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DATA TRANSMISSION<br />

Reliable Transport over SpaceWire for<br />

James Webb Space Telescope (JWST)<br />

Focal Plane Electronics (FPE) Network<br />

– 14<br />

DEBONDING (MATERIALS)<br />

Effect of a BN Interphase that Debonds<br />

Between the Interphase and the Matrix In<br />

SiC/SiC Composites – 35<br />

DECISION MAKING<br />

A Product Development Decision Model<br />

for Cockpit Weather Information Systems<br />

– 72<br />

The Use of the Janus Wargame Simulation<br />

to Investigate Naturalistic Decision-<br />

Making: A Preliminary Examination – 95<br />

Visualizing Decision-making Behaviours<br />

in Agent-based Autonomous Spacecraft<br />

– 8<br />

DECISION SUPPORT SYSTEMS<br />

A Virtual Mission Operations Center -<br />

Collaborative Environment – 11<br />

DEFECTS<br />

Flaw Tolerance in Lap Shear Brazed<br />

Joints – 54<br />

DEGREES OF FREEDOM<br />

A Nonlinear, Six-Degree of Freedom Precision<br />

Formation Control Algorithm,<br />

Based on Restricted Three Body Dynamics<br />

– 8<br />

DELTA LAUNCH VEHICLE<br />

Orbit Determination Support for the Microwave<br />

Anisotropy Probe (MAP) – 20<br />

DELTA WINGS<br />

Transonic Reynolds Number and<br />

Leading-Edge Bluntness Effects on a 65<br />

deg Delta Wing – 2<br />

DENSITY MEASUREMENT<br />

The Intercluster Medium in Clusters<br />

– 117<br />

DEPOLARIZATION<br />

Three-Signal Method for Accurate Measurements<br />

of Depolarization Ratio with<br />

Lidar – 88<br />

DEPOSITION<br />

Material Outgassing, Identification and<br />

Deposition, MOLIDEP System – 52<br />

DESIGN ANALYSIS<br />

Advanced Control Surface Seal Development<br />

at NASA GRC for 3rd Generation<br />

RLV – 56<br />

Design and Analysis of the ST7 Disturbance<br />

Reduction System (DRS) Spacecraft<br />

Controller – 20<br />

Hubble Space Telescope On-orbit NiH2<br />

Battery Performance – 25<br />

LEO Spacecraft Charging Guidelines<br />

– 17<br />

Optical Testing of Diamond Machined,<br />

Aspheric Mirrors for Groundbased,<br />

Near-IR Astronomy – 53<br />

The Design of a Remotely Operated<br />

Shutter (ROS) for Thermal Vacuum Testing<br />

– 55<br />

A-10<br />

DESIGN OPTIMIZATION<br />

Collectives for the Optimal Combination<br />

of Imperfect Objects – 105<br />

Sperm Whale Impulse Noise and Incoherent<br />

Narrowband CFAR Processing<br />

– 107<br />

DESIGN<br />

A NASA Perspective and Validation and<br />

Testing of Design Hardening for the<br />

Natural Space Radiation Environment<br />

(GOMAC Tech 03) – 56<br />

DESTRUCTIVE TESTS<br />

Current Single Event Effects and Radiation<br />

Damage Results for Candidate<br />

Spacecraft Electronics – 27<br />

Status on Mechanical Testing at NASA<br />

GSFC – 54<br />

DETECTORS<br />

Comparison of the Gamma-Ray Burst<br />

Sensitivity of Different Detectors – 123<br />

Effect of Clouds on Apertures of Spacebased<br />

Air Fluorescence Detectors<br />

– 126<br />

DIAGNOSIS<br />

The Filtered Abel Transform and Its Application<br />

in Combustion Diagnostics<br />

– 31<br />

DIELECTRICS<br />

Switching Oxide Traps – 47<br />

DIFFUSION FLAMES<br />

The Filtered Abel Transform and Its Application<br />

in Combustion Diagnostics<br />

– 31<br />

DIRECT NUMERICAL SIMULATION<br />

Source Term Model for an Array of Vortex<br />

Generator Vanes – 50<br />

DIRECTIONAL SOLIDIFICATION (CRYS-<br />

TALS)<br />

Directional Solidification and Convection<br />

in Small Diameter Crucibles – 41<br />

DISPLAY DEVICES<br />

Human Centered Design and Development<br />

for NASA’s MerBoard – 100<br />

Low Frequency High Amplitude Temperature<br />

Oscillations in Loop Heat Pipe<br />

Operation – 49<br />

DISTRIBUTED MEMORY<br />

Scalability of a Low-Cost Multi-Teraflop<br />

Linux Cluster for High-End Classical Atomistic<br />

and Quantum Mechanical Simulations<br />

– 98<br />

DISTRIBUTED PROCESSING<br />

Applicability of Markets to Global Scheduling<br />

in Grids: Critical Examination of<br />

General Equilibrium Theory and Market<br />

Folklore – 114<br />

Collectives for Multiple Resource Job<br />

Scheduling Across Heterogeneous Servers<br />

– 99<br />

DISTRIBUTION FUNCTIONS<br />

The Impact of Aerosols on Cloud and<br />

Precipitation Processes: Cloud-<br />

Resolving Model Simulations – 73<br />

DOCUMENT MARKUP LANGUAGES<br />

Distributed Framework for Dynamic Telescope<br />

and Instrument Control – 52<br />

DOCUMENTS<br />

HEASARC Software Archive – 98<br />

DOMAINS<br />

Foundations of the Bandera Abstraction<br />

Tools – 100<br />

DROPS (LIQUIDS)<br />

The Fluids And Combustion Facility<br />

Combustion Integrated Rack And The<br />

Multi-User Droplet Combustion Apparatus:<br />

Microgravity Combustion Science<br />

Using Modular Multi-User Hardware<br />

– 44<br />

DROUGHT<br />

Causes of Long-Term Drought in the<br />

USA Great Plains – 86<br />

DRYING<br />

Lidar Measurements of Wind, Moisture,<br />

and Boundary Layer Evolution in a Dry<br />

Line during 1HOP 2002 – 77<br />

DUCTS<br />

Sound Propagation from a Supersonic<br />

Jet Flowing through a Rigid-walled Duct<br />

with a J-Deflector – 7<br />

DUST<br />

Characterization of Dust Properties during<br />

ACE-Asia and PRIDE: A Column<br />

Satellite-Surface Perspective – 81<br />

Effects of Non-Sphericity on Mineral Dust<br />

Modeling – 71<br />

Evaluation of the MODIS Retrievals of<br />

Dust Aerosol over the Ocean during<br />

PRIDE – 70<br />

Long-Term Simulation of Dust Distribution<br />

with the GOCART Model: Correlation<br />

with the North Atlantic Oscillation<br />

– 74<br />

DYNAMIC CONTROL<br />

Benchmark Problems for Space Mission<br />

Formation Flying – 54<br />

Coupled Attitude and Orbit Dynamics<br />

and Control in Formation Flying Systems<br />

– 11<br />

Development of a Thrust Stand to Meet<br />

LISA Mission Requirements – 29<br />

Membrane Vibration Tests Using<br />

Surface-Bonded Piezoelectric Patch Actuation<br />

– 45<br />

DYNAMIC MODELS<br />

Coupled Attitude and Orbit Dynamics<br />

and Control in Formation Flying Systems<br />

– 11<br />

DYNAMIC PRESSURE<br />

Static Aeroelastic Predictions for a Transonic<br />

Transport Model Using an<br />

Unstructured-Grid Flow Solver Coupled<br />

With a Structural Plate Technique – 3<br />

DYNAMIC RESPONSE<br />

A Time Integration Algorithm Based on<br />

the State Transition Matrix for Structures<br />

with Time Varying and Nonlinear Properties<br />

– 104

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