First-Principles-Based Battery Model Investigated for the International Space Station
Glenn’s Fuel Cell Test Laboratory Became Operational
Life-Cycle Testing of Mars Surveyor Program Lander Lithium-Ion Battery Achieved Over 10,000Low-Earth-Orbit Cycles
Flywheel Integrated Power and Attitude Control System Demonstrated
High-Power Hall Thruster Designed for Exploration Applications
Piezoelectric Ignition Systems Demonstrated for Spacecraft Propulsion Applications
Microwave Discharge and Neutralization Plasma Production
Developed as an Alternative to Direct-CurrentHollow Cathode Plasmas for Ion Propulsion
Hall Thruster Developed for Robotic Science Missions
Electric Propulsion Technology Developed for Prometheus 1
Brayton-Cycle Power-Conversion Unit Tested for Operational Vibration Levels
Novel Analysis Tools Created to Enable Stirling Radioisotope Space Power Systems
Brayton Power-Conversion Modeling Enhanced With Closed-Cycle System Simulation
Stirling Power Convertors Demonstrated in Extended Operation
Alpha-Voltaic Power Source Designs Investigated
Carbon Nanotubes Synthesized and Assessed for Space Photovoltaics
Indium Arsenide (InAs) Quantum Dots Grown for Space Solar Cells
Integrated Photovoltaic and Communications Technology Demonstrated
Contamination Flakes in the Discharge Chamber of a NASA Solar Electric Propulsion Technology Readiness (NSTAR) Ion Engine Found To Be Test-Cell Generated
Conductive Thermoplastic Composites Fabricated
Honeycomb Target Evaluated for Reducing Backsputter From Chamber Walls During Long-Life Tests of Ion Thrusters
Silicon Germanium Power Transistors Developed for Cryogenic Space Missions
Last updated: October 12, 2006 11:11 AM
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