12.5kW Advanced Electric Propulsion System Thruster Development Testing
Demonstration of a 600 Watt Hybrid Iodine-Xenon Electric Propulsion System [STUB]
Ion Propulsion System for the Asteroid Redirect Robotic Mission
Facility Effect Characterization Test of NASA's HERMeS Hall Thruster
Overview of NASA Iodine Hall Thruster Propulsion System Development
High Throughput 600 Watt Hall Effect Thruster for Space Exploration
Status of Propulsion Technology Development Under the NASA In-space Propulsion Technology Program
Status of Propulsion Technology Development Under the NASA In-space Propulsion Technology Program
Status of Propulsion Technology Development Under the NASA In-Space Propulsion Technology Program
First Firing of a 100-kW Nested-Channel Hall Thruster
EP of a Different Class: The Challenges of Testing for MW Missions
Electric Propulsion of a Different Class: The Challenges of Testing for MegaWatt Missions
High-Power Hall Propulsion Development at NASA Glenn Research Center
Advanced Diagnostic Characterization of High-Power Hall Thruster Wear and Operation
Radioisotope Electric Propulsion (REP): A Near-Term Approach to Nuclear Propulsion
Overview of Advanced Electromagnetic Propulsion Development at NASA Glenn Research Center