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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Investigation of Rectifier Diode Failures in the NEXT-C Power Processing Unit
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Power Quality Analysis for a High Voltage Power System for Urban Air Mobility Application
Power Cable Mass Estimation for Electric Aircraft Propulsion
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Health Monitoring and Prognostics for More Electric Aircrafts
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
Time-Varying Operating Condition–Based Prediction of the Remaining Useful Life for Aeroengine
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Electric Motor Considerations for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
New Franklin engine offers increased performance
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
An End-To-End Test of A Simulated Nuclear Electric Propulsion System