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Ion
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Post-Test Inspection of Nasa's Evolutionary Xenon Thruster Long Duration Test Hardware: Ion Optics
Development Status of High-Thrust Density Electrostatic Engines
Life test of the Deep Space 1 ion engine
Variable specific impulse high power ion thruster
NSTAR: Overview and Status of NASA's Program to Validate Ion Propulsion Technology
Comparison of NASA's 30-cm Ion Thruster Capabilities with the Dawn Mission Requirements
Operating Characteristics of a 15-cm dia. Ion Engine for Small Planetary Spacecraft
Implementation of the dawn ion propulsion system
A 100 Hour Wear Test of the NASA NSTAR Ion Thruster
High voltage breakdown limits of molybdenum and carbon-based grids for ion thrusters
Vibration test and analysis of the NEXIS ion engine
Performance Characteristics of the NSTAR Ion Thruster During an On-Going Long Duration Ground Test
The Role of Analysis and Testing in the Service Life Assessment of Ion Engines
NSTAR Technology Validation Report
Development of Nanosized/Nanostructured Silicon as Advanced Anodes for Lithium-Ion Cells
Performance testing of lithium-ion cells at JPL for future NASA aerospace applications
Numerical simulations of ion thruster accelerator grid erosion
Experimental and computational investigation of the performance of a micro-ion thruster
International Space Station Lithium-Ion Battery Safety Considerations
Performance Evaluation of an Expanded Range XIPS Ion Thruster System for NASA Science Missions
The DS1 hyper-extended mission
Performance of the NSTAR ion propulsion system on the Deep Space One mission
Design and Testing of a Hall Effect Thruster with 3D Printed Channel and Propellant Distributor
Point-of-Use Xenen Purity Provision for Ion Propulsion System on Deep Space One
Performance tesing of Lithion 8-cell, 25AHr Lithium-ion batteries for future aerospace applications
Xenon Acquisition Strategies for High-Power Electric Propulsion NASA Missions
Advanced Ion Propulsion Systems for Affordable Deep-Space Missions
The Ion Propulsion System for the Solar Electric Propulsion Technology Demonstration Mission
The Ion Propulsion System for the Solar Electric Propulsion Technology Demonstration Mission
Low temperature lithium-ion electrolyte development at JPL for aerospace applications
Next generation of ion propulsion: setting up new requirements for trajectory optimizations