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Overview of NASA GRC Electrified Aircraft Propulsion (EAP) Controls Research
NASA Power and Thermal Technology Overview
Electrified Aircraft Propulsion Controls Hardware Testing
NASA’s Electric Aircraft Propulsion Research: Yesterday, Today and Tomorrow
Foundational Electrified Aircraft Propulsion Overview
Overview of NASA Electrified Aircraft Propulsion Controls Research
Health Management Considerations for Electrified Aircraft Propulsion Systems
High Efficiency Megawatt Motor Conceptual Design
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
An Electrical Modeling and Thermal Analysis Toolbox for Electrified Aircraft Propulsion Simulation
Optimizing Thermal Management Systems in Electric Aircraft
System-Level Impact of Propulsive Uncertainties for Low-Boom Aircraft Concepts
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 Overview of NASA’s AAM Electric Aircraft Propulsion
Battery Key Performance Projections based on Historical Trends and Chemistries
NASA AERONAUTICS: Electrified Aircraft Propulsion Research Overview
NASA Reference Motor Designs for Electric Vertical Takeoff and Landing Vehicles
Electric Propulsion: Challenges and Opportunities
Health Management Considerations for Electrified Aircraft Propulsion Systems
Validation of Software Tools for the Analysis of Electrified Aircraft
Results of NASA's Magnetic Gear Program to Date
Reliability Requirements and Research Strategies for Urban Air Mobility Propulsion
Design of a Magnetic Gear for NASA's Vertical Lift Quadrotor Reference Vehicle
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
CFD Evaluation Of Lean-Direct Injection Combustors for Commercial Supersonics Technology
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Overview of NASA Electrified Aircraft Propulsion Activities
Health Monitoring and Prognostics for More Electric Aircrafts
Real-time Hardware-in-the-Loop Evaluation of a Partially Turboelectric Propulsion Control Design
High Voltage Hybrid Electric Propulsion (HVHEP) Activity
Overview of the NASA STARC-ABL (Rev. B) Advanced Concept