11.12.2012 Views

NASA Scientific and Technical Aerospace Reports

NASA Scientific and Technical Aerospace Reports

NASA Scientific and Technical Aerospace Reports

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Prediction <strong>and</strong> Measurement of the Vibration<br />

<strong>and</strong> Acoustic Radiation of Panels<br />

Subjected to Acoustic Loading – 288<br />

SOUNDING ROCKETS<br />

Observations of Vehicle Surface Charging<br />

in Dusty Plasma – 36<br />

SOYBEANS<br />

Is Peripheral Benzodiazepine Receptor<br />

(PBR) Gene Expression Involved in<br />

Breast Cancer Suppression by Dietary<br />

Soybean Protein – 222<br />

SPACE CHARGE<br />

Modeling of the Photoelectron Sheath<br />

Around an Active Magnetospheric<br />

Spacecraft With PicUp3D – 317<br />

SPACE DEBRIS<br />

Evaluation of Space Station<br />

Meteoroid/Debris<br />

Supplement – 40<br />

Shielding Materials,<br />

Using Lasers in Space: Laser Orbital<br />

Debris Removal <strong>and</strong> Asteroid Deflection<br />

– 26<br />

SPACE ENVIRONMENT SIMULATION<br />

NASCAP-2K: An Overview – 30<br />

SPACE EXPLORATION<br />

Aerocapture Performance Analysis for a<br />

Neptune-Triton Exploration Mission<br />

– 320<br />

SPACE MISSIONS<br />

A ‘Free Lunch’ Tour of the Jovian System<br />

– 320<br />

Aerocapture Performance Analysis for a<br />

Neptune-Triton Exploration Mission<br />

– 320<br />

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

In-Space Technology Experiment<br />

– 44<br />

Mixed-Initiative Planning <strong>and</strong> Scheduling<br />

for Science Missions – 304<br />

OAST Technology for the Future. Executive<br />

Summary – 22<br />

OAST Technology for the Future. Volume<br />

2 - Critical Technologies, Themes<br />

1-4 – 22<br />

OAST Technology for the Future. Volume<br />

3 - Critical Technologies, Themes<br />

5-8 – 21<br />

Reusable Launch Vehicles <strong>and</strong> Space<br />

Operations – 26<br />

Structural Design for a Neptune Aerocapture<br />

Mission – 40<br />

STS-107 Mission after the Mission: Recovery<br />

of Data from the Debris of Columbia<br />

– 28<br />

SPACE PLASMAS<br />

Current Collection by a Segmented<br />

Langmuir Probe in the Ionosphere<br />

Plasma – 43<br />

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

Simulation of Spacecraft Arcing in Ambient<br />

Plasma Environments – 262<br />

Modeling of the Plasma Environment of a<br />

FEEP Micro Thruster with PicUp3D<br />

Simulation Code: Sample Results – 45<br />

Plasma Interactions With a Negative Biased<br />

Electrodynamic Tether – 324<br />

Representation of the Geosynchronous<br />

Plasma Environment for Spacecraft<br />

Charging Calculations – 38<br />

Simulations of Solar Wind Plasma Flow<br />

Around a Simple Solar Sail – 325<br />

The Deflection Plate Analyzer: A Technique<br />

for Space Plasma Measurements<br />

Under Highly Disturbed Conditions – 43<br />

SPACE PLATFORMS<br />

High Voltage Solar Array for 400V Operation<br />

in LEO Plasma Environment – 37<br />

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

In-Space Technology Experiment<br />

– 44<br />

SPACE SHUTTLE BOOSTERS<br />

Identifying, Assessing, <strong>and</strong> Mitigating<br />

Risk of Single-Point Inspections on the<br />

Space Shuttle Reusable Solid Rocket<br />

Motor – 133<br />

SPACE SHUTTLES<br />

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

of 3-D Graphics in Engineering<br />

Training for Shuttle Ground Processing<br />

– 27<br />

STS-107 Mission after the Mission: Recovery<br />

of Data from the Debris of Columbia<br />

– 28<br />

SPACE STATION FREEDOM<br />

Electron Collection by International<br />

Space Station Solar Arrays – 325<br />

SPACE TECHNOLOGY EXPERIMENTS<br />

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

In-Space Technology Experiment<br />

– 44<br />

SPACE TRANSPORTATION SYSTEM<br />

STS-107 Mission after the Mission: Recovery<br />

of Data from the Debris of Columbia<br />

– 28<br />

SPACE TRANSPORTATION<br />

Reusable Launch Vehicles <strong>and</strong> Space<br />

Operations – 26<br />

SPACE WEATHER<br />

AF-Geospace 2.0 – 238<br />

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

Role as a Space Weather Watchdog<br />

– 44<br />

SPACEBORNE ASTRONOMY<br />

Five Years of Operation of the Ch<strong>and</strong>ra<br />

X-Ray Observatory – 319<br />

SPACEBORNE EXPERIMENTS<br />

An Overview of the NIRA 2003 Vibratory<br />

Analysis – 89<br />

Mission Success for Combustion Science<br />

– 89<br />

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

Measuring the Spacecraft Charging<br />

– 327<br />

Structure of Flame Balls at Low Lewis-<br />

Number (SOFBALL): New Results from<br />

STS-107 – 69<br />

SPACECRAFT ANTENNAS<br />

NASCAP-2K as a PIC Code – 37<br />

SPACECRAFT CHARGING<br />

8th Spacecraft Charging Technology<br />

Conference – 29<br />

A Novel Spacecraft Charge Monitor for<br />

LEO – 33<br />

An Educational Multimedia Presentation<br />

on the Introduction to Spacecraft Charging<br />

– 31<br />

Assessment <strong>and</strong> Control of Spacecraft<br />

Charging Risks on the International<br />

Space Station – 35<br />

Calibrating the Floating Potential Measurement<br />

Unit – 43<br />

Charge Storage, Conductivity <strong>and</strong><br />

Charge Profiles of Insulators as Related<br />

to Spacecraft Charging – 315<br />

Clear, Conductive, Transparent, Flexible<br />

Space Durable Composite Films for<br />

Electrostatic Charge Mitigation – 52<br />

Comparison of Classical <strong>and</strong> Charge<br />

Storage Methods for Determining Conductivity<br />

of Thin Film Insulators – 25<br />

ECSS-E-20-06 Draft St<strong>and</strong>ard on Spacecraft<br />

Charging: Environment-Induced Effects<br />

on the Electrostatic Behaviour of<br />

Space Systems – 316<br />

Effects of Large-Amplitude RF Emissions<br />

on OEDIPUS-C Floating Voltages – 32<br />

European Approach to Material Characterization<br />

for Plasma Interaction Analysis<br />

– 296<br />

Feasibility Study of an Experimental Platform<br />

With Active Plasma Emission for<br />

Japan Experimental Module Onboard<br />

ISS – 34<br />

Features of Charging of Composite Configuration<br />

Spacecraft Charging in High<br />

Orbits – 39<br />

High Voltage Solar Array Arc Testing for a<br />

Direct Drive Hall Effect Thruster System<br />

– 30<br />

High-Level Spacecraft Charging at Geosynchronous<br />

Altitudes: A Statistical<br />

Study – 36<br />

Improved Demonstration of Internal<br />

Charging Hazards Using the Realistic<br />

Electron Environment Facility<br />

(REEF) – 31<br />

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

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

Investigation of Electrostatic Potential<br />

Barrier Near an Electron-Emitting<br />

Body – 32<br />

Leo Spacecraft Charging Design Guidelines:<br />

A Proposed <strong>NASA</strong> St<strong>and</strong>ard – 41<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-63

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!