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Flugtriebwerk
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keywords:(Flugtriebwerk)
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Power Quality Analysis for a High Voltage Power System for Urban Air Mobility Application
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Investigation of Rectifier Diode Failures in the NEXT-C Power Processing Unit
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Power Cable Mass Estimation for Electric Aircraft Propulsion
X-57 Maxwell Battery from Cell Level to System Level Design and Testing
Health Monitoring and Prognostics for More Electric Aircrafts
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
Impedance Measurements of Motor Drives and Supplies in NASA NEAT Facility
Future Concepts for Modular, Intelligent Aerospace Power Systems
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
A Study on the Use of Solid-Oxide Fuel Cells for Increased Power Generation on Small Aircraft
Electric Motors for Non-Cryogenic Hybrid Electric and Turboelectric Propulsion
Design and Performance of a Hybrid-Electric Fuel Cell Flight Demonstration Concept