Rocket Engine Fuzzy-Based Decision Fusion J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX Control System Sensors LAUNCH VEHICLE AND Airbreathing Propulsion B09-114 Flame Spectra of a Turbulent Liquid- MISSILE (LV/M) TECHNOLOGY B09-028 Experiments on Electrically Controlled Fueled Swirl-Stabilized Lean-Direct Injection Flameholding on a Plane Wall in a Supersonic Combustor Propulsion and Propellant Systems Airflow B09-030 Influence of Heat Capacity Ratio on Engine Control B09-151 Transient Behavior of H202 Thruster Pressure and Nozzle Flow of a Scramjets Effect of injector Type and Ullage Volume B09-140 Forced Flame Response of Turbulent B09-026 Measurement of Flow Properties and B09-002 Effect of Recess in High-Pressure Liquid-Fueled Lean-Direct-Injection Combustion Thrust on Scramjet Nozzle Using Pressure- Liquid Oxygen/Methane Coaxial Injection and to Fuel Modulations e Paint Combustion B09-057 Experiment il Study of a Mach 3 Bump- Soft Computing B09-134 Air-Hydrogen Heat Exchangers for Compression I low field Advanced Space Launchers B09-033 Gas Turbine Fault Diagnosis Using B09-142 Thrust Mea surement of a Multicycle B09-144 Numerical Investigation of Roll Torque Fuzzy-Based Decision Fusion Partially Filled Pulse Detonation Rocket Engine Induced by Solid Rocket Motor Internal Flow B09-105 Emissions Reductions in Diesel and B09-112 Scaling and Evaluation of Pt/Al203 Kerosene Flames Using a Novel Fuel Injector INTERDISCIPLINARY TOPICS Catalytic Reactor for Hydrogen Peroxide B09-064 Ada nstability Suppression Con- Monopropellant Thruster rols Method For \ircraft Gas Turbine Engine Analytical and Numerical Methods B09-054 Compatibility of Glycidy! Azide Poly ( ombustors mer with Hydroxyl Terminated Polybutadienaen d B09-131 Numerical Simulation of SMART-1 B09-124 Vortical Structure of Reacting Flow in a Plasticizers Hall-Thruster Plasma Interactions Sudden-Expansion Combustor with Solid Fuel B09-081 Performance Characteristics of an B09-038 Influence of Electrode Shape on B09-134 Air-Hydrogen Heat Exchangers for Annular Conical Aerospike Nozzle with Free Performance of Pulsed Magnetoplasmadynamic Advanced Space Launchers stream Effect Thruster SIMP-LEX B09-100 Tip-Clearance Effects on Hot-Streak B09-125 Singular Spectrum Analysis Applied to Migration in Low-Pressure Stage of Vaneless Simulation Time-Series Measurements in a Self-Excited Tube Counter-Rotating Turbine Combustor B09-072 Optimization of Second Throat Ejectors B09-069 Shock/I lary-Layer/Tip-Clearance for High-Altitude Test Facility interaction1 nsonic Rotor Blade Environmental Effects B09-029 Upstream Injection on B09-121 Chemical Properties of Aircraft Engine Testing, Flight and Ground Scramjet Performance Using an Entropy-Based Particulate Exhaust Emissions B09-072 Optimization of Second Throat Ejectors Metho B09-065 Performance Evaluation of a Fast for High-Altitude Test Facility B09-094 Investigation on Lithium Mobility-Based Particle Spectrometer for Aircraft B09-016 Performance Validation of a Single Hydrid 5 ‘| for Solid-Fueled Scramjet Exhaust Tube Pulse Detonation Rocket System I B09-120 Infrare srmography and Pitot Pres- Lasers and Laser Applications Thermal Protection Systems Measurements of a Scramjet Nozzle B09-093 Oxygen/Hydrogen-Planar-Laser-In B09-116 Mitigation of Graphite Nozzle Erosion Flowfield duced Fluorescence Measurements and Accuracy by Boundary-Layer Control in Solid Propellant B09-140 Forced Flame Response of Turbulent Investigation in High-Pressure Combustion Rocket Motors Liquid-Fueled I in-Direct-Injection Combustion B09-092 Temperature Measurements in a Gas B09-082 Passive Control of Pressure Oscillations Fuel Modulations Turbine-Combustor Sector Rig Using Swept in Solid Rocket Motors: Cold-Flow Experiments B09-035 Experimental Evaluation of a Low Wavelength Absorption Spectroscopy izer Applied Engineering B09-041 [Impulse Generation on Aluminum Target Irradiated with Nd:YAG Laser Pulse in PROPULSION Ambient Gas Combined-Cycle Engines B09-056 Wall-Propelled, In-Tube Propulsion Advanced Space Propulsion B09-123 |M ulti-Objective Optimization of Rock- with Repetitive-Pulse Laser Ablation B09-045 Film Cooling of Accelerated Flow in a i-Cycle Engine Performance B09-122 Comparative Study of Plastics as Subscale Combustion Chamber ionary Algorithm Propellants for Laser Ablation Plasma Thrusters B09-102 Zero-Dimensional Time-Dependent Model of High-Pressure Ablative Capillary Multidisciplinary Design Optimization Discharge for Plasma Thrusters Combustion and Combustor Designs B09-074 Design of Quiet Propeller for an Electric B09-079 Circumferential Film Cooling Effective B09-089 Li Monopropellant Combustion in Mini Unmanned Air Vehicle ness ina LOX/H2 Subscale Combustion Chamber Mesoscale Vortex Chamber B09-017 Aerothermal Analysis of a Partially B09-101 Creation of Onset Voltage Hash by B09-060 S »-Edge Pylon Effects ona Shrouded Axial Turbine Anode Spots in a Magnetoplasmadynamic Scramijet Pylon ity Flameholder Flowfield B09-118 Comparison of Several Optimization Thruster B09-007 me Calculations for Com- Strategies for Robust Turbine Blade Design B09-039 Langmuir Probe Studies of Magnetic sing a Vorticity-Velocity Confinement in an Ion Thruster Discharge Plasma I Research Facilities and Instrumentation B09-075 Thrust Measurement of the Hybrid B09-036 Experimental Investigoaf tThieromona - B09-065 Performance Evaluation of a _ Fast Electric Thruster TIHTUS by a Baffle Plate Coupling for Low-Swirl Lean Premixed Mobility-Based Particle Spectrometer for Aircraft B09-041 Impulse Generation on Aluminum Flames Exhaust Target Irradiated with Nd:YAG Laser Pulse in B09-105 Emissions Reductions in Diesel and B09-147 Hardware-in-the-Loop Testing of a Fuel Ambient Gas Kerosen e Flames Using a Novel Fuel Injector Cell Aircraft Powerplant B09-055 Thrust Measurement of a Pure Magnetic B09-093 Oxygen/Hydrogen-Planar-Laser-In- B09-087 Development of a Specific Impulse Sail Using Parallelogram-Pendulum Method duced Fluorescence Measurements and Accuracy Balance for Capillary Discharge Pulsed Plasma B09-109 Operation of an Annular Helicon Plasma Investigation in High-Pressure Combustion Thrusters Source B09-021 Time Delay Analysis of Turbofan B09-010 Deep Space | Flight Spare lon Thruster Engine Direct and Indirect Combustion Noise Sensor Systems 30,000-Hour Life Test Sources B09-092 Temperature Measurements in a Gas- B09-081 Performance Characteristics of an B09-048 Production, Characterization, and Com- Turbine-Combustor Sector Rig Using Swept- Annular Conical Aerospike Nozzle with Free bustion of Nanoaluminum in Composite Solid Wavelength Absorption Spectroscopy stream Effect Propellants 1366 J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX B09-046 High-Pressure Supercritical Turbulent B09-035 Experimental Evaluation of a Low Engine Control Integration and Health Cryogenic Injection and Combustion: A Single- Pressure-Swirl Atomizer Applied Engineering Monitoring Phase Flow Modeling Proposal Design Procedure B09-066 Multiple-Point Adaptive Performance B09-063 Experimental Investigation of a Novel B09-034 Twin-Fluid Atomization and Novel Simulation Tuned to Aeroengine Test-Bed Data Combustor Model for Gas Turbines Lifted Swirl-Stabilized Spray Flames B09-035 Experimental Evaluation of a Low Engine Cooling and Heat Transfer Pressure-Swirl Atomizer Applied Engineering Ducted Rocket Engines B09-079 Circumferential Film Cooling Effective- Design Procedure B09-123 Multi-Objective Optimization of Rock- ness in a LOX/H2 Subscale Combustion Chamber B09-001 Flame Stabilization in High-Pressure et-Based Combined-Cycle Engine Performance B09-045 Film Cooling of Accelerated Flow in a Liquid Oxygen/Methane Rocket Engine Com- Using a Hybrid Evolutionary Algorithm Subscale Combustion Chamber bustion B09-133 Catalyzed Ignition of Using Methane/ Electric Propulsion Engine Performance Hydrogen Fuel in a Microtube for Microthruster Applications B09-038 Influence of Electrode Shape on B09-143 Performance of a Monopropellant B09-032 Reacting Mixing-Layer Computations Performance of Pulsed Magnetoplasmadynamic Thruster Prototype Using Advanced Hydrogen Thruster SIMP-LEX Peroxide Catalytic Beds in a Simulated Turbine-Stator Passage B09-015 Analytic Model for Single-Cycle Deto- B09-039 Langmuir Probe Studies of Magnetic B09-066 Multiple-Point Adaptive Performance nation Tube with Diverging Nozzles Confinement in an Ion Thruster Discharge Plasma Simulation Tuned to Aeroengine Test-Bed Data B09-102 Zero-Dimensional Time-Dependent B09-148 Optimum Design of Turboprop Engines Model of High-Pressure Ablative Capillary Using Genetic Algorithm Combustion Instability Discharge for Plasma Thrusters B09-129 Assessment of Technologies for the B09-077 Validating a Plasma Momentum Flux Silent Aircraft Initiative B09-036 Experimental Investigation of Thermoa- Sensor to an Inverted Pendulum Thrust Stand B09-016 Performance Validation of a Single- coustic Coupling for Low-Swirl Lean Premixed B09-087 Development of a Specific Impulse Tube Pulse Detonation Rocket System Flames Balance for Capillary Discharge Pulsed Plasma B09-053 Submerged Combustion and Two-Phase Thrusters Fuel Cells Exhaust Jet Instabilities B09-064 Adaptive Instability Suppression Con- B09-009 Environmental Testing of NASA's B09-147 Hardware-in-the-Loop Testing of a Fuel trols Method For Aircraft Gas Turbine Engine Evolutionary Xenon Thruster Prototype Model | Cell Aircraft Powerplant Reworked Ion Engine Combustors B09-052 Aluminum Combustion Driven Insta- B09-109 Operation ofa n Annular Helicon Plasma Fuels and Propellants, Properties of Source bilities in Solid Rocket Motors B09-117 Characterization of Nanothermite Ma- B09-130 Methodology and Historical Perspective B09-146 Acoustics, Vortex Shedding, and Low- terial for Solid-Fuel Microthruster Applications of a Hall Thruster Efficiency Analysis Frequency Dynamics Interaction in an Unstable B09-136 Catalytic Cracking and Heat Sink B09-103 Regenerable Field Emission Cathode for Hybrid Rocket Capacity of Aviation Kerosene under Supercritical Spacecraft Neutralization B09-125 Singular Spectrum Analysis Applied to Conditions B09-107 SMART-1 from Conception to Moon Time-Series Measurements in a Self-Excited Tube B09-054 Compatibility of Glycidy! Azide Poly- Impact Combustor mer with Hydroxy! Terminated Polybutadiene and B09-101 Creation of Onset Voltage Hash by B09-114 Flame Spectra of a Turbulent Liquid- Plasticizers Anode Spots in a Magnetoplasmadynamic Fueled Swirl-Stabilized Lean-Direct Injection B09-048 Production, Characterization, and Com- Thruster Combustor bustion of Nanoaluminum in Composite Solid B09-108 Performance Modeling of a Thrust B09-140 Forced Flame Response of Turbulent Propellants Vectoring Device for Hall Effect Thrusters Liquid-Fueled Lean-Direct-Injection Combustion B09-094 Preliminary Investigation on Lithium B09-076 Plume Profiles of a Planar Crossed-Field to Fuel Modulations Hydride as Fuel for Solid-Fueled Scramjet Thruster with Hall Current Injection B09-149 Measurement of Flame Transfer Func- Engines B09-055 Thrust Measurement of a Pure Magnetic tions in Swirl-Stabilized, Lean-Premixed Com- B09-024 Thermoanalytical Screening of Nitro- Sail Using Parallelogram-Pendulum Method bustion gen-Rich Compounds for Ballistic Requirements B09-040 Numerical Study of Plasma Behavior in B09-110 Simulation of Combustion Instabilities of Gun Propellant a Magnetoplasmadynamic Thruster Around in Liquid Rocket Engines with Acoustic B09-083 Pyrolysis/Evaporation Study of Suc- Critical Current Perturbation Equations cinic Acid/Polyvinyl Acetate for Reducing Nozzle B09-132, Dawn lon Propulsion System: Initial Throat Erosion Detonation Checkout after Launch B09-131 Numerical Simulation of SMART-1 B09-090 Review of Recent Developments in Gas Turbine Engines Hall-Thruster Plasma Interactions Wave Rotor Combustion Technology B09-066 Multiple-Point Adaptive Performance B09-010 Deep Space | Flight Spare Ion Thruster B09-142 Thrust Measurement of a Multicycle Simulation Tuned to Aeroengine Test-Bed Data 30,000-Hour Life Test Partially Filled Pulse Detonation Rocket Engine B09-148 Optimum Design of Turboprop Engines B09-062 Investigation of Self-Sustaining Waves Using Genetic Algorithm Emissions and Noises in Metastable Systems: Deflagration to Detona- B09-068 Experimental Investigations of Pressure tion Transition B09-121 Chemical Properties of Aircraft Engine Distortions on the High-Pressure Compressor B09-014 Pressure Measurements and Attenuation Particulate Exhaust Emissions Operating Behavior in a Hybrid Multitube Pulse Detonation Turbine B09-053 Submerged Combustion and Two-Phase B09-129 Assessment of Technologies for the System Exhaust Jet Instabilities Silent Aircraft Initiative B09-015 Analytic Model for Single-Cycle Deto- B09-105 Emissions Reductions in Diesel and B09-118 Comparison of Several Optimization nation Tube with Diverging Nozzles Kerosene Flames Using a Novel Fuel Injector Strategies for Robust Turbine Blade Design B09-016 Performance Validation of a Single- B09-129 Assessment of Technologies for the B09-106 Bayesian Framework for Calibration of Tube Pulse Detonation Rocket System Silent Aircraft Initiative Gas Turbine Simulator B09-138 Resonant Response of Mistuned Bladed Droplet and Spray Characterization Energy Conservation Disks Including Aerodynamic Damping Effects B09-003 Cryogenic Flow and Atomization from a B09-053 Submerged Combustion and Two-Phase B09-034 Twin-Fluid Atomization and Novel Coaxial Injector Exhaust Jet Instabilities Lifted Swirl-Stabilized Spray Flames B09-025 Spray Structure in Near-Injector Region B09-034 Twin-Fluid Atomization and Novel B09-090 Review of Recent Developments in of Aerated Jet in Subsonic Crossflow Lifted Swirl-Stabilized Spray Flames Wave Rotor Combustion Technology J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX 1367 B09-114 Flame Spectra of a Turbulent Liquid- B09-143 Performance of a Monopropellant B09-028 Experiments on Electrically Controlled Fueled Swirl-Stabilized Lean-Direct Injection Thruster Prototype Using Advanced Hydrogen Flameholding on a Plane Wall in a Supersonic Combustor Peroxide Catalytic Beds Airflow B09-033 Gas Turbine Fault Diagnosis Using B09-045 Film Cooling of Accelerated Flow in a B09-095 In-Stream Hypermixer Fueling Pylons Fuzzy-Based Decision Fusion Subscale Combustion Chamber in Supersonic Flow B09-014 Pressure Measurements and Attenuation B09-080 Computational Analysis of the Oxidizer B09-060 Swept-Leading-Edge Pylon Effectson a in a Hybrid Multitube Pulse Detonation Turbine Preflow in an Upper-Stage Rocket Engine Scramjet Pylon-Cavity Flameholder Flowfield System B09-110 Simulation of Combustion Instabilities B09-026 Measurement of Flow Properties and B09-063 Experimental Investigation of a Novel in Liquid Rocket Engines with Acoustic Thrust on Scramjet Nozzle Using Pressure- Combustor Model for Gas Turbines Perturbation Equations Sensitive Paint B09-119 Vane Clocking in a_ Three-Stage B09-093 Oxygen/Hydrogen-Planar-Laser-In- B09-120 Infrared Thermography and Pitot Pres- Compressor: Frequency Domain Data Analysis duced Fluorescence Measurements and Accuracy sure Measurements of a Scramjet Nozzle B09-032 Reacting Mixing-Layer Computations Investigation in High-Pressure Combustion Flowfield in a Simulated Turbine-Stator Passage B09-003 Cryogenic Flow and Atomization from a B09-013 Oscillatory Flows of Rectangular Hy- Coaxial Injector personic Inlet Unstart Caused by Downstream Hybrid Rocket Engines B09-079 Circumferential Film Cooling Effective Mass-Flow Choking B09-005 Large Eddy Simulation of Flow Devel- ness in a LOX/H2 Subscale Combustion Chamber B09-059 Suitability of C2-, C3-Hydrocarbon opment in Chamber with Surface Mass Injection B09-096 Effect of Chamber Backpressure on Fuels for Plasma Ignition in High-Speed Flow B09-085 Predicting Hybrid Propellant Regres- Swirl Injector Fluid Mechanics Rotating Machinery sion Rate Using Response Surfaces B09-088 Condensation-Induced Surface Boiling B09-146 Acoustics, Vortex Shedding, and Low- of Alcohol Fuel Droplets in Combustion B09-138 Resonant Response of Mistuned Bladed Frequency Dynamics Interaction in an Unstable Chambers Disks Including Aerodynamic Damping Effects Hybrid Rocket B09-001 Flame Stabilization in High-Pressure B09-067 Development and Application of an Liquid Oxygen/Methane Rocket Engine Com Arbitrary Lagrangian Eulerian Solver for Turbo- Hypersonic Propulsion bustion machinery Aeromechanics B09-091 Reaction Mechanism of Aluminum- B09-044 Experimental Verification for Acoustic Solid Rocket Motors Damping Enhancement by Gaps in Injector Particle-Air Detonation B09-144_ Numerical Investigation of Roll Torque Formed Baffles B09-135 A Quasi-One-Dimensional Model of Induced by Solid Rocket Motor Internal Flow B09-046 High-Pressure Supercritical Turbulent Hydrogen-Fueled Scramjet Combustors B09-084 Flame-Spreading Behavior in a Fin-Slot Cryogenic Injection and Combustion: A Single- B09-137 Simulation of Supersonic Combustion Solid Propellant Rocket Motor Grain (Part IT) Phase Flow Modeling Proposal in Three Dimensional Configurations B09-115 Nano Additives and Plateau Burning B09-112 Scaling and Evaluation of Pt/Al203 B09-058 Shock-Tunnel Experiments with a Mach Rates of Ammonium-Perchlorate-Based Compo- Catalytic Reactor for Hydrogen Peroxide 12 Rectangular-to-Elliptical Shape-Transition site Solid Propellants Monopropellant Thruster Scramjet at Offdesign Conditions B09-052 Aluminum Combustion Driven Insta- B09-018 Effects of Floating-Ring Seal Clearance B09-027 Probabilistic Aspects of Scramjet De- bilities in Solid Rocket Motors on the Pump Performance for Turbopumps sign B09-145 Single-Phase Internal Flowfield Valida- B09-002 Effect of Recess in High-Pressure B09-029 Effects of Upstream Injection on tion with an Experimental Solid Rocket Motor Liquid Oxygen/Methane Coaxial Injection and Scramjet Performance Using an Entropy-Based Model Combustion Method B09-049 Nanoaluminum as a Solid Propellant Fuel Magnetohydrodynamic Power Generation Ignition B09-097 Experimental Characterization of a B09-062 Investigation of Self-Sustaining Waves B09-008 Feasibility of an Onboard Surface Hall Two-Phase Flowfield in a Solid Rocket Motor in Metastable Systems: Deflagration to Detona- Magnetohydrodynamic Power Generator in Model Reentry Flight tion Transition B09-117 Characterization of Nanothermite Ma- B09-001 Flame Stabilization in High-Pressure Micro Propulsion and Power terial for Solid-Fuel Microthruster Applications Liquid Oxygen/Methane Rocket Engine Com- B09-051 Flowfield Structure in a Fin-Slot Solid bustion B09-089 Liquid Monopropellant Combustion in Rocket Motor (Part I) Mesoscale Vortex Chamber B09-059 Suitability of C2-, C3-Hydrocarbon B09-085 Predicting Hybrid Propellant Regres- Fuels for Plasma Ignition in High-Speed Flow B09-077 Validating a Plasma Momentum Flux sion Rate Using Response Surfaces B09-028 Experiments on Electrically Controlled Sensor to an Inverted Pendulum Thrust Stand B09-048 Production, Characterization, and Com- Flameholding on a Plane Wall in a Supersonic B09-133 Catalyzed Ignition of Using Methane bustion of Nanoaluminum in Composite Solid Airflow Hydrogen Fuel in a Microtube for Microthrustet Propellants B09-133 Catalyzed Ignition of Using Methane/ Applications B09-082 Passive Control of Pressure Oscillations B09-047 Effect of Bulk Density on Reaction in Solid Rocket Motors: Cold-Flow Experiments Hydrogen Fuel in a Microtube for Microthruster Propagation in Nanothermites and Micron Applications B09-083 Pyrolysis/Evaporation Study of Suc- B09-150 Simplified Theory for Ignition Times of Thermites cinic Acid/Polyviny! Aceftora Rteduecin g Nozzle Hypergolic Gelled Propellants Microwaves Throat Erosion B09-012 Microwave and Direct-Current Dis- B09-054 Compatibility of Glycidyl Azide Poly- charges in High-Speed Flow: Fundamentals and B09-011 Thrust Performance of Microwave mer with Hydroxy! Terminated Polybutadiene and Application to Ignition Rocket Under Repetitive-Pulse Operation Plasticizers B09-116 Mitigation of Graphite Nozzle Erosion Ramjets and Scramjets xy Boundary-Layer Control in Solid Propellant Laser Integration/Systems B09-030 Influence of Heat Capacity Ratio on Rocket Motors B09-122 Comparative Study of Plastics as Pressure and Nozzle Flow of a Scramjets B09-006 Fracture Mechanics of Composite Solid Propellants for Laser Ablation Plasma Thrusters B09-025 Spray Structure in Near-Injector Region Rocket Propellant Grains: Material Testing B09-056 Wall-Propelled, In-Tube Propulsion of Aerated Jet in Subsonic Crossflow B09-004_ Chemical Erosion of Refractory-Metal with Repetitive-Pulse Laser Ablation B09-086 Buzz Instability in a Mixed-Compres- Nozzle Inserts in Solid-Propellant Rocket Motors sion Air Intake Liquid Rocket Engines B09-136 Catalytic Cracking and Heat Sink Supersonic Combustion B09-151 Transient Behavior of H2O2 Thruster: Capacity of Aviation Kerosene under Supercritical B09-060 Swept-Leading-Edge Pylon Effects on a Effect of Injector Type and Ullage Volume Conditions Scramjet Pylon-Cavity Flameholder Flowfield 1368 J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX B09-094 Preliminary Investigation on Lithium B09-104 System-Level Feasibility Assessment of B09-041 Impulse Generation on Aluminum Hydride as Fuel for Solid-Fueled Scramjet Microwave Power Beaming for Small Satellites Target Irradiated with Nd:YAG Laser Pulse in Engines Ambient Gas Spacecraft Power B09-117 Characterization of Nanothermite Ma- terial for Solid-Fuel Microthruster Applications B09-104 System-Level Feasibility Assessment of Aerothermodynamics/Thermal Protection B09-064 Adaptive Instability Suppression Con- Microwave Power Beaming for Small Satellites B09-100 Tip-Clearance Effects on Hot-Streak B09-042 Jupiter Power Generation with Electro- Migration in Low-Pressure Stage of Vaneless trols Method For Aircraft Gas Turbine Engine Combustors dynamic Tethers at Constant Orbital Energy Counter-Rotating Turbine B09-027 Probabilistic Aspects of Scramjet De- Spacecraft Propulsion System Integration Boiling/Condensation sign B09-131 Numerical Simulation of SMART-1 B09-088 Condensation-Induced Surface Boiling B09-029 Effects of Upstream Injection on Hall-Thruster Plasma Interactions of Alcohol Fuel Droplets in Combustion Scramjet Performance Using an Entropy-Based Chambers Method Spacecraft Test and Evaluation B09-059 Suitability of C2-, C3-Hydrocarbon B09-132 Dawn Ion Propulsion System: Initial Computational Heat Transfer Fuels for Plasma Ignition in High-Speed Flow Checkout after Launch B09-139 Computational Simulation of Cylindri- B09-010 Deep Space | Flight Spare Ion Thruster cal Film Hole with Jet Pulsation on Flat Plates Transient Combustion 30,000-Hour Life Test B09-062 Investigation of Self-Sustaining Waves Cryogenics B09-078 Ground Test Investigation of Temper- in Metastable Systems: Deflagration to Detona- ature Distribution in Four Parallel High-Altitude B09-043 Comparison of Several Zero-Boil-Off tion Transition Engines Pressure Control Strategies for Cryogenic Fluid Storage in Microgravity Turbomachinery B09-138 Resonant Response of Mistuned Bladed STRUCTURAL MECHANICS Forced Convection Disks Including Aerodynamic Damping Effects AND MATERIALS B09-139 Computational Simulation of Cylindri- B09-100 Tip-Clearance Effects on Hot-Streak cal Film Hole with Jet Pulsation on Flat Plates Migration in Low-Pressure Stage of Vaneless Materials Structural Properties Mixed Convection Counter-Rotating Turbine B09-006 Fracture Mechanics of Composite Solid B09-031 New Simulation Strategy for an Rocket Propellant Grains: Material Testing B09-047 Effect of Bulk Density on Reaction Oscillating Cascade in Turbomachinery Using B09-024 Thermoanalytical Screening of Nitro- Propagation in Nanothermites and Micron Immersed-Boundary Method gen-Rich Compounds for Ballistic Requirements Thermites B09-069 Shock/Boundary-Layer/Tip-Clearance of Gun Propellant Nonintrusive Diagnostics Interaction in a Transonic Rotor Blade B09-018 Effects of Floating-Ring Seal Clearance Structural Durability (Including Fatigue, B09-092 Temperature Measurements in a Gas- on the Pump Performance for Turbopumps Fracture, and Environmental Turbine-Combustor Sector Rig Using Swept- Wavelength Absorption Spectroscopy B09-070 Flow Characteristics of Tip Injection on Degradation) Compressor Rotating Spike via Time-Accurate B09-006 Fracture Mechanics of Composite Solid Radiation Interchange Between Surfaces Simulation Rocket Propellant Grains: Material Testing B09-078 Ground Test Investigation of Temper- B09-119 Vane Clocking in a Three-Stage Thermal Effects ature Distribution in Four Parallel High-Altitude Compressor: Frequency Domain Data Analysis Engines B09-017 Aerothermal Analysis of a Partially B09-078 Ground Test Investigation of Temper- Shrouded Axial Turbine ature Distribution in Four Parallel High-Altitude Thermal Control Engines B09-043 Comparison of Several Zero-Boil-Off SPACE TECHNOLOGY Pressure Control Strategies for Cryogenic Fluid THERMOPHYSICS AND HEAT Storage in Microgravity Mission Design and Analysis TRANSFER Thermochemistry and Chemical Kinetics B09-107 SMART-! from Conception to Moon Impact Ablation, Pyrolysis, Thermal B09-024 Thermoanalytical Screening of Nitro- gen-Rich Compounds for Ballistic Requirements Mission Trajectories (Earth and Decomposition and Degradation of Gun Propellant Interplanetary) B09-077 Validating a Plasma Momentum Flux B09-050 High-Temperature Heterogeneous Re- B09-107 SMART-1! from Conception to Moon Sensor to an Inverted Pendulum Thrust Stand action Kinetics of Tungsten Oxidation by CO2, Impact B09-136 Catalytic Cracking and Heat Sink CO, and O2 Capacity of Aviation Kerosene under Supercritical Space Systems Conditions Thermophysical Properties B09-038 Influence of Electrode Shape on B09-004 Chemical Erosion of Refractory-Metal B09-047 Effect of Bulk Density on Reaction Performance of Pulsed Magnetoplasmadynamic Nozzle Inserts in Solid-Propellant Rocket Motors Propagation in Nanothermites and Micron Thruster SIMP-LEX B09-083 Pyrolysis/Evaporation Study of Suc- Thermites B09-042 Jupiter Power Generation with Electro- cinic Acid/Polyviny! Acetate for Reducing Nozzle B09-111 Thermophysical Properties Measure- dynamic Tethers at Constant Orbital Energy Throat Erosion ments of Rocket Propellants RP-1 and RP-2 J. PROPULSION, VOI 25, NO. 6: 2009 INDEX Author Index Abe, Naoyuki, B09-059 Choi, Chang-Ho, B09-018 Giilhan, Ali, B09-026, B09-030, Kopasakis, George, B09-064 Abhari, Reza S., B09-017 Choi, Hwan Seok, B09-044 B09-120 Kranendonk, Laura Ann, B09-092 Acharya, Ragini, B09-083 Choi, Yoon S., B09-138 Gupta, Ashwani K., B09-003, Kubota, Kenichi, B09-040 Agrawal, Ajay K., B09-105 Choueiri, Edgar Y., B09-101 B09-034, B09-053 Kumaran, K., B09-061 Akbari, Pezhman, B09-090 Costa, Mario, B09-063 Gur, Ohad, B09-074 Kumaresan, K., B09-072 Aleksandrov, Andrew F., B09-012 Couto, Heraldo Silva, B09-035 Gustavsson, Jonas P., B09-093 Kuo, Kenneth K., B09-051, Alofs, Darry] J., B09-065 d’ Agostino, L., B09-143 Haeffele, Bruce, B09-057 B09-083. B09-084 Alyari Shurekhdeli, Shaban, Daimon, Yu, B09-142 Hagelaar, G. J. M., B09-108 Kwon, Sejin, B09-112, B09-151 B09-062 Damse, R. S., B09-024 Hagen, Christopher L., B09-092 Kyriazis, Andreas, B09-033 An, Sungyong, B09-112, B09-151 Dang, Thong, B09-019 Hagen, Donald E., B09-065 acava, Pedro Teixeira, B09-035 Anand, K. V., B09-048 Danila, Daniel, B09-139 Haidn, Oskar, B09-001, B09-002 aesecke, Arno, B09-111 Anderson, Bruce E., B09-121 Dean, Anthony J., B09-014 B09-045, B09-079, BO9-113 afleur, Jarret M., B09-104 Anderson, John A., B09-010 de Groh, Kim, B09-010 Hall, Cesare A., B09-129 ai, Y.H., BO9-124 Anderson, John R., B09-009 DeLaat, John C., B09-064 Hanson, Ronald K., B09-015 arson, C. William, B09-130 Anderson, Paul E., B09-117 De Luca, Luigi, B09-006, B69-049 Hasegawa, Akira, B09-016 aurendeau, Normand M., B09-125 Anthoine, Jerome, B09-082, Demoulin, Francois-Xavier, Hassan, H. A., B09-137 awless, Patrick B., B09-067, B09-097, BO9-145 B09-046 Hathaway, Michael D., B09-070 BO09-119 Apperson, Steven J., B09-117 Dippold, Vance F., B09-020 Heintz, Nicolas, B09-134 ee, Changjin, B09-005 Arias-Zugasti, Manuel, B09-088 Dolotkazin, Iidar, B09-049 Henderson, Jack B., B09-047 Jaiho, BO9-025 Arnold, Richard, B09-045, B09-079 Doolan, Con J., B09-135 Hendrick, Patrick, B09-134 ee, Kwang Jin, B09-044 Auweter-Kurtz, Monika, B09-038, Doster, Jason C., B09-095 Henne, Ulrich, B09-026 Lema, M. R., B09-082, B09-145 B09-075 Duchemin, O., B09-108 Herdrich, Georg, B09-038 eonov, Sergey, B09-028 Babuk, Valery, B09-049 Babu, V., Dutton, J. Craig, BO9-057 Herndon, Scott, B09-121 evitas, Valery I., B0O9-047 B09-061 Dygert, Ryan K., B09-019 Hileman, James I., B09-129 evy, Yeshayahou, B09-063 Balas, Wendy A., B09-117 Endo, Takuma, B09-142 Hirano, Masao, B09-142 J. G., BO9-136 Banks, Bruce, B09-010 Ershov, Alexey P., B09-012 Hirschen, Christian, B09-026 i, Peng, B09-078 Barbour, Ethan A., B09-015 Fan, X. J., BO9-136 B09-030, BO9-120 i, Yi-Guang, B09-066 Bastos-Netto, Demetrio, B09-035 Fassl, Felix, B09-110 Hong, Soon-Sam, B09-018 illy, Taylor C., B09-087 Beal, Brian E., B09-130 Ferrara, Peter J., B09-051, B09-084 Horisawa, Hideyuki, B09-055 inck, Martin B., B09-034, B09-053 Beck, Walter, B09-026 Fleeter, Sanford, B09-067, B09-119, Houim, Ryan W., B09-051 in, Kuo-Cheng, B09-025 Beckstead, Merrill W., B09-007 B09-138 Hsiao, F,C,, B09-124 iu, Feng, B09-032 Behrouzi, Parviz, B09-099 Foster, Lancert E., B09-020 Hsu, Kuang- Yu, B09-095 Lo Gatto, E., B09-066 Benini, Ernesto, B09-069 Frederick, Robert A., B09-085 Huang, Yun, B09-036 Lobo, Prem, B09-065 Bering, Edgar A., B09-077 Freeborn, Andrew B., B09-060 Hulka, James R., B09-096 Longmier, Benjamin W., B09-077 Bezmelnitsyn, Andrey V., B09-117 Fujino, Takayasu, B09-008 Ibarreta, Alfonso F., B09-133 Lorenzini, Enrico C., B09-042 Bhatt, David S., B09-048 Fukunaga, Mihoko, B09-144 Ibrahim, Essam A., B09-017T(C Loth, Eric, B09-057 Biollo, Roberto, B09-069 Fuller, Thomas F., B09-147 Ibrahim, Mounir B., B09-139 Lux, Johannes, B09-001, B09-002 Birzer, Cristian H., B09-135 Funaki, Ikkoh, B09-040, B09-055 Iqbal, Salman, B09-122 Mace, James, B09-057 Bizzarri, Didier, B09-134 Furman, Anthony H., B09-014 Ishikawa, Motoo, B09-008 Majdalani, Joe, B09-098 Black, P. R., B09-149 Galfetti, Luciano, B09-049 Jayaraman, K., B09-048 Makela, Jason M., B09-103 Blacodon, Daniel, B09-037 Gallier, Stany, B09-052 Jayne, John T., B09-121 Manikanda Kumaran, R., B09-072 Boeuf, J. P., BO9-108 Gallimore, Alec D., B09-077, Johnson, Andrew, B09-071 Manu, S. K., B09-054 Bohrk, Hannah, B09-075 B09-130 Johnson, Benjamin P., B09-070 Marinai, Luca, B09-066 Bombardelli, Claudio, B09-042 Gamsov, Alexey, B09-049 Jurczyk, Brian, B09-076 Martin, C. R., BO9-149 Boniface, C., BO9-108 Gangopadhyay, Keshab, B09-117 Kalfas, Anestis 1., B09-017 Mathew, Suresh, B09-054 Boyd, Eric, B09-083 Gangopadhyay, Shubhra, Kappenstein, Charles, B09-151 Mathioudakis, Kostas, B09-033 Bradley, Thomas H., B09-147 BO09-117 Karniotis, Tina A., B09-010 Matsuda, Atsushi, B09-056 Brahmi, Rachid, B09-151 Garner, Charles E., B09-010, Kartuzova, Olga, B09-139 Matsuo, Akiko, B09-142 Brophy, John R., B09-010, BO9-132 B09-132 Kasahara, Jiro, B09-016, BO9-142 Mavris, Dmintri N., B09-147 Brown, Daniel L., B09-130 Garrigues, L., B09-108 Kassemi, Mohammad, B09-043 McGilvray, Matthew, B09-029 Brumback, Karin J., BO9-111 Gautam, Vivek, B09-003 Kasugai, Atsushi, B09-011 McGuirk, James J., B09-099 Bruno, Claudio, B09-094 Gerrard, Keith, B09-091 Keane, Andy J., B09-118 Melo, Mario, B09-063 Carmicino, Carmine, B09-146 Ghenaiet, Adel, B09-148 Keistler, P. G., B09-137 Mento, Christopher A., B09-133 Carro, Rodolphe, B09-115 Ghosh, Mrinal, B09-024 Kenny, R. J., B09-096 Miake-Lye, Richard C., B09-121 Carter, Campbell D., B09-025, Giacomi, Matthew, B09-076 Ketsdever, Andrew, B09-087 Mikes, Steven C., B09-132 B09-028, BO9-095 Glebov, Andrey, B09-049 Key, Nicole L., B09-119 Miles, Jeffrey Hilton, B09-021 Caswell, Andrew W., B09-092 Glover, Tim W., B09-077 Khan, Shakeel A., B09-122 Mirani, Ricardo L., B07-059TC Cervone, A., B09-143 Godfroy, Franck, B09-052 Kim, Dae-Jin, B09-018 Mittal, Sanjay, B09-086 Chakravarthy, Satyanarayanan R., Goebel, Dan M., B09-039 Kim, Hong Jip, B09-044 Moffitt, Blake A., BO9-147 B09-048 Gord, James R., B09-092 Kim, Jinhan, B09-018 Moore, Jeffrey D., B09-051, Chang-Diaz, Franklin R., B09-077 Gottfried, Dana A., B09-067, Kimura, Toshiyuki, B09-055 B09-084 Chang, Clarence T., B09-064 B09-138 King, Galen B., B09-125 Morgan, Richard G., B09-029 Chavers, Greg, B09-077 Granier, John J., B09-047 King, Lyon B., B09-103 Mortimer, I. Phil, BO9-121 Cheng, Felix, B09-032 Gross, Matthew L., B09-007 King, Paul I., B09-060, B09-095 Moser, Marlow D., B09-096 Cheng, Huier, B09-078 Gruber, Mark R., B09-060, B09-095 Kojima, Takayuki, B09-016 Mundt, Christian, B09-068 Chen, Jen-Ping, B09-070 Gualini, Muddassir M. S., B09-122 Komurasaki, Kimiya, B09-011 Mura, Arnaud, B09-046 Chernikov, Vladimir A., B09-012 Guidos, Michael J., B0O9-141 Kontis, Konstantinos, B09-073 Murray, James, B09-134 1370 J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX Naik, N. H., B09-024 Renfro, Michael W., B09-125 Shouse, Dale T., B09-092 Varghese, T. L., B09-054 Nalim, Razi, B09-090 Reuss, Niko, B09-068 Sikder, A. K., B09-024 Venkatesan, Krishna K., B09-125 Nawaz, Anuscheh, B09-038 Rhys, Noah O., B09-096 Simone, Domenico, B09-094 Verma, Shashi Bhushan, B09-081, Na, Yang, B09-005 Ripley, Robert C., B09-091 Sirignano, William, B09-032 B09-113 Nemoto, Toyoshi, B09-016 Romeo, L., B09-143 Smart, Michael K., B09-058 Vivek, P., B09-086 Neuroth, Craig T., B09-092 Romera, Francisco, B09-134 Smirnov, Nickolay N., B09-062 Vivekanand, P. K, B09-072 Ngendakumana, Philippe, B09-134 Rosa Sentinella, Matteo, B09-123 Snyder, John S., B09-009 Volino, Ralph J., B09-139 Nicolich, Steven M., B09-117 Rosen, Aviv, B09-074 Soulas, George C., B09-009 Walker, Mitchell L. R., B09-109 Nikitin, Valeriy F., B09-062 Roser, Hans-Peter, B09-038 Sousa, Jodo, B09-063 Wang, Huishe, B09-100 Ninan, K. N., B09-054 Rosner, Daniel E., B09-088 Squire, Jared P., B09-077 Wang, Ten-See, B09-141 Noble, Andrew C., B09-125 Rovey, Joshua L., B09-076 Staudacher, Stephan, B09-027 Wang, Yanxing, B09-089 Noh, Jun-Gu, B09-018 Ryan, Michael D., B09-095 Steelant, Johan, B09-080, B09-097, Washeleski, Robert L., B09-103 Oda, Yasuhisa, B09-011 Saad, Tony, B09-098 B09-145 Webster, Robert S., B09-070 Ohashi, Ryuta, B09-059 Sabourin, Justin L., B09-050 Stephens, Matthew A., B09-115 /ehrman, Robert B., B09-051 Okuno, Yoshihiro, B09-040 Sakai, Takeharu, B09-041 Stubbers, Robert, B09-076 Werle, Michael J., B09-022 Onasch, Timothy B., B09-121 Sakamoto, Keishi, B09-011 Sudhakar, K., B09-106 West, R., B09-149 Outcalt, Stephanie L., BO9-111 Saleh, Joseph H., B09-104 Sun, Shu, B09-013 Whitefield, Philip D., B09-065 Owens, Allison G., B09-039 Sallam, Khaled A., B09-025 Sun, Xiaofeng, B09-031 Whitehead, Joshua J., B09-085 Pachidis, Vassilios, B09-066 Sanders, Scott T., B09-092 Sundararajan, T., B09-072 Wiese, Michael R., B09-020 Palmer, Douglas D., B09-109 Sane, S. K., B09-106 Sung, Chih-Jen, B09-133, B09-136 Williams, Forman A., B09-150 Panchasara, Heena V., B09-105 Sanmartin, Juan R., BO9-042 Suraweera, Milinda V., B09-058 Worsnop, Douglas R., B09-121 Pancotti, Anthony P., B09-087 Santavicca, Domenic A., B09-114, Suslov, Dmitry, B09-045, B09-079 Wu, Ming-Hsun, B09-089 Pantoya, Michelle L., B09-047 B09-140 Suzuki, Shingo, B09-056 Xiao, Qing, B09-071 Panzarella, Charles H., B09-043 Saouma, Victor, B09-006 Tagade, Piyush M., B09-106 Xiao, X., BO9-137 Papamoschou, Dimitri, B09-071 Sarathi, R., BO9-048 Tajmar, Martin, B09-131 Xu, Jianzhong, B09-100 Parekh, David E., B09-147 Sasoh, Akihiro, B09-056 Takahashi, Koji, B09-011 Yajima, Takashi, B09-016 Pasini, A., BO9-143 Sattelmayer, Thomas, B09-110 Takita, Kenichi, B09-059 Yamaguchi, Hiroyuki, B09-016 Pastrone, Dario, B09-123 Scharlemann, Carsten, B09-131 Tan, Hui-jun, B09-013 Yamakawa, Hiroshi, B09-055 Pekker, Leonid, B09-102 Schmehl, Roland, B09-080 Tayeb, Boulekraa, B09-148 Yang, J.T., BO9-124 Petersen, Eric L., BO9-115 Schmid, Otmar, B09-065 Terzenbach, Robert, B09-006 Yang, Vigor, B09-004, B09-089, Philidis, P., BO9-066 Schneider, Steven J., BO9-133 Thakre, Piyush, B09-004, BO9-116 B09-116 Pieringer, Jutta, BO9-110 Schénherr, Tony, B09-038 Thiruvengadathan, Rajagopalan, Yarantsev, Dmitry, B09-028 Pimenta, Amilcar Porto, B09-035 Schreiber, Willard C., B09-105 B09-117 Yetter, Richard A., B09-050, Porreca, Luca, B09-017 Schiitte, Gerrit, B09-027 Thynell, Stefan, B09-083 B09-089 Presz, Walter M., Jr., BO9-022 Schwartz, Emily, B09-129 Tillotson, Benjamin J., B09-057 Yi, Tongxun, B09-114, BO9-140 Qin, Wenbo, B09-078 Seal, Sudipta, BO9-115 Torre, L., BO9-143 Yin, Zhi-long, B09-013 Racca, Giuseppe D., B09-107 Sedmik, Rene, B09-131 Toth, B., BO9-145 Young, Marcus, B09-087 Raja Manohar, D., B09-072 Segal, Corin, B09-093 Toth, Balazs, B09-097 Yu, G., B09-136 Ramakrishnan, Kishore, B09-067 Sekino, Nobuhiro, B09-144 Trueblood, Max B., B09-065 Yu, Kenneth H., B09-053 Rambaud, P., B09-145 Sengupta, Anita, B09-010, B09-039 Tsai, Her Mann, B09-071 Zare-Behtash, Hossein, B09-073 Ranalli, J. A., BO9-149 Seo, Seonghyeon, B09-044 Tussiwand, Giuseppe S., B09-006 Zhang, Fan, B09-091 Rani, Sarma L., B09-023 Sequera, Daniel E., B09-105 Ueno, Kazuma, B09-055 Zhao, Qingjun, BO9-100 Rasheed, Adam, B09-014 Shibata, Teppei, B09-011 Uribarri, Luke, B09-101 Zhao, Xiaolu, BO9-100 Ratner, Albert, B09-036 Shibkova, Lidia V., B09-012 Vaidyanathan, Aravind, B09-093 Zhong, F. Q., B09-136 Reid, Bryan M., B09-077 Shibkov, Valeriy M., B09-012 Vandsburger, U., B09-149 Zhong, Guohua, B09-031 Reid, David L., B09-115 Shimada, Toru, B09-144 Van Noord, Jonathan L., B09-009 Zurbach, Stephan, B09-046 J. PROPULSION, VOI 25, NO. 6: 2009 INDEX Chronological Index B95-017 Atomization Characteristics of Impinging Liquid Jets. H B09-012 Microwave and Direct-Current Discharges in High-Speed M. Ryan, W. E. Anderson, S. Pal, and R. J. Santoro, Pennsylvania State Flow: Fundamentals and Application to Ignition. Valeriy M. Shibkov, University (11, 1, p. 135) Article Andrew F. Aleksandrov, Vladimir A. Chernikov, Alexey P. Ershov, and Lidia Technical Comment by Essam A. Ibrahim, Alabama A&M University (25, V. Shibkova, Moscow State | rsity, Russia (25, 1, p. 123) Article 6, p. 1361) B09-013 Oscillatory Flows of Rectangular Hypersonic Inlet Unstart B07-059 Direct Experimental Evidence of Electromagnetic Inertia Caused by Downstream Mass-Flow Choking. Hui-jun Tan and Shu Sun, Manipulation Thrusting. Hector H. Brito, Instituto Universitario Nanjing University of Aeronautics and Astronautics, China (PRC); and Zhi- Aeronautico Argentina; and Sergio A. Elaskar, CONICET, Universidad long Yin, Hongdu Aviation Industry Group, China (PRC) (25, 1, p. 138) Nacional de Cordoba, Argentina (23, 2, p. 487) Article based on AIAA Papert Article 2003-4989 Technical Comment by Ricardo L Mirani, Z/nstituto Universitario B09-014 Pressure Measurements and Attenuation in a Hybrid Aeronautico, Argentina (25, 2, p. 543) Multitube Pulse Detonation Turbine System. Adam Rasheed, Anthony H. Furman, and Anthony J. Dean General Ele Global Research (25, 1, p. B09-001 Flame Stabilization in High-Pressure Liquid Oxygen/ 148) Article based on AIAA Paper 2006-1235 Methane Rocket Engine Combustion. Johannes Lux and Oskar Haidn, DLR German Aerospace Center, Germany (25, 1, p. 15) Article BO09-015 Analytic Model for Single-Cycle Detonation Tube with Diverging Nozzles. Ethan A. Barbour and Ronald K. Hanson, Stanford B09-002 Effect of Recess in High-Pressure Liquid Oxygen/Methane University (25, 1, p. 162) Article Coaxial Injection and Combustion. Johannes Lux and Oskar Haidn, DLR German Aerospace Center, Germany (25, 1, p. 24) Article B09-016 Performance Validation of a Single-Tube Pulse Detonation Rocket System. Jiro Kasahara, Akira Hasegawa, Toyoshi Nemoto, and B09-003 Cryogenic Flow and Atomization from a Coaxial Injector. Hiroyuki Yamaguchi, sity of Tsukuba, Japan, Takashi Yajima, /HI Vivek Gautam and Ashwani K. Gupta, University of Maryland (25, 1, p. 33) Aerospace Engineerin Japa and Takayuki Kojima, Japan Aerospace Exploration Agency, Japan (25, 1, p. 173) Article basedo n AIAA Paper 2007- Article SOO B09-004 Chemical Erosion of Refractory-Metal Nozzle Inserts in B09-017 Aerothermal Analysis of a Partially Shrouded Axial Solid-Propellant Rocket Motors. Piyush Thakre and Vigor Yang, Turbine. Luca Porreca, Anestis I. Kalfas, a nd Reza S. Abhari, Swiss Federal Pennsylvania State University (25, 1, p. 40) Article based on AIAA Paper Institute of Technology, S nd (25, 1, p. 181) Article based on AIAA 2008-1030 Paper 2007-1299 B09-005 Large Eddy Simulation of Flow Development in Chamber B09-018 Effects of Floating-Ring Seal Clearance on the Pump with Surface Mass Injection. Changjin Lee and Yang Na, Konkuk University Performance for Turbopumps. Chan Ho Choi, Jun-Gu Noh, Dae-Jin Kim, ROK (25, 1, p. 51) Article based on AIAA Paper 2007-5357 Soon-Sam Hong, and Jinhan Kim, Korea Aerospace Research Institute, ROK (25, 1, p. 191) Article B09-006 Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing. Giuseppe S. Tussiwand, MBDA Bayern-Chemic B09-019 Experimental Investigation of Embedded Crossflow Fan for Germany, Victor Saouma, University of Colorado at Boulder, Robert Airfoil Propulsion/Circulation Control. Ryan K. Dygert and Thong Dang, Terzenbach, MBDA Bayern-Chemie, Germany, and Luigi De Luca Syracuse University (25, 1, p. 196) Article based on AIAA Paper 2007-368 Politecnico di Milano, Italy (25, 1, p. 60) Article B09-020 Computational Analyses of Offset-Stream Nozzles for Noise B09-007 Diffusion Flame Calculations for Composite Propellants Reduction. Vance F. Dippold and Lancert E. Foster, NASA John H. Glenn Using a Vorticity-Velocity Formulation. Matthew | Gross and Merrill W Research Center at Lewis | ind Michael R. Wiese, Analytical Services Beckstead, Brigham Young University (25, 1, p. 74) Article 1 Material(s25 , 1, p. 204) Article bi AITAA Paper 2007-3589 B09-008 Feasibility of an Onboard Surface Hall Magnetohydrody- B09-021 Time Delay Analysis of Turbofan Engine Direct and namic Power Generator in Reentry Flight. Takayasu Fujino and Motoo Indirect Combustion Noise Sources. Jeffrey H. Miles, NASA John H. Glenn Ishikawa, University of Tsukuba, Japan (25, 1, p. 83) Article based on AIAA Research Center at Le / 25. 1, p. 218) Article based on AIAA Paper Paper 2007-4248 2008-50 B09-009 Environmental Testing of NASA’s Evolutionary Xenon B09-022 Shroud and Ejector Augmenters for Subsonic Propulsion Thruster Prototype Model | Reworked Ion Engine. John S. Snyder and and Power Systems. Michael J. Werle 1d Walter M. Presz Jr... FloDesign, John R. Anderson, Jet Propulsion Laboratory, California Institut 2 l,p 228) Article Technology, Jonathan I Van Noord and George C. Soulas, NASA John H Glenn Research Center at Lewis Field (25, 1, p. 94) Article B09-023 Reduced-Order Model for Combustion Instability in a Two- Dimensional Duct with a Flameholder. Sarma | Rani, CFD Research B09-010 Deep Space | Flight Spare lon Thruster 30,000-Hour Life Corporation (25, 1, p. 237) Article based on AIAA Paper 2007-5649 Test. Anita Sengupta, John A. Anderson, Charles Garner, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Kim de Groh B09-024 rhermoanalytical Screening of Nitrogen-Rich Compounds and Bruce Banks, NASA John H. Glenn Research Center at Lewis Field; and for Ballistic Requirements of Gun Propellant. R. S.D amse, Mrinal Ghosh, Tina A. Karniotis, Sherwin-Williams Company (25, |, p. 105) Article based on N. H. Naik, and A. K. Sikder, High Energ) Material Research Laboratory, AIAA Paper 2004-3608 India (25, 1, p. 249) Article B09-011 Thrust Performance of Microwave Rocket Under B09-025 Spray Structure in Near-Injector Region of Aerated Jet in Repetitive-Pulse Operation. Yasuhisa Oda, Teppei Shibata, and Kimiya Subsonic Crossflow. Jaiho Lee and Khaled A. Sallam, Oklahoma State Komurasaki, University of Tokyo, Japan; Koji Takahashi, Atsushi Kasugai, University; Kuo-Cheng Lin, Taitech, Inc.; and Campbell D. Carter, U.S. Air and Keishi Sakamoto, Japan Atomic Energy Agency, Japan (25, 1, p. 118) Force Research Laboratory 2, p. 258) Article based on AIAA Paper 2008- Article 1043 1372 J. PROPULSION, VOL. 25, NO. 6: 2009 INDEX B09-026 Measurement of Flow Properties and Thrust on Scramjet B09-042 Jupiter Power Generation with Electrodynamic Tethers at Nozzle Using Pressure-Sensitive Paint. Christian M. Hirschen, Ali Giilhan, Constant Orbital Energy. Claudio Bombardelli, ESA, The Netherlands: Walter Beck, and Ulrich Henne, DLR, German Aerospace Center, Germany Enrico C. Lorenzini, University of Padova, Italy, and Juan R. Sanmartin, (25, 2, p. 267) Article Universidad Politécnica de Madrid, Spain (25, 2, p. 415) Article B09-027 Probabilistic Aspects of Scramjet Design. Gerrit Schiitte and B09-043 Comparison of Several Zero-Boil-Off Pressure Control Stephan Staudacher, /nstitute of Aircraft Propulsion Systems, Germany (25, 2, Strategies for Cryogenic Fluid Storage in Microgravity. Charles H. p. 281) Article based on AIAA Paper 2008-1811 Panzarella, Equity Engineering Group; and Mohammad Kassemi, NASA John H. Glenn Research Center at Lewis Field (25, 2, p. 424) Article B09-028 Experiments on Electrically Controlled Flameholding on a Plane Wall in a Supersonic Airflow. Sergey Leonov and Dmitry Yarantsev, B09-044 Experimental Verification for Acoustic Damping Enhance- Russian Academy of Sciences, Russia, and Campbell Carter, U.S. Air Force ment by Gaps in Injector-Formed Baffles. Kwang Jin Lee, Hong Jip Kim, Research Laboratory (25, 2, p. 289) Article Seonghyeon Seo, and Hwan Seok Choi, Korea Aerospace Research Institute, - ROK (25, 2, p. 435) Article based on AIAA Paper 2005-4446 B09-029 Effects of Upstream Injection on Scramjet Performance Using an Entropy-Based Method. Matthew McGilvray and Richard G. B09-045 Film Cooling of Accelerated Flow in a Subscale Combustion Morgan, University of Queensland, Australia (25, 2, p. 295) Article Chamber. Richard Armold, Dmitry Suslov, and Oskar J. Haidn, DLR, German B09-030 Influence of Heat Capacity Ratio on Pressure and Nozzle Aerospace Center, Germany (25, 2, p. 443) Article Flow of a Scramjets. Christian Hirschen and Ali Giilhan, DLR, German Aerospace Center, Germany (25, 2, p. 303) Article based on AIAA Paper B09-046 High-Pressure Supercritical Turbulent Cryogenic Injection 2006-8095 and Combustion: A Single-Phase Flow Modeling Proposal. Francois- Xavier Demoulin, Universite de Rouen, France, Stephan Zurbach, Societe B09-031 New Simulation Strategy for an Oscillating Cascade in Nationale d'Etude et de Construction de Moteurs d’Aviation, France; and Turbomachinery Using Immersed-Boundary Method. Xiaofeng Sun and Arnaud Mura, Ecole Nationale Supérieure de Mécanique et d’Aérotechnique, Guohua Zhong, Beijing University of Aeronautics and Astronautics, China France (25, 2, p. 452) Article (PRC) (25, 2, p. 312) Article B09-047 Effect of Bulk Density on Reaction Propagation in B09-032 Reacting Mixing-Layer Computations in a Simulated Nanothermites and Micron Thermites. Michelle L. Pantoya, Texas Tech Turbine-Stator Passage. Felix Cheng, William Sirignano, and Feng Liu, University; Valery 1. Levitas, lowa State University; John J. Granier, Texas University of California, Irvine (25, 2, p. 322) Article Tech University; and Jack B. Henderson, Netzsch Instruments, Inc. (25, 2, p. 465) Article B09-033 Gas Turbine Fault Diagnosis Using Fuzzy-Based Decision Fusion. Andreas Kyriazis and Kostas Mathioudakis, National Technical B09-048 Production, Characterization, and Combustion of Nano- University of Athens, Greece (25, 2, p. 335) Article aluminum in Composite Solid Propellants. K. Jayaraman, K. V. Anand, David S. Bhatt, Satyanarayanan R. Chakravarthy, and R. Sarathi, /ndian B09-034 Twin-Fluid Atomization and Novel Lifted Swirl-Stabilized Institute of Technology-Madras, India (25, 2, p. 471) Article Spray Flames. Martin B. Linck and Ashwani K. Gupta, University of Maryland (25, 2, p. 344) Article B09-049 Nanoaluminum as a Solid Propellant Fuel. Valery Babuk, B09-035 Experimental Evaluation of a Low Pressure-Swirl Atomizer Ildar Dolotkazin, Alexey Gamsov, and Andrey Glebov, Baltic State Technical Applied Engineering Design Procedure. Heraldo Couto, Center for University, Russia; Luigi DeLuca and Luciano Galfetti, Politecnico di Milano, Technology in Energy, Brazil; Pedro T. Lacava, Aeronautical Technology Italy (25, 2, p. 482) Article Institute, Brazil; Demetrio Bastos-Netto, Center for Technology in Energy, Brazil, and Amilcar P. Pimenta, Aeronautical Technology Institute, Brazil (25, B09-050 High-Temperature Heterogeneous Reaction Kinetics of 2, p. 358) Article Tungsten Oxidation by CO2, CO, and O2. Justin L. Sabourin and Richard A. Yetter, Pennsylvania State University (25, 2, p. 490) Article B09-036 Experimental Investigation of Thermoacoustic Coupling for Low-Swirl Lean Premixed Flames.Yun Huang and Albert Ratner, B09-051 Flowfield Structure in a Fin-Slot Solid Rocket Motor (Part University of lowa (25, 2, p. 365) Article 1). Jeffrey D. Moore, Robert B. Wehrman, Kenneth K. Kuo, Peter J. Ferrara, and Ryan W. Houim, Pennsylvania State University (25, 2, p. 499) Article B09-037 Combustion-Noise Characterization of a Turbofan Engine based on AIAA Paper 2006-4772 with a Spectral Estimation Method. Daniel Blacodon, ONERA, France (25, 2, p. 374) Article based on AIAA Paper 2008-2940 B09-052 Aluminum Combustion Driven Instabilities in Solid Rocket Motors. Stany Gallier and Franck Godfroy, SVPE Matériaux Energétiques, B09-038 Influence of Electrode Shape on Performance of Pulsed France (25, 2, p. 509) Article Magnetoplasmadynamic Thruster SIMP-LEX. Tony Schénherr, Anuscheh Nawaz, Georg Herdrich, Hans-Peter Roser, and Monika Auweter-Kurtz, B09-053 Submerged Combustion and Two-Phase Exhaust Jet Universitdt Stuttgart, Germany (25, 2, p. 380) Article Instabilities. Martin B. Linck, Ashwani K. Gupta, and Kenneth H. Yu, University of Maryland (25, 2, p. 522) Article B09-039 Langmuir Probe Studies of Magnetic Confinement in an [on Thruster Discharge Plasma. Anita Sengupta, Dan M. Goebel, and Allison G. Owens, Jet Propulsion Laboratory, California Institute of Technology (25, 2, B09-054 Compatibility of Glycidyl Azide Polymer with Hydroxyl p. 387) Article based on AIAA Paper 2005-4069 Terminated Polybutadiene and Plasticizers. S. K. Manu and T. L. Varghese, Vikram Sarabhai Space Centre, India; Suresh Mathew, Mahatma Gandhi B09-040 Numerical Study of Plasma Behavior in a Magneto- University, India; and K. N. Ninan, Vikram Sarabhai Space Centre, India (25, plasmadynamic Thruster Around Critical Current. Kenichi Kubota, 2, p. 533) Technical Note Tokyo Institute of Technology, Japan; \kkoh Funaki, Japan Aerospace Exploration Agency, Japan; and Yoshihiro Okuno, Tokyo Institute of B09-055 Thrust Measurement of a Pure Magnetic Sail Using Technology, Japan (25, 2, p. 397) Article Parallelogram-Pendulum Method. Kazuma Ueno, Graduate University for Advanced Studies, Japan, \kkoh Funaki, Japan Aerospace Exploration B09-041 Impulse Generation on Aluminum Target Irradiated with Agency, Japan; Toshiyuki Kimura and Hideyuki Horisawa, Tokai University, Nd:YAG Laser Pulse in Ambient Gas. Takeharu Sakai, Nagoya University, Japan, and Hiroshi Yamakawa, Kyoto University, Japan (25, 2, p. 536) Japan (25, 2, p. 406) Article based on AIAA Paper 2008-1080 Technical Note