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NASA Scientific and Technical Aerospace Reports

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Modeling of the Plasma Thruster Impact<br />

on Spacecraft Charging – 37<br />

NASCAP-2K: An Overview – 30<br />

NASCAP-2K as a PIC Code – 37<br />

New <strong>NASA</strong> SEE LEO Spacecraft Charging<br />

Design Guidelines: How to Survive in<br />

LEO Rather than GEO – 32<br />

Observations of Vehicle Surface Charging<br />

in Dusty Plasma – 36<br />

On-Orbit Experiments <strong>and</strong> Research on<br />

Measuring the Spacecraft Charging<br />

– 327<br />

Onset of Spacecraft Charging in Single<br />

<strong>and</strong> Double Maxwellian Plasmas in<br />

Space: A Pedagogical Review – 316<br />

Operational Prediction <strong>and</strong> Specification<br />

of the Spacecraft Charging Environment<br />

– 328<br />

Representation of the Geosynchronous<br />

Plasma Environment for Spacecraft<br />

Charging Calculations – 38<br />

Secondary Electron Emission Causing<br />

Potential Barriers Around Negatively<br />

Charged Spacecraft – 37<br />

Space Environments <strong>and</strong> Effects (SEE)<br />

Program: Spacecraft Charging Technology<br />

Development Activities – 31<br />

Spacecraft Charging in a Quasi-Static<br />

<strong>and</strong> Dynamic Plasma Environment <strong>and</strong><br />

the Scaling Laws for ESD-Induced Current<br />

Transients – 31<br />

SPARCS: An Advanced Software for<br />

Spacecraft Charging Analyses – 259<br />

Specification of ISS Plasma Environment<br />

Variability – 296<br />

The Flumic Electron Environment<br />

Model – 327<br />

Validation of NASCAP-2K Spacecraft-<br />

Environment Interactions Calculations<br />

– 239<br />

Wake Effects on Positively Charged<br />

Spacecraft in Flowing Tenuous Plasmas:<br />

Cluster Observations <strong>and</strong> Modeling<br />

– 39<br />

SPACECRAFT COMPONENTS<br />

On-Orbit Daytime Solar Heating Effects:<br />

A Comparison of Ground Chamber Arcing<br />

Results – 38<br />

SPACECRAFT CONFIGURATIONS<br />

A Flight Control Approach for Small Reentry<br />

Vehicles – 41<br />

Plasma Phenomena Associated With Solar<br />

Array Discharges <strong>and</strong> Their Role in<br />

Scaling Coupon Test Results to a Full<br />

Panel – 30<br />

SPACECRAFT CONSTRUCTION MATERI-<br />

ALS<br />

Materials Characterization at Utah State<br />

University: Facilities <strong>and</strong> Knowledgebase<br />

of Electronic Properties of Materials<br />

Applicable to Spacecraft Charging – 33<br />

A-64<br />

SPACECRAFT CONTROL<br />

Active Spacecraft Potential Control for<br />

Cluster Results from Three Years in Orbit<br />

– 42<br />

SPACECRAFT DESIGN<br />

Electron Emission Properties of Insulator<br />

Materials Pertinent to the International<br />

Space Station – 35<br />

Leo Spacecraft Charging Design Guidelines:<br />

A Proposed <strong>NASA</strong> St<strong>and</strong>ard – 41<br />

New <strong>NASA</strong> SEE LEO Spacecraft Charging<br />

Design Guidelines: How to Survive in<br />

LEO Rather than GEO – 32<br />

Secondary Electron Emission Causing<br />

Potential Barriers Around Negatively<br />

Charged Spacecraft – 37<br />

Space Weather Effects on SOHO <strong>and</strong> its<br />

Role as a Space Weather Watchdog<br />

– 44<br />

Structural Design for a Neptune Aerocapture<br />

Mission – 40<br />

SPACECRAFT ELECTRONIC EQUIP-<br />

MENT<br />

Cylindrical Asymmetrical Capacitor Devices<br />

for Space Applications – 105<br />

SPACECRAFT ENVIRONMENTS<br />

A Review of Spacecraft Effects on<br />

Plasma Measurements – 33<br />

Ground Experiment <strong>and</strong> Numerical<br />

Simulation of Spacecraft Arcing in Ambient<br />

Plasma Environments – 262<br />

In-Flight Anomalies Attributed to ESD’s.<br />

Recent Cases <strong>and</strong> Trends – 44<br />

SPACECRAFT INSTRUMENTS<br />

A Novel Spacecraft Charge Monitor for<br />

LEO – 33<br />

Active Spacecraft Potential Control for<br />

Cluster Results from Three Years in Orbit<br />

– 42<br />

In-Flight Anomalies Attributed to ESD’s.<br />

Recent Cases <strong>and</strong> Trends – 44<br />

In-Flight Thermal Performance of the Lidar<br />

In-Space Technology Experiment<br />

– 44<br />

Space Weather Effects on SOHO <strong>and</strong> its<br />

Role as a Space Weather Watchdog<br />

– 44<br />

SPACECRAFT MAINTENANCE<br />

Intelligent Work Process Engineering<br />

System – 271<br />

SPACECRAFT MODELS<br />

Features of Charging of Composite Configuration<br />

Spacecraft Charging in High<br />

Orbits – 39<br />

Parameter Estimation of Spacecraft Nutation<br />

Growth Model – 120<br />

Shuttle Systems 3-D Applications: Application<br />

of 3-D Graphics in Engineering<br />

Training for Shuttle Ground Processing<br />

– 27<br />

The Electric Propulsion Interactions<br />

Code (EPIC) – 238<br />

SPACECRAFT MODULES<br />

Feasibility Study of an Experimental Platform<br />

With Active Plasma Emission for<br />

Japan Experimental Module Onboard<br />

ISS – 34<br />

SPACECRAFT PERFORMANCE<br />

Aerocapture Performance Analysis for a<br />

Neptune-Triton Exploration Mission<br />

– 320<br />

SPACECRAFT POWER SUPPLIES<br />

Advanced Technology Development for<br />

Stirling Convertors – 46<br />

Performance Expectations of Closed-<br />

Brayton-Cycle Heat Exchangers in 100kWe<br />

Nuclear Space Power Systems<br />

– 47<br />

Power Management <strong>and</strong> Distribution<br />

Trades Studies for a Deep-Space Mission<br />

<strong>Scientific</strong> Spacecraft – 47<br />

System Mass Variation <strong>and</strong> Entropy<br />

Generation in 100-kWe Closed-Brayton-<br />

Cycle Space Power Systems – 47<br />

SPACECRAFT PROPULSION<br />

Experimental Investigation from the Operation<br />

of a 2 kW Brayton Power Conversion<br />

Unit <strong>and</strong> a Xenon Ion Thruster – 46<br />

Modeling of the Plasma Environment of a<br />

FEEP Micro Thruster with PicUp3D<br />

Simulation Code: Sample Results – 45<br />

SPACECRAFT SHIELDING<br />

Evaluation of Space Station<br />

Meteoroid/Debris Shielding Materials,<br />

Supplement – 40<br />

SPACECRAFT STRUCTURES<br />

Degradation of Spacecraft Materials<br />

– 41<br />

SPACECRAFT SURVIVABILITY<br />

Space Environmental Effects <strong>and</strong> Spacecraft<br />

EMC – 42<br />

SPACECRAFT TRACKING<br />

Analysis of Return <strong>and</strong> Forward Links<br />

from STARS’ Flight Demonstration<br />

1 – 42<br />

SPACECRAFT<br />

Meteor Outbursts <strong>and</strong> Storms from the<br />

Spacecraft Hazard Perspective – 28<br />

SPACE-TIME CE/SE METHOD<br />

Computation of Tone Noises Generated<br />

in Viscous Flows – 290<br />

SPATIAL DISTRIBUTION<br />

A Comparison between Growth Morphology<br />

of ‘Eutectic’ Cells/Dendrites <strong>and</strong><br />

Single-Phase Cells/Dendrites – 77<br />

RGS Spectroscopy of the Cygnus Loop<br />

XA Knot – 317<br />

SPECTRAL EMISSION<br />

Seasonal Surface Spectral Emissivity<br />

Derived from Terra MODIS Data – 157<br />

SPECTRA<br />

Asymptotic Technique for the Far Field<br />

Pattern of a Dipole in an Infinite Stratified<br />

Medium – 93

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