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Flugtriebwerk
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Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
Electrified Aircraft Propulsion Controls Hardware Testing
Continued Exploration of the Electrified Aircraft Propulsion Design Space
NASA’s Quiet Electric ENgines (QUEEN): Summary of the QUEEN V2 Test
Electrical Propulsive Fuselage Concept for Transonic Transport Aircraft
Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
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
Feasibility of a Solid Oxide Fuel Cell System Applied to Hybrid-Electric Regional Aircraft
Propulsion System Optimization for a Turboelectric Tiltwing Urban Air Mobility Aircraft
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project
NASA Electrified Aircraft Propulsion Efforts
Remaining Flying Time Prediction Implementing Battery Prognostics Framework for Electric UAV's
Turbine Electrified Energy Management (TEEM) For Enabling More Efficient Engine Designs
Electrical System Trade Study for SUSAN Electrofan Concept Vehicle
Update on SUSAN Concept Vehicle Power and Propulsion System
Optimization of an Air Core Dual Halbach Array Axial Flux Rim Drive for Electric Aircraft
High Efficiency Megawatt Motor Conceptual Design
Power Cable Mass Estimation for Electric Aircraft Propulsion
Results for an Electrified Aircraft Propulsion Design Exploration
Real-time Hardware-in-the-Loop Evaluation of a Partially Turboelectric Propulsion Control Design
Design of a High Power Density, High Efficiency, Low THD 250kW Converter for Electric Aircraft
Low-Noise Operating Mode for Propeller-Driven Electric Airplanes
Virtual Flight Demonstration of the Stratospheric Dual-Aircraft Platform
Implementation Approach for an Electrified Aircraft Concept Vehicle in a Research Flight Simulator
Design of a Magnetic Gear for NASA's Vertical Lift Quadrotor Concept Vehicle
NASA's Magnetic Gearing Research for Electrified Aircraft Propulsion
Resonance and Tones in Dual-Stream Nozzle Flows
Development of a Rotating Rake Array for Boundary-Layer-Ingesting Fan-Stage Measurements
Revolutionary Aeropropulsion Concept for Sustainable Aviation: Turboelectric Distributed Propulsion
An Intelligent Propulsion Control Architecture to Enable More Autonomous Vehicle Operation
Advanced Single-Aisle Transport Propulsion Design Options Revisited
Battery Key Performance Projections based on Historical Trends and Chemistries
Development and Testing of Propulsion Health Management
Requirements for a Hydrogen Powered All-Electric Manned Helicopter
Modeling and Control Design for a Turboelectric Single Aisle Aircraft Propulsion System