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Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
NASA’s Electric Aircraft Propulsion Research: Yesterday, Today and Tomorrow
Foundational Electrified Aircraft Propulsion Overview
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
NASA Power and Thermal Technology Overview
Electrified Aircraft Propulsion Controls Hardware Testing
Electrified Aircraft Propulsion Controls Hardware Testing
System-Level Control Concepts for Electrified Aircraft Propulsion Systems
Continued Exploration of the Electrified Aircraft Propulsion Design Space
Hybrid Electric MC-12 Ground Testing Plan Chapter
Validation of Software Tools for the Analysis of Electrified Aircraft
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Overview of NASA Electrified Aircraft Propulsion Controls Research
Health Management Considerations for Electrified Aircraft Propulsion Systems
Electrical Propulsive Fuselage Concept for Transonic Transport Aircraft
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Cruise Propulsion System Thermal Analysis for NASA’s X-57 “Maxwell” Mod II Configuration
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Optimizing Thermal Management Systems in Electric Aircraft
Additive Manufacture of Refractory Metal Green Propulsion Thrusters
Power Quality Analysis for a High Voltage Power System for Urban Air Mobility Application
Investigation of Rectifier Diode Failures in the NEXT-C Power Processing Unit
Cruise Propulsion System Thermal Analysis for NASA’s X-57 “Maxwell” Mod II Configuration
NASA Aeronautics Electrified Aircraft Propulsion (EAP) Research Overview
Aircraft Transportation Electrification Eco-System and Technologies
Electromagnetic Redesign of NASA’s High Efficiency Megawatt Motor
An Electrical Modeling and Thermal Analysis Toolbox for Electrified Aircraft Propulsion Simulation
An Overview of NASA’s AAM Electric Aircraft Propulsion
Battery Key Performance Projections based on Historical Trends and Chemistries
Estimating Inducer Blade Damping in Water with On-Blade Strain Measurements
NASA AERONAUTICS: Electrified Aircraft Propulsion Research Overview
NASA Reference Motor Designs for Electric Vertical Takeoff and Landing Vehicles
Health Management Considerations for Electrified Aircraft Propulsion Systems
Design of a Magnetic Gear for NASA's Vertical Lift Quadrotor Concept Vehicle
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
NASA Electrified Propulsion Research Summary