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Flugtriebwerk
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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
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
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
Power Cable Mass Estimation for Electric Aircraft Propulsion
Health Monitoring and Prognostics for More Electric Aircrafts
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
The science, technology, and implementation of TiAl alloys in commercial aircraft engines
Electric Motor Considerations for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Liquid-Hydrogen-Cooled 450-hp Electric Motor Test Stand Being Developed
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Future Concepts for Modular, Intelligent Aerospace Power Systems
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept