Journal of Spacecraft and Rockets 2002: Vol 39 Index

13 Pages·2002·3.9 MB·English

JOURNAL OF SPACECRAFT AND ROCKETS
Volume 39, No. 6, November—December 2002
2002 Journal of Spacecraft and Rockets Index
How to Use the Index
In the Subject Index, pages 936-940, 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, page 941-942, lists all authors associated with a given technical paper. The locating numbers are identical
to those in the Subject Index. The Chronological Index, pages 943-947, 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, as well as the ISBN number if the paper was published
in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they
refer. If the paper to which they refer was published prior to 2002, 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, Conventional, Simulation Hypersonic Flow
STOL/VTOL
A02-080 Identification of Influential Uncertain- A02-124 Aerodynamics of Two Side-by-Side
ties in Monte Carlo Analysis Plates in Hypersonic Rarefied-Gas Flows
Aerodynamics
A02-029 Three-Dimensional Simulation: Micro- A02-079 Applications of a Counterflow Drag
A02-124 Aerodynamics of Two Side-by-Side gravity Environments and Applications Reduction Technique in High-Speed Systems
Plates in Hypersonic Rarefied-Gas Flows A02-034 Experimental and Numerical Investi-
Structural Design (Including Loads)
A02-079 Applications of a Counterflow Drag gation on Martian Atmosphere Entry
Reduction Technique in High-Speed Systems A02-088 Design Study of a Square Solar Sail A02-033 Frequency Response of Pneumatic
A02-034 Experimental and Numerical Investi- Architecture Tubing and Pressure Sensor Configurations in
gation on Martian Atmosphere Entry Slip-Flow Conditions
A02-033 Frequency Response of Pneumatic Structural Materials
A02-049 Hypersonic Flow over a Blunt Body
Tubing and Pressure Sensor Configurations in
A02-115 Time-Dependent Response of Thin with Plasma Injection
Slip-Flow Conditions
Film Piezoelectric Polymer Polyvinylidene A02-125 Power-Law Shaped Leading Edges in
A02-049 Hypersonic Flow over a Blunt Body
Fluoride Rarefied Hypersonic Flow
with Plasma Injection
A02-108 Supersonic/Hypersonic Flutter and
Vibration
Aeroelasticity and Aeroservoelasticity Postflutter of Geometrically Imperfect Circular
A02-031 Six-Axis Vibration Isolation System Cylindrical Panels
A02-009 Flutter Analysis of a Wraparound Fin
Using Soft Actuators and Multiple Sensors
Projectile Considering Rolling Motion Jets, Wakes, and Viscid-Inviscid Flow
A02-108 Supersonic/Hypersonic Flutter and Interactions
Fluid Dynamics
Postflutter of Geometrically Imperfect Circular
Cylindrical Panels A02-048 Comprehensive Numerical Study of
Boundary-Layer Stability and Transition Jet-Flow Impingement over Flat Plates
Aerospace Plane
A02-078 Drag Reduction on Blunt-Based Vehi- A02-026 Modeling of the Interaction of a Side
A02-078 Drag Reduction on Blunt-Based Vehi- cles Using Forebody Surface Roughness Jet with a Rarefied Atmosphere
cles Using Forebody Surface Roughness A02-025 Review and Synthesis of Roughness- A02-050 Numerical Investigation of Supersonic
Dominated Transition Correlations for Reentry Jet Interaction for Finned Bodies
Cabin Environment, Crew Training, and
Applications
Life Support Multiphase Flows
Computational Fluid Dynamics
A02-029 Three-Dimensional Simulation: Micro- A02-040 Modeling of Chill Down in Cryogenic
gravity Environments and Applications A02-048 Comprehensive Numerical Study of Transfer Lines
Jet-Flow Impingement over Flat Plates
Flight Mechanics Plasmadynamics and MHD
A02-034 Experimental and Numerical Investi-
A02-005 To the Far Side of the Sun Using Venus gation on Martian Atmosphere Entry A02-049 Hypersonic Flow over a Blunt Body
Gravity Assist A02-057 Numerical Analysis on Separation with Plasma Injection
Dynamics of Strap-On Boosters in the Atmos- A02-054 Particle-in-Cell with Monte Carlo Sim-
Powerplant Integration
phere ulation of SPT-100 Exhaust Plumes
A02-017 Design of a Hybrid Chemical/Electric A02-050 Numerical Investigation of Supersonic A02-123 Plume Study of a 1.35-kW SPT-100
Propulsion Orbital Transfer Vehicle Jet Interaction for Finned Bodies Using an ExB Probe
936
JOURNAL OF SPACECRAFT AND ROCKETS
Volume 39, No. 6, November—December 2002
2002 Journal of Spacecraft and Rockets Index
How to Use the Index
In the Subject Index, pages 936-940, 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, page 941-942, lists all authors associated with a given technical paper. The locating numbers are identical
to those in the Subject Index. The Chronological Index, pages 943-947, 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, as well as the ISBN number if the paper was published
in a bound collection of meetings papers. Comments, Replies, and Errata are listed directly beneath the paper to which they
refer. If the paper to which they refer was published prior to 2002, 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, Conventional, Simulation Hypersonic Flow
STOL/VTOL
A02-080 Identification of Influential Uncertain- A02-124 Aerodynamics of Two Side-by-Side
ties in Monte Carlo Analysis Plates in Hypersonic Rarefied-Gas Flows
Aerodynamics
A02-029 Three-Dimensional Simulation: Micro- A02-079 Applications of a Counterflow Drag
A02-124 Aerodynamics of Two Side-by-Side gravity Environments and Applications Reduction Technique in High-Speed Systems
Plates in Hypersonic Rarefied-Gas Flows A02-034 Experimental and Numerical Investi-
Structural Design (Including Loads)
A02-079 Applications of a Counterflow Drag gation on Martian Atmosphere Entry
Reduction Technique in High-Speed Systems A02-088 Design Study of a Square Solar Sail A02-033 Frequency Response of Pneumatic
A02-034 Experimental and Numerical Investi- Architecture Tubing and Pressure Sensor Configurations in
gation on Martian Atmosphere Entry Slip-Flow Conditions
A02-033 Frequency Response of Pneumatic Structural Materials
A02-049 Hypersonic Flow over a Blunt Body
Tubing and Pressure Sensor Configurations in
A02-115 Time-Dependent Response of Thin with Plasma Injection
Slip-Flow Conditions
Film Piezoelectric Polymer Polyvinylidene A02-125 Power-Law Shaped Leading Edges in
A02-049 Hypersonic Flow over a Blunt Body
Fluoride Rarefied Hypersonic Flow
with Plasma Injection
A02-108 Supersonic/Hypersonic Flutter and
Vibration
Aeroelasticity and Aeroservoelasticity Postflutter of Geometrically Imperfect Circular
A02-031 Six-Axis Vibration Isolation System Cylindrical Panels
A02-009 Flutter Analysis of a Wraparound Fin
Using Soft Actuators and Multiple Sensors
Projectile Considering Rolling Motion Jets, Wakes, and Viscid-Inviscid Flow
A02-108 Supersonic/Hypersonic Flutter and Interactions
Fluid Dynamics
Postflutter of Geometrically Imperfect Circular
Cylindrical Panels A02-048 Comprehensive Numerical Study of
Boundary-Layer Stability and Transition Jet-Flow Impingement over Flat Plates
Aerospace Plane
A02-078 Drag Reduction on Blunt-Based Vehi- A02-026 Modeling of the Interaction of a Side
A02-078 Drag Reduction on Blunt-Based Vehi- cles Using Forebody Surface Roughness Jet with a Rarefied Atmosphere
cles Using Forebody Surface Roughness A02-025 Review and Synthesis of Roughness- A02-050 Numerical Investigation of Supersonic
Dominated Transition Correlations for Reentry Jet Interaction for Finned Bodies
Cabin Environment, Crew Training, and
Applications
Life Support Multiphase Flows
Computational Fluid Dynamics
A02-029 Three-Dimensional Simulation: Micro- A02-040 Modeling of Chill Down in Cryogenic
gravity Environments and Applications A02-048 Comprehensive Numerical Study of Transfer Lines
Jet-Flow Impingement over Flat Plates
Flight Mechanics Plasmadynamics and MHD
A02-034 Experimental and Numerical Investi-
A02-005 To the Far Side of the Sun Using Venus gation on Martian Atmosphere Entry A02-049 Hypersonic Flow over a Blunt Body
Gravity Assist A02-057 Numerical Analysis on Separation with Plasma Injection
Dynamics of Strap-On Boosters in the Atmos- A02-054 Particle-in-Cell with Monte Carlo Sim-
Powerplant Integration
phere ulation of SPT-100 Exhaust Plumes
A02-017 Design of a Hybrid Chemical/Electric A02-050 Numerical Investigation of Supersonic A02-123 Plume Study of a 1.35-kW SPT-100
Propulsion Orbital Transfer Vehicle Jet Interaction for Finned Bodies Using an ExB Probe
936
937 J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX
Rarefied Flows Control System Sensors A02-038 Hardware Experiments of a Truss
Assembly by an Autonomous Space Learning
A02-124 Aerodynamics of Two Side-by-Side A02-010 Determining Angular Velocity and
Robot
Plates in Hypersonic Rarefied-Gas Flows Angular Acceleration of Projectiles Using Triax-
A02-117 Orbit Determination for the QuikSCAT
A02-033 Frequency Response of Pneumatic ial Acceleration Measurements
Spacecraft
Tubing and Pressure Sensor Configurations in
Dynamics
Slip-Flow Conditions State Estimation
A02-026 Modeling of the Interaction of a Side A02-083 Atmospheric Reentry Modeling and
A02-116 Estimation and Prediction of Orbital
Jet with a Rarefied Atmosphere Simulation
Debris Reentry Trajectories
A02-125 Power-Law Shaped Leading Edges in A02-096 Resistive Deployment of Inflatable
A02-107 Orbit Determination of Spacecraft
Rarefied Hypersonic Flow Structures Using Velcro
Using Global Positioning System Single-Fre-
Separated Flows Fiber Optics quency Measurement
A02-056 Mean and Fluctuating Pressure in A02-024 Fiber-Optic Sensors for the Study of Structural Control
Boat-Tail Separated Flows at Transonic Speeds Spacecraft-Thruster Interactions: lon Sputtering
A02-045 Thermally-Induced Attitude Distur-
Supersonic Flow Flight Mechanics bance Control for a Spacecraft with a Flexible
Boom
A02-108 Supersonic/Hypersonic Flutter and A02-083 Atmospheric Reentry Modeling and
Postflutter of Geometrically Imperfect Circular Simulation Trajectory Optimization
Cylindrical Panels A02-007 Dynamic Stability of Blunt Atmos-
A02-079 Applications of a Counterflow Drag
Transonic Flow pheric Entry Configurations Reduction Technique in High-Speed Systems
A02-051 Linearized Motion of a Fin-Stabilized A02-083 Atmospheric Reentry Modeling and
A02-056 Mean and Fluctuating Pressure in Projectile Subjected to a Lateral Impulse Simulation
Boat-Tail Separated Flows at Transonic Speeds
Launch Vehicle Guidance and Control A02-069 Initial Guess Generation for Rocket
Viscous Non-Boundary-Layer Flows Ascent Trajectory Optimization Using Indirect
A02-069 Initial Guess Generation for Rocket Methods
A02-078 Drag Reduction on Blunt-Based Vehi- Ascent Trajectory Optimization Using Indirect A02-118 Optimal Spacecraft Rendezvous Using
cles Using Forebody Surface Roughness Methods Genetic Algorithms
A02-005 To the Far Side of the Sun Using Venus
Missile Dynamics
Guidance, Control, and Dynamics Gravity Assist
Technology A02-010 Determining Angular Velocity and
Angular Acceleration of Projectiles Using Triax- Interdisciplinary Topics
Astrodynamics ial Acceleration Measurements
A02-051 Linearized Motion of a Fin-Stabilized Aerospace Management
A02-002 Automated Design of the Europa
Projectile Subjected to a Lateral Impulse
Orbiter Tour A02-036 Spacecraft Design Lifetime
A02-071 Collision Risk Posed to the Global Missile Guidance and Control
Aerospace Technology Utilization
Positioning System by Disposal Orbit Instability
A02-010 Determining Angular Velocity and
A02-003 Design of Aerogravity-Assist A02-065 Cellular Automata-Based Reconfig-
Angular Acceleration of Projectiles Using Triax-
Trajectories urable Systems as Transitional Approach to
ial Acceleration Measurements
A02-072 Energetic Cost and Viability of the Pro- Gigascale Electronic Architectures
posed Space Debris Mitigation Measures Optimization Techniques
Analytical and Numerical Methods
A02-116 Estimation and Prediction of Orbital
A02-118 Optimal Spacecraft Rendezvous Using
Debris Reentry Trajectories A02-053 Plasma Response to Jump of Insulator
Genetic Algorithms
A02-001 Graphical Method for Gravity-Assist Surface Potential in lonospheric Plasma
Trajectory Design Pointing Systems Environment
A02-118 Optimal Spacecraft Rendezvous Using A02-110 Simplified Algorithm for Short Target-
Genetic Algorithms A02-043 Condition Monitoring of Filament- Approach Paths in Orbit
A02-117 Orbit Determination for the QuikSCAT Wound Composite Flywheels Having Circum-
Spacecraft ferential Cracks Atmospheric and Space Sciences
A02-107 Orbit Determination of Spacecraft Signal Processing A02-044 lonospheric Specification and Forecast
Using Global Positioning System Single-Fre- Modeling
quency Measurement A02-065 Cellular Automata-Based Reconfig- A02-093 Multilayered Polymer Mirror
A02-012 Orbital Debris Environment Model in urable Systems as Transitional Approach to Experiment
the Geosynchronous Region Gigascale Electronic Architectures
Environmental Effects
A02-005 To the Far Side of the Sun Using Venus
Software Technology
Gravity Assist A02-072 Energetic Cost and Viability of the Pro-
A02-064 Advances in Data Handling Systems posed Space Debris Mitigation Measures
Computer Science
for Space Experiment Control A02-014 Hazards of Hypervelocity Impacts on
A02-065 Cellular Automata-Based Reconfig- Spacecraft
Spacecraft Dynamics
urable Systems as Transitional Approach to A02-053 Plasma Response to Jump of Insulator
Gigascale Electronic Architectures A02-047 Plasma Propulsion Options for Multi- Surface Potential in lonospheric Plasma
A02-080 Identification of Influential Uncertain- ple Terrestrial Planet Finder Architectures Environment
ties in Monte Carlo Analysis A02-102 Satellite Attitude Stabilization Through
Lasers and Laser Applications
Kite-Like Tether Configuration
Control System Design
A02-045 Thermally-Induced Attitude Distur- A02-037 Laser Elevator: Momentum Transfer
A02-070 Evolved Seasparrow Missile Jet Vane bance Control for a Spacecraft with a Flexible Using an Optical Resonator
Control System Prototype Hardware Boom A02-011 Laser Radiation for Cleaning Lower
Development Earth Orbits
Spacecraft Guidance and Control
A02-038 Hardware Experiments of a Truss A02-055 Optimized Solutions for Kistler K-1
Assembly by an Autonomous Space Learning A02-032 Dynamic Model and Control of Mass- Branching Trajectories Using Multidisciplinary
Robot Distributed Tether Satellite System Design OptimizationTechniques
J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX 938
Multidisciplinary Design Optimization A02-055 Optimized Solutions for Kistler K-1 Humans in Space/Life Support Systems,
Branching Trajectories Using Multidisciplinary EVA
402-019 Cost-Optimum Electric Propulsion for
Design OptimizationTechniques
Constellations A02-029 Three-Dimensional Simulation: Micro-
402-103 Optimization of Double Link Transmi- Vibration gravity Environments and Applications
sion in Case in Hybrid Orbit Satellite
Constellations A02-009 Flutter Analysis of a Wraparound Fin Mission Design and Analysis
Projectile Considering Rolling Motion
A02-100 Arizona State University Satellite
Safety
(ASUSat1): Low-Cost, Student-Designed
402-011 Laser Radiation for Cleaning Lower Propulsion Nanosatellite
Earth Orbits 402-002 Automated Design of the Europa
402-012 Orbital Debris Environment Model in Advanced Space Propulsion Orbiter Tour
the Geosynchronous Region 402-030 Analysis of Bare-Tether Systems for 402-019 Cost-Optimum Electric Propulsion for
Deorbiting Low-Earth-Orbit Satellites Constellations
Sensor Systems
402-017 Design of a Hybrid Chemical/Electric A02-003 Design of Aerogravity-Assist Trajecto-
402-093 Multilayered Polymer Mirror Propulsion Orbital Transfer Vehicle ries
Experiment 402-037 Laser Elevator: Momentum Transfer A02-077 Design of the First InterplanetarySolar
Using an Optical Resonator Electric Propulsion Mission
Launch Vehicle and Missile (LV/M) 402-128 Payload Mass Fraction Optimization A02-072 Energetic Cost and Viability of the Pro-
Technology for Solar Sail Cargo Missions posed Space Debris Mitigation Measures
A02-001 Graphical Method for Gravity-Assist
402-120 Realizing “2001: A Space Odyssey”:
Aerodynamics Piloted Spherical Torus Nuclear Fusion Trajectory Design
A02-103 Optimization of Double Link Transmi-
Propulsion
402-008 Improved Semi-Empirical Method for sion in Case in Hybrid Orbit Satellite Constella-
Power-On Base-Drag Prediction Electric Propulsion tions
402-050 Numerical Investigation of Supersonic A02-128 Payload Mass Fraction Optimization
Jet Interaction for Finned Bodies 402-030 Analysis of Bare-Tether Systems for for Solar Sail Cargo Missions
402-082 Sabot Opening Lift Force: Analysis, Deorbiting Low-Earth-Orbit Satellites A02-036 Spacecraft Design Lifetime
Computation, and Test 402-019 Cost-Optimum Electric Propulsion for A02-016 Two-Stage Launch Vehicles For Heavy
Constellations
Payloads
Configuration Design A02-017 Design of a Hybrid Chemical/Electric
402-075 First Stage Design Variations of Par- Propulsion Orbital Transfer Vehicle Mission Trajectories (Earth and
tially Reusable Launch Vehicles 402-077 Design of the First InterplanetarySolar Interplanetary)
402-008 Improved Semi-Empirical Method for Electric Propulsion Mission A02-002 Automated Design of the Europa
Power-On Base-Drag Prediction A02-121 Electric Propulsion Plasma Simula- Orbiter Tour
402-111 Low-Cost Small-Satellite Delivery tions and Influence on Spacecraft Charging A02-03 Design of Aerogravity-Assist
System A02-027 Electric Propulsion Space Experiment
Trajectories
A02-057 Numerical Analysis on Separation (ESEX) On-Orbit Results
A02-077 Design of the First InterplanetarySolar
Dynamics of Strap-On Boosters in the Atmos- A02-024 Fiber-Optic Sensors for the Study of
Electric Propulsion Mission
phere Spacecraft-Thruster Interactions: lon Sputtering
A02-001 Graphical Method for Gravity-Assist
402-016 Two-Stage Launch Vehicles for Heavy 402-015 Impact Analysis of Hall Thrusters on
Trajectory Design
Payloads Satellite Antenna Performance A02-128 Payload Mass Fraction Optimization
Launch Vehicle and Sounding Rocket 402-047 Plasma Propulsion Options for Multi- for Solar Sail Cargo Missions
Systems ple Terrestrial Planet Finder Architectures 402-110 Simplified Algorithm for Short Target-
402-123 Plume Study of a 1.35-kW SPT-100 Approach Paths in Orbit
402-075 First Stage Design Variations of Par- Using an ExB Probe
tially Reusable Launch Vehicles Space Experiments
Engine Materials
402-111 Low-Cost Small-Satellite Delivery A02-064. Advances in Data Handling Systems
Sy stem 402-018 New Failure Criterion for Space Shut- for Space Experiment Control
A02-055 Optimized Solutions for Kistler K-1 tle Main Engine Turbine Blades A02-058 Effects of Ambient Air Exposure on
Branching Trajectories Using Multidisciplinary Atomic Oxygen-Exposed Kapton-H Films
Design OptimizationTechniques Liquid Rocket Engines A02-027 Electric Propulsion Space Experiment
402-016 Two-Stage Launch Vehicles for Heavy A02-018 New Failure Criterion for Space Shut- (ESEX) On-Orbit Results
Payloads
tle Main Engine Turbine Blades
Space Processing
Missile Systems
Solid Rocket Motors
402-064 Advances in Data Handling Systems
402-008 Improved Semi-Empirical Method for 402-070 Evolved Seasparrow Missile Jet Vane for Space Experiment Control
Power-On Base-Drag Prediction
Control System Prototype Hardware
Space Systems
Mission Studies and Economics Development
A02-030 Analysis of Bare-Tether Systems for
402-047 Plasma Propulsion Options for Mullti- Space Technology Deorbiting Low-Earth-Orbit Satellites
ple Terrestrial Planet Finder Architectures
A02-100 Arizona State University Satellite
Propulsion and Propellant Systems Aerobraking Flight Mechanics (ASUSat1): Low-Cost, Student-Designed
Nanosatellite
402-088 Design Study of a Square Solar Sail 402-007 Dynamic Stability of Blunt Atmos- A02-071 Collision Risk Posed to the Global
Architecture pheric Entry Configurations Positioning System by Disposal Orbit Instability
402-037 Laser Elevator: Momentum Transfer Global Positioning System A02-032. Dynamic Model and Control of Mass-
Using an Optical Resonator Distributed Tether Satellite System
402-071 Collision Risk Posed to the Global A02-038 Hardware Experiments of a Truss
Trajectories and Tracking Systems
Positioning System by Disposal Orbit Instability Assembly by an Autonomous Space Learning
402-069 Initial Guess Generation for Rocket 402-107 Orbit Determination of Spacecraft Robot
Ascent Trajectory Optimization Using Indirect Using Global Positioning System Single-Fre- A02-014 Hazards of Hypervelocity Impacts on
Methods quency Measurement Spacecraft
939 J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX
A02-021 In-Flight Estimation of the Cassini Spacecraft Structural Configuration, Structural Composite Materials
Spacecraft’s Inertia Tensor Design, and Analysis
402-059 Detection of Hydrogen Leakage in a
A02-011 Laser Radiation for Cleaning Lower
402-100 Arizona State University Satellite Composite Sandwich Structure at Cryogenic
Earth Orbits
(ASUSatl): Low-Cost, Student-Designed Temperature
A02-028 Mir Solar-Array Return Experiment:
Nanosatellite 402-087 Dimensional Repeatability of an Elas-
Power Performance Measurements and Molecu- 402-087 Dimensional Repeatability of an Elas- tically Folded Composite Hinge for Deployed
lar Contamination Analysis Results tically Folded Composite Hinge for Deployed Spacecraft Optics
402-076 Parametric Analysis of Fiber-Rein- Spacecraft Optics 402-076 Parametric Analysis of Fiber-Rein-
forced Laminated Momentum Wheel Rotors 402-089 Geometric Imperfection Effects in an forced Laminated Momentum Wheel Rotors
402-102 Satellite Attitude Stabilization Through Elastically Deployable Isogrid Column 402-091 Rational for Defining Structural
Kite-Like Tether Configuration A02-042 Local Effects of Piezopolymer Patches Requirements for Large Space Telescopes
A02-073 Space Systems Flexibility Provided by on Inflatable Space-Based Structures
On-Orbit Servicing: Part | 402-091 Rational for Defining Structural Structural Design
402-074 Space Systems Flexibility Provided by Requirements for Large Space Telescopes
402-095 Deployable Tensegrity Reflectors for
On-Orbit Servicing: Part 2
Spacecraft Test and Evaluation Small Satellites
402-036 Spacecraft Design Lifetime 402-023, Fundamental Frequency of Rocket and
402-059 Detection of Hydrogen Leakage in a
Spacecraft Attitude Determination Composite Sandwich Structure at Cryogenic Missile Upper Stages: Quick Preliminary Design
Solution
Temperature
A02-060 Everything Is Relative in Spacecratt 402-076 Parametric Analysis of Fiber-Rein-
402-007 Dynamic Stability of Blunt Atmos-
System Alignment Calibration forced Laminated Momentum Wheel Rotors
pheric Entry Configurations
402-091 Rational for Defining Structural
Spacecraft Communication
Spacecraft Thermal Management Requirements for Large Space Telescopes
A02-015 Impact Analysis of Hall Thrusters on A02-092 Self-Rigidizable Space Inflatable
A02-006 Design Considerations When Using
Satellite Antenna Performance Edge-Mounted Heat Pipes in Space Radiators Boom
A02-103 Optimization of Double Link Transmi- 402-058 Effects of Ambient Air Exposure on Structural Durability (Including Fatigue,
sion in Case in Hybrid Orbit Satellite Constella- Atomic Oxygen-Exposed Kapton-H Films
Fracture, and Environmental
tions A02-114 Electron, Proton, and Ultraviolet Radi-
Degradation)
ation Effects on Thermophysical Properties of
Spacecraft Contamination/Sterilization
Polymeric Films A02-043 Condition Monitoring of Filament-
A02-026 Modeling of the Interaction of a Side A02-046 Review of Spacecraft Cryogenic Wound Composite Flywheels Having Circum-
Jet with a Rarefied Atmosphere Coolers ferential Cracks
A02-020 Spacecraft Thermal Analysis and Con- 402-059 Detection of Hydrogen Leakage in a
Spacecraft Power trol by Thermal Energy Optimum Distribution Composite Sandwich Structure at Cryogenic
A02-043 Condition Monitoring of Filament- Temperature
Wound Composite Flywheels Having Circum- Structural Mechanics and 402-022 Impingement Angle Dependence of
ferential Cracks Materials Erosion Rate of Polyimide in Atomic Oxygen
A02-006 Design Considerations When Using Exposures
Edge-Mounted Heat Pipes in Space Radiators Dynamic Model Analysis A02-115 Time-Dependent Response of Thin
A02-028 Mir Solar-Array Return Experiment: A02-032. Dynamic Model and Control of Mass- Film Piezoelectric Polymer Polyvinylidene
Power Performance Measurements and Molecu- Distributed Tether Satellite System Fluoride
lar Contamination Analysis Results A02-098 Modeling a Piezothermoelastic Structural Dynamics and
A02-053 Plasma Response to Jump of Insulator Beam-String Characterization
Surface Potential in lonospheric Plasma Envi-
Flexible and Active Structures
ronment 402-009 Flutter Analysis of a Wraparound Fin
402-120 Realizing “2001: A Space Odyssey”: A02-095 Deployable Tensegrity Reflectors for Projectile Considering Rolling Motion
Piloted Spherical Torus Nuclear Fusion Small Satellites 402-023 Fundamental Frequency of Rocket and
Propulsion 402-042 Local Effects of Piezopolymer Patches Missile Upper Stages: Quick Preliminary Design
on Inflatable Space-Based Structures Solution
Spacecraft Propulsion System A02-098 Modeling a Piezothermoelastic 402-042 Local Effects of Piezopolymer Patches
Integration Beam-String on Inflatable Space-Based Structures
402-096 Resistive Deployment of Inflatable A02-099 Nonlinear Pressurization and Modal
A02-121 Electric Propulsion Plasma Simula- Structures Using Velcro Analysis Procedure for Dynamic Modeling of
tions and Influence on Spacecraft Charging A02-031 Six-Axis Vibration Isolation System Inflatable Structures
402-027 Electric Propulsion Space Experiment Using Soft Actuators and Multiple Sensors A02-096 Resistive Deployment of Inflatable
(ESEX) On-Orbit Results A02-045 Thermally Induced Attitude Distur- Structures Using Velcro
A02-015 Impact Analysis of Hall Thrusters on bance Control for a Spacecraft with a Flexible 402-092 Self-Rigidizable Space Inflatable
Satellite Antenna Performance Boom Boom
A02-120 Realizing “2001: A Space Odyssey”:
Materials Structural Properties
Piloted Spherical Torus Nuclear Fusion Structural Finite Elements
Propulsion A02-114 Electron, Proton, and Ultraviolet Radi- A02-113 Finite Element Modeling of the Axial
ation Effects on Thermophysical Properties of
Spacecraft Radiation Protection Polymeric Films Collapse of Foam-Filled Structures
A02-014 Hazards of Hypervelocity Impacts on A02-113 Finite Element Modeling of the Axial Structural Modeling
Collapse of Foam-Filled Structures
Spacecraft A02-018 New Failure Criterion for Space Shut- A02-023 Fundamental Frequency of Rocket and
Spacecraft Sensor Systems tle Main Engine Turbine Blades Missile Upper Stages: Quick Preliminary Design
A02-092 Self-Rigidizable Space Inflatable Solution
A02-024 Fiber-Optic Sensors for the Study of Boom A02-089 Geometric Imperfection Effects in an
Spacecratt-Thruster Interactions: lon Sputtering A02-115 Time-Dependent Response of Thin Elastically Deployable Isogrid Column
A02-093 Multilayered Polymer Mirror Film Piezoelectric Polymer Polyvinylidene A02-098 Modeling a Piezothermoelastic Beam-
Experiment Fluoride String
J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX
Structural Stability Computational Heat Transfer Thermal Control
A02-088 Design Study of a Square Solar Sail A02-040 Modeling of Chill Down in Cryogenic A02-046 Review of Spacecraft Cryogenic
Architecture Transfer Lines Coolers
402-087 Dimensional Repeatability of an Elas-
Cryogenics
tically Folded Composite Hinge for Deployed Thermal Modeling and Analysis
Spacecraft Optics 402-046 Review of Spacecratt Cryogenic Cool- A02-067 Coupled Aeroheating/Ablation Analy-
A02-089 Geometric Imperfection Effects in an ers
sis for Missile Configurations
Elastically Deployable Isogrid Column Heat Conduction
A02-040 Modeling of Chill Down in Cryogenic
402-068 Thermal Analysis and Design Opti- Transfer Lines
Thermophysics and Heat Transfer
mization of Multilayer Insulation for Reentry
Thermochemistry and Chemical Kinetics
Aerothermodynamics/Thermal Protection Aerodynamic Heating
402-028 Mir Solar-Array Return Experiment:
402-067 Coupled Aeroheating/Ablation Analy- Heat Pipes
Power Performance Measurements and Molecu-
sis for Missile Configurations 402-006 Design Considerations When Using
402-025 Review and Synthesis of Roughness Edge-Mounted Heat Pipes in Space Radiators lar Contamination Analysis Results
Dominated Transition Correlations for Reentry Thermophysical Properties
Radiation in Participating Media
Applications
402-068 Thermal Analysis and Design Opti- 402-068 Thermal Analysis and Design Opti- 402-114 Electron, Proton, and Ultraviolet Radi-
mization of Multilayer Insulation for Reentry mization of Multilayer Insulation for Reentry ation Effects on Thermophysical Properties of
Aerodynamic Heating Aerodynamic Heating Polymeric Films
J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX
Author Index
Adachi, Hirokazu, 402-038 Drager, S. L., A02-063 Karna, Shashi P., 402-065 Meek, Matthew C., A02-117
Agnes, Gregory S., A02-098 Dudzinski, Leonard A., Kasdin, N. Jeremy, A02-047 Meguid, S. A., 402-113
Ahedo, E., 402-030 A02-120 Katz, Ira, 402-122 Mehlem, Klaus, 402-069
Albyn, Keith, 402-028 Dulligan, M. J., 02-027 Kellas. Sotiris, A02-035 Meissinger, Hans F., A02-110
Alexeenko, A. A., A02-026 Eccles, Brian M., A02-024 Kessel, Ramona L., A02-105 Menart, J., A02-049
Arafa, Hani A., 402-076 Ecoffet, Robert, 402-066 Ketsdever, Andrew D., A02-024 Menzies, R. D.D., A02-085
Atanassov, Uta, A02-075 Esposito, Antonio, 402-034 Khanna, Ashish, 402-015 Meyer, J. William, 402-015
Austin, Eric M., 402-042 Estes, S., A02-029 Kim, Chongam, A02-057 Meyer, Thomas R., 402-037
Avery, Keith, A02-064 Evans, Robin W., A02-126 Kim, Jaehoon, 402-107 Mikellides, loannis G., A02-122
Axelrad, Penina, A02-117 Facciano, Andrew B., A02-070 Kim, Sang-Wook, A02-123 Mikhail, Ameer G., A02-082
Badcock, K. J., 402-085 Fang, H., A02-096, A02-092 Kim, Young Ha, A02-118 Mikulas, M. M., A02-088
Bae, Jae-Sung, A02-009 Farrell, W. M., A02-101 Kinard, William, A02-028 Milstein, Frederick, A02-041
Bahei-El-Din, Yehia A., Fasanella, Edwin L., A02-035 Kinoshita, Hiroshi, 402-058 Misuya, Akira, A02-038
A02-076 Ferring, Shea, A02-100 Klevanski, Josef, A02-075 Miyazaki, Yasuyuki, A02-094
Bakis, Charles E., 402-043 Fife, J. M., A02-027 Kluever, Craig A., A02-116 Miyazawa, Yoshikazu, A02-080
Bang, Hyochoong, A02-119 Flotow, Andrew von, A02-031 Knight, Jr., Norman F., 402-035 Mollenhauer, David, A02-093
Banks, Bruce, A02-028 Fogdall, Lawrence B., A02-114 Kobayashi, R. W., A02-013 Monti, Rodolfo, 402-034
Bar-Cohen, Yoseph, A02-112 Fragnito, Marino, 402-020 Kohler, R. L., 402-063 Moon, Bo-Yeon, A02-107
Bennett, Jr., John C., A02-040 Friedman, Assi, A02-100 Koppenwallner, G., 402-061 Moore, F. G., A02-008
Berner, Claude, A02-007 Gallimore, Alec D., A02-123 Korte, J. J., A02-106 Moss, Todd William, 402-006
Bhatia, Ravinder Singh, Garrett, Henry B., A02-126 Kubitschek, Daniel G., A02-117 Motoda, Toshikazu, A02-080
A02-046 Gath, Peter F., 402-069 Kumar, K. D., A02-102, A02-086 Mulder, J. A., A02-083
Blake, William B., 402-079 Ghosh, A. K., 402-062 Kumar, Rajan, A02-056 Murad, Edmond, A02-014
Blandino, Joseph R. , A2-097 Gick, R. Anne, A02-071 Lai, Shu T., A02-014 Murashko, Vyacheslav M.,
Boardsen, Scott A., A02-105 Gimelshein, S. F., 402-026 Lake, Mark S., 402-091 A02-019
Boltz, Frederick W., 402-109, Gold, Kenn L., A02-117 Lamassoure, Elisabeth, Murotsu, Yoshisada, A02-038
A02-111 Graham, Mary Jane, A02-050 A02-073, A02-074 Murray, A. L., A02-067
Bonfiglio, Eugene P., 402-002 Greschik, G., A02-088 Ledsinger, Laura A., A02-055 Myung, Hyun-Sam, Ao1-119
Born, George H., A02-117 Guidos, Bernard J., 402-051 LeDuc, J.R., A02-027 Natori, M. C., A02-094
Borowski, Stanley K., 402-120 Gurfil, Pini, 402-047 Lee, Allan Y., A02-021 Naughton, Jonathan W.,
Bowman, W. Jerry, 402-006 Hallock, Gary A., A02-015 Lee, Byoung-Sun, A02-107 A02-078
Brandeis, Julius, 402-050 Hanada, Toshiya, A02-012 Lee, In, A02-009 Newman, Dava J., A02-036
Brezna, Paul A., A02-064 Hassan, Rania A., A02-076 Lee, Jeong-Sook, A02-107 Ohmae, Nobuo, A02-022,
Brinker, David, A02-028 Hastings, Daniel E., A02-036, Lenz, Christian, 402-100 A02-058
Bromaghim, D.R., 402-027 A02-073, A02-074 Lepsch, Roger A., 402-106 Okutsu, Masataka, A02-004
Campbell, Mark, 402-039, Hathaway, Wayne H., 402-007 Lesieutre, George A., A02-043 Olds, John R., A02-055
A02-031 Hayes, J., A02-049 Levin, D. A., A02-026 Paek, Seung-Kil, 402-009
Camping, John, 402-093 Heald, Johanne C., A02-104 Levine, Marie B., A02-091 Park, Eun-Seo, A02-107
Capitelli, Mario, 402-054 Heaton, Andrew F., 402-002 Lewis, Mark J., A02-125 Park, Jeong-joo, A02-057
Chang, Young-Keun, A02-107 Heavey, Karen R., A02-082 Librescu, Liviu, A02-108 Park, Sang- Young, A02-045
Chapman, Gary T., 402-007 Heister, Stephen D., 402-017 Linderman, M. L., A02-063 Parmenter, Kelly E., A02-041
Cho, Mengu, A02-052, A02-053 Heyerman, J., A02-113 Loane, Joseph T., A02-015 Pastena, Massimiliano, A02-020
Choi, Kyu-Hong, A02-107 Hikita, Masayuki, 402-082, Longo, Savino, A02-054 Paterna, Diego, A02-034
Choi, Seongjin, 402-057 402-053 Longuski, James M., A02-003, Pellegrino, S., A02-095
Choueiri, Edgar Y., A02-047 Hinkle, Jason D., A02-087, A02-002, A02-004, A02-001 Penzo, Paul A., A02-005
Chu, Q. P., A02-083 A02-089 Loéseken, J., A02-085 Peterson, Lee D., A02-104,
Cinnella, Pasquale, A02-048 Hoffman, Klaus A., A02-081 Lou, M., A02-096 A02-087, 402-089, A02-091
Connell, J. W., 402-114 Hsia, Lih-Min, A02-092 Lou, Michael, 402-092 Piertroni, Walter, A02-103
Cooper, Gene R., A02-051 Hughes, Gareth, A02-128 Luglio, Michele, 402-103 Pinney, Mark, 402-079
Costa, R. R., A02-083 Hunter, S. L., 402-029 Luke, Edward A., A02-048 Pittelkau, Mark E., 402-060
Costello, Mark, 402-010 Hyner, T. C., A02-008 Lyke, James C., A02-064, Pochet, Louis M., A02-063
Cross, Matthew F., 402-040 Inman, Daniel J., 402-042 A02-065 Polzin, Kurt A., A02-047
D’Errico, Marco, 402-020 Ito, Shinichi, 402-038 Macdonald, Malcolm, A02-128 Prabhu, A., 402-056
Damevin, Henri-Marie, Jenkin, Alan B.. A02-071 Mailhe, Laurie M., 402-017 Pryor, Wayne R., A02-037
A02-081 Jenkins, C. H., 402-090 Majumdar, Alok K., 402-040 Rademacher, Joel, A02-100
Daryabeigi, Kamran, A02-068 Jitpraphai, Thanat, 402-010 Malla, Ramesh B., A02-040 Raisinghani, S. C., A02-062
Dehury, S. K., 402-062 Johnson, L. K., A02-027 Manzella, David H., A02-122 Raju, K. Kanaka, A02-023
Dharamsi, Urmil K., 402-097 Johnson, W. R., A02-003 Marzocca, Piergiovanni, Ramasamy, Raju, 402-052,
Diaz, David, A02-110 Johnston, J. D., 402-097 A02-108 A02-053
Dickinson, T. J., A02-013 Jones, Yvonne, A02-035 McInnes, Colin R., A02-128 Ramsey, Alvin, A02-007
Dischinger, C., A02-029 Jongeward, Gary A., A02-122 McKay, Christopher P., Rao, G. Venkateswara ,
Domber, Jeanette L., A02-087 Josyula, Eswar, A02-079 A02-037 A02-023
Donahue, B. B., 402-016 Juhasz, Albert J., A02-120 McKenna, Paul M., A02-037 Rasky, Daniel J., A02-041
Donohue, Greg W., A02-065 Kahl, M., A02-085 McNeil, William J., A02-014 Rayman, Marc D., A02-077
J. SPACECRAFT. VOL 39. NO. 6: 2002 INDEX
Reda, Daniel C., A02-025 Scherliess, Ludger, A02-044 Szalai, Christine E., 402-041 Well, Klaus H., 402-069
Reed, Helen, A02-100 Schetter, Thomas, A02-039, Taccogna, Francesco, A02-054 Wertz, Julie A., 402-021
Rezgui, Sana, A02-066 Schilling, J. H.,A02-027 Tagawa, Masahito, A02-022, Westberry-Kutz, Teri L.,
Rho, Oh-Hyun, A02-057 Schmid, Volker, 402-075 402-058
402-070
Riabov, Vladimir V., 402-124 Schonberg, W. P., A02-018 Tahk, M. -J., A02-119
White, D. C., A01-027
Richards, B. E., A02-085 Schumacher, Shane C., 402-115 Tajmar, M., A02-121
Whitmore, Stephen A.,
Rivers, H. Kevin, A02-059 Schunk, Robert W., A02-044 Tanaka, Koji, A02-052, 402-053
Rodriguez, Santiago, A02-066 Schur, W. W., 402-090 Tardy, Jason M., A02-116 402-033, A02-078
Rogers, Jr., James W., 402-098 Scortecci, Fabrizio, A02-019 Tartabini, Paul V., A02-106 Widmer, Dale O., 402-070
Roh, Kyoung-Min, A02-107 Senda, Kei, 402-038 Thayer, Doug, A02-031 Wiley, James C., 402-015
Rossi, A., A02-072 Seybold, Karleen G., 402-070 Thompson, Blair F., A02-117 Williams, Craig H., A02-120
Russel, Dennis A., A02-114 Shang, J. S., A02-049 Tibert, A. G., A02-095 Williams, R. Brett, A02-042
Russel, G. W., 402-067 Shitakubo, Junya, 402-038 Tinker, Michael L., 402-099
Williams, Steven N.. A02-077
Sakamoto, Hiraku, A02-094 Shiue, Fuh-Wen, A02-043 Tong, Xiao-Ling A., A02-048
Winchenbach, Gerald L.,
Salama, Moktar, A02-096 Shuman, Karl, 402-041 Tran, Huy K., 402-041
402-007
Salasovich, R. M., 402-027 Sikora, Joseph G., 402-059 Tribble, A. C., A02-101
Saleh, Joseph H., 402-036, Silva, J. A., 402-083 Underhill, Brian, A02-100 Wu, Junxiao, A02-048
402-073, A02-074 Silva, Walter A.. 402-108 Vagners, Juris, A02-031 Wu, S. F., A02-083
Sankaran, Sankara N., A02-059 Sippel, Martin, A02-075 Velazco, Raoul, A02-066 Wurster, Kathryn E., 402-106
Sanmartin, J. R., A02-030 Smalley, Kurt B., 402-099 Verma, S. B., A02-061 Yasaka, T., A02-012,
Santos, Wilson F.N., A02-125 Sojka, Jan J.. A02-044 Vinogradov, Aleksandra M.., 402-102
Sarper, Hiiseyin, 402-084 Spanjers, G. G., A02-027 02-115 Yokota, Kumiko, A02-022,
Sasaki, Susumu, A02-052, Spencer, David B., A02-118 Vinogradov, Vladimir N.,
402-053 Spencer, Edmund A., 402-015 402-019 402-058
Yoon, Jae-Cheol, A02-107
Sauer, Wolfgang J., 402-084 Steinberg, J. T., A02-101 Visentine, James, A02-028
Savino, Raffaele, A02-034 Stranart, J. C.. A02-113 Viswanath, P. R., A02-056 Younan, Maher Y. A.. 402-076
Sayyah, M. Tarek, A02-018 Strange, Nathan J., 402-002, Warren, Peter, 402-087, A02-089 Yu, Shaohua, A02-032
Schall, Wolfgang O., A02-011 402-001 Weinacht, Paul, 402-050 Zaldivar, R. J.. A02-013
J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX
Chronological Index
A02-001 Graphical Method for Gravity-Assist Trajectory A02-014 Hazards of Hypervelocity Impacts on Spacecraft. Shu
Design. Nathan J. Strange and James M. Longuski, Purdue T. Lai and Edmond Murad, U.S. Air Force Research Laboratory;
University (39, 1, p. 9) Article and William J. McNeil, Radex, Inc., (39, 1, p. 106) Article
A02-002 Automated Design of the Europa Orbiter Tour. A02-015 Impact Analysis of Hall Thrusters on Satellite
Andrew F. Heaton, Nathan J. Strange, and James M. Longuski, Antenna Performance. Gary A. Hallock, James C. Wiley, Ashish
Purdue University; and Eugene P. Bonfiglio, Jet Propulsion Khanna, and Edmund A. Spencer, The University of Texas at
Laboratory (39, 1, p. 17) Article Austin, and J. William Meyer and Joseph T. Loane, Lockheed
Martin Space Systems Company (39, 1, p. 115) Article based on
A02-003 Design of Aerogravity-Assist Trajectories. W. R. AIAA Paper 2000-3519
Johnson and James M. Longuski, Purdue University (39, 1, p. 23)
Article A02-016 Two-Stage Launch Vehicles for Heavy Payloads. B. B.
Donahue, The Boeing Company (39, 1, p. 125) Article
A02-004 Mars Free Returns via Gravity Assist From Venus.
Masataka Okutsu and James M. Longuski, Purdue University A02-017 Design of a Hybrid Chemical/Electric Propulsion
(39, 1, p. 31) Article Orbital Transfer Vehicle. Laurie M. Mailhe and Stephen D.
Heister, Purdue University (39, 1, p. 131) Article
A02-005 To the Far Side of the Sun Using Venus Gravity Assist.
Paul A. Penzo, Jet Propulsion Laboratory (39, 1, p. 37) Article A02-018 New Failure Criterion for Space Shuttle Main Engine
based on AIAA Paper AIAA-2000-4140 Turbine Blades. M. Tarek Sayyah, Sverdrup Technology, Inc.; and
W. P. Schonberg, University of Missouri-Rolla (39, 1, p. 140)
A02-006 Design Considerations When Using Edge-Mounted Article
Heat Pipes in Space Radiators. Todd William Moss and W. Jerry
Bowman, Brigham Young University (39, 1, p. 41) Article A02-019 Cost-Optimum Electric Propulsion for Constellations.
Vladimir N. Vinogradov and Vyacheslav M. Murashko,
A02-007 Dynamic Stability of Blunt Atmospheric Entry Experimental Design Bureau “Fakel”, Russia; and Fabrizio
Configurations. Gerald L. Winchenbach and Gary T. Chapman, Scortecci, Aerospazio Tecnologie s.r.l., Italy (39, 1, p. 146)
University of Florida; Wayne H. Hathaway, Arrow Tech Associates; Engineering Note
Alvin Ramsey, University of California at Berkeley: and Claude
Berner, French German Research Institute, France (39, 1, p. 49) A02-020 Spacecraft Thermal Analysis and Control by Thermal
Article Energy Optimum Distribution. Marino Fragnito, Goupe d’ Etudes
et de Conseils en Ingenierie, France; and Massimiliano Pastena and
A02-008 Improved Semi-Empirical Method for Power-On Marco D’Errico, Second University of Naples, Italy (39, 1, p. 149)
Base-Drag Prediction. F. G. Moore, Aeroprediction Inc.; and T. C. Engineering Note
Hyner, U. S. Naval Surface Warfare Center (39, 1, p. 56) Article
based on AIAA Paper 2001-4328 A02-021 In-Flight Estimation of the Cassini Spacecraft’s
Inertia Tensor. Allan Y. Lee, Jet Propulsion Laboratory,
A02-009 Flutter Anzlysis of a Wraparound Fin Projectile California Institute of Technology; and Julie A. Wertz,
Considering Rolling Motion. Seung-Kil Paek, Jae-Sung Bae, and Massachusetts Institute of Technology (39, 1, p. 153)
In Lee, Korea Advanced Institute of Science and Technology, Engineering Note
Republic of Korea (39, 1, p. 66) Article
A02-022 Impingement Angle Dependence of Erosion Rate of
A02-010 Determining Angular Velocity and Angular Polyimide in Atomic Oxygen Exposures. Kumiko Yokota,
Acceleration of Projectiles Using Triaxial Acceleration Masahito Tagawa, and Nobuo Ohmae, Kobe University, Japan
Measurements. Mark Costello and Thanat Jitpraphai, Oregon (39, 1, p. 155) Engineering Note
State University (39, 1, p. 73) Article
A02-023 Fundamental Frequency of Rocket and Missile Upper
A02-011 Laser Radiation for Cleaning Lower Earth Orbits. Stages: Quick Preliminary Design Solution. G. Venkateswara
Wolfgang O. Schall, DLR, German Aerospace Center, Germany Rao and K. Kanaka Raju, Vikram Sarabhai Space Centre, India
(39, 1, p. 81) Article (39, 1, p. 157) Engineering Note
A02-012 Orbital Debris Environment Model in_ the A02-024 Fiber-Optic Sensors for the Study of Spacecraft-
Geosynchronous Region. Toshiya Hanada and Tetsuo Yasaka, Thruster Interactions: Ion Sputtering. Andrew D. Ketsdever,
Kyushu University, Japan (39, 1, p. 92) Article U.S. Air Force Research Laboratory; and Brian M. Eccles,
University of Southern California (39, 1, p. 158) Engineering Note
A02-013 Exposure of Polycyanurate and Epoxy Matrix based on AJAA Paper 2001-2958
Composites to Hypergolic Rocket Fuel Components. R. J.
Zaldivar, The Aerospace Corporation; R. W. Kobayashi, The A02-025 Review and Synthesis of Roughness-Dominated
Areospace Corporation; and T. J. Dickinson, U.S. Air Force Space Transition Correlations for Reentry Applications. Daniel C.
and Missiles Command (39, 1, p. 99) Article Reda, NASA Ames Research Center (39, 2, p. 161) Survey
J. SPACECRAFT, VOL. 39, NO. 6: 2002 INDEX 944
A02-026 Modeling of the Interaction of a Side Jet with a A02-038 Hardware Experiments of a Truss Assembly by an
Rarefied Atmosphere. S. F. Gimelshein, George Washington Autonomous Space Learning Robot. Kei Senda, Yoshisada
University; A. A. Alexeenko, Pennsylvania State University; and Murotsu, Akira Misuya, Hirokazu Adachi, Shin’ichi Ito, Junya
D. A. Levin, Pennsylvania State University (39, 2, p. 168) Article Shitakubo, and Tsutomu Matsumoto, Osaka Prefecture University,
Japan (39, 2, p. 267) Article based on AIAA Paper 2000-4377
A02-027 Electric Propulsion Space Experiment (ESEX)
On-Orbit Results. D.R. Bromaghim, J.R. LeDuc, R. M. A02-039 Comparison of Multiple Agent-Based Organizations
Salasovich, G. G. Spanjers, J. M. Fife, and M. J. Dulligan, J. H. for Satellite Constellations. Mark Campbell and Thomas Schetter,
University of Washington (39, 2, p. 274) Article
Schilling, and D. C. White, U.S. Air Force Research Laboratory;
and L. K. Johnson, The Aerospace Corporation (39, 2, p. 177)
A02-040 Modeling of Chill Down in Cryogenic Transfer Lines.
Article
Matthew F. Cross, University of Connecticut; Alok K. Majumdar,
Marshall Space Flight Center; and John C. Bennett, Jr., and
A02-028 Mir Solar-Array Return Experiment: Power
Ramesh B. Malla, University of Connecticut (39, 2, p. 284) Article
Performance Measurements and Molecular Contamination
Analysis Results. James Visentine, Boeing Space Station Program
A02-041 Compressive Response of Lightweight Ceramic
Office: William Kinard, NASA Langley Research Center, David
Ablators: Silicone Impregnated Reusable Ceramic Ablator.
Brinker and Bruce Banks, NASA John H. Glenn Research Center at
Kelly E. Parmenter, Karl Shuman, and Frederick Milstein,
Lewis Field; and Keith Albyn, NASA Marshall Space Flight Center
University of California, Santa Barbara; and Christine E. Szalai,
(39, 2, p. 187) Article based on AIAA Paper 2001-0684
Huy K. Tran, and Daniel J. Rasky, NASA Ames Research Center
(39, 2, p. 290) Article
A02-029 Three-Dimensional Simulation: Microgravity
Environments and Applications. S. L. Hunter, C. Dischinger, and
A02-042 Local Effects of Piezopolymer Patches on Inflatable
S. Estes, NASA Marshall Space Flight Center (39, 2, p. 194) Article Space-Based Structures. R. Brett Williams, Virginia Polytechnic
Institute and State University; Eric M. Austin, Clemson University;
A02-030 Analysis of Bare-Tether Systems for Deorbiting Low- and Daniel J. Inman, Virginia Polytechnic Institute and State
Earth-Orbit Satellites. E. Ahedo and J. R. Sanmartin, Universidad University (39, 2, p. 299) Article
Politécnica De Madrid, Spain (39, 2, p. 198) Article
A02-043 Condition Monitoring of Filament-Wound Composite
A02-031 Six-Axis Vibration Isolation System Using Soft Flywheels Having Circumferential Cracks. Fuh-Wen Shiue,
Actuators and Multiple Sensors. Doug Thayer, Mark Campbell, George A. Lesieutre, and Charles E. Bakis, Pennsylvania State
and Juris Vagners, University of Washington, Andrew von Flotow, University (39, 2, p. 306) Article based on AIAA Paper 2001-1441
Hood Technology Corporation (39, 2, p. 206) Article
A02-044 Ionospheric Specification and Forecast Modeling.
A02-032 Dynamic Model and Control of Mass-Distributed Robert W. Schunk, Ludger Scherliess, and Jan J. Sojka, Utah State
Tether Satellite System. Shaohua Yu, Academia Sinica, People’s University (39, 2, p. 314) Article
Republic of China (39, 2, p. 213) Article
A02-045 Thermally Induced Attitude Disturbance Control for
A02-033 Frequency Response of Pneumatic Tubing and a Spacecraft with a Flexible Boom. Sang-Young Park, Naval
Pressure Sensor Configurations in Slip-Flow Conditions. Postgraduate School (39, 2, p. 325) Engineering Note
Stephen A. Whitmore, Naval Postgraduate School (39, 2, p. 219)
A02-046 Review of Spacecraft Cryogenic Coolers. Ravinder
Article
Singh Bhatia, California Institute of Technology (39, 3, p. 329)
Survey
A02-034 Experimental and Numerical Investigation on
Martian Atmosphere Entry. Diego Paterna, Rodolfo Monti,
A02-047 Plasma Propulsion Options for Multiple Terrestrial
Raffaele Savino, and Antonio Esposito, Universita di Napoles
Planet Finder Architectures. Kurt A. Polzin, Edgar Y. Choueiri,
“Federico Il", Italy (39, 2, p. 227) Article based on AIAA
Pini Gurfil, and N. Jeremy Kasdin, Princeton University
Paper 2001-0751
(39, 3, p. 347) Article
A02-035 Earth Impact Studies for Mars Sample Return. Edwin
A02-048 Comprehensive Numerical Study of Jet-Flow
L. Fasanella and Yvonne Jones, NASA Langley Research Center;
Impingement over Flat Plates . Junxiao Wu, Edward A. Luke,
Norman F. Knight and Sotiris Kellas, Veridian Systems (39, 2, p.
Xiao-Ling A. Tong, and Pasquale Cinnella, Mississippi State
237) Article
University (39, 3, p. 357) Article
A02-036 Spacecraft Design Lifetime. Joseph H. Saleh, Daniel E.
A02-049 Hypersonic Flow over a Blunt Body with Plasma
Hastings, and Dava J. Newman, Massachusetts Institute of Injection. J. S. Shang and J. Hayes, U.S. Air Force Research
Technology (39, 2, p. 244) Article Laboratory; and J. Menart, Wright State University (39, 3, p. 367)
Article
A02-037 Laser Elevator: Momentum Transfer Using an
Optical Resonator. Thomas R. Meyer, Boulder Center for Science A02-050 Numerical Investigation of Supersonic Jet Interaction
and Policy; Wayne R. Pryor, University of Colorado; Christopher P. for Finned Bodies. Mary Jane Graham, U.S. Military Academy,
McKay, NASA Ames Research Center; and Paul M. McKenna, West Point, Paul Weinacht, U.S. Army Research Laboratory; and
National Telecommunications and Information Administration Julius Brandeis, RAFAEL, Ministry of Defense (39, 3, p. 376)
(39, 2, p. 258) Article Article