New Voltage and Current Thresholds Determined for Sustained Space Plasma Arcing
System Analysis Initiated for All-Electric Aircraft Propulsion
Polymer Energy Rechargeable System Battery Being Developed
High-Power Hall Thruster Technology Evaluated for Primary Propulsion Applications
Development Efforts Expanded in Ion Propulsion: Ion Thrusters Developed With Higher Power Levels
Pulsed Plasma Thruster (PPT) Technology: Earth Observing-1 PPT Operational and Advanced Components Being Developed
New Technique of High-Performance Torque Control Developed for Induction Machines
New Active Optical Technique Developed for Measuring Low-Earth-Orbit Atomic Oxygen Erosion of Polymers
Thermal Contributions to the Degradation of Ground-Laboratory- and Space-Irradiated Teflon Investigated
Greener Method Developed for Intercalating Graphite Fibers With Bromine
Solar Selective Coatings Prepared From Thin-Film Molecular Mixtures and Evaluated
Power Electronics Being Developed for Deep Space Cryogenic Applications
Microelectromechanical System (MEMS) Device Being Developed for Active Cooling and Temperature Control
Three-Dimensional Magnetic Analysis Technique Developed for Evaluating Stirling Convertor Linear Alternators
Brayton Power Conversion Unit Tested--Provides a Path to Future High-Power Electric Propulsion Missions
Stirling Convertor Technologies Being Developed for a Stirling Radioisotope Generator
Mercury Conditions for the Messenger Mission Simulated in High-Solar-Radiation Vacuum Tests
Last updated: June 25, 2003
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