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Flugtriebwerk
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Initial Regulatory and Certification Approach for the SUSAN Electrofan Concept
X-57 Electromagnetic Interference Design, Integration, and Test Consideration
Conceptual Exploration of Aircraft Configurations for the SUSAN Electrofan
Health Management Considerations for Electrified Aircraft Propulsion Systems
NASA Meeting on Cryogenic Fuel Systems for Aircraft: Overview of Previous Workshops and Studies
Establishing Electrified Aircraft Propulsion Concepts
Introduction to Advanced Engine Control Concepts
Materials Aspects of Turboelectric Aircraft Propulsion
An Overview of Low-Emission Combustion Research at NASA Glenn
Investigation of Current Methods to Identify Helicopter Gear Health
An Experimental Approach to a Rapid Propulsion and Aeronautics Concepts Testbed
Hypersonic Vehicle Propulsion System Simplified Model Development
Small UAV Research and Evolution in Long Endurance Electric Powered Vehicles
Supersonic Cruise Efficiency - Propulsion Tech Challenge Overview
Overview of Engineering Design and Analysis at the NASA John C. Stennis Space Center
System Analysis and Performance Benefits of an Optimized Rotorcraft Propulsion System
The Design and Testing of a Miniature Turbofan Engine
A Cryogenically-Cooled MW Inverter for Electric Aircraft Propulsion
Green Propulsion Technologies for Advanced Air Transports
Ceramic Matrix Composites for Rotorcraft Engines
Aqueous, Quick-Charging Battery Integration for Electric Flight Research (AQUIFER)
Thermal Hydraulics for Nuclear Space Applications
Preliminary Design of the Superconducting Rotor for NASA's High-Efficiency Megawatt Motor
Turbofan Engine Core Compartment Vent Aerodynamic Configuration Development Methodology
Engine Company Evaluation of Feasibility of Aircraft Retrofit Water-Injected Turbomachines
Propulsion Controls Modeling for a Small Turbofan Engine
Rate-Based Model Predictive Control of Turbofan Engine Clearance
Evaluation of an Outer Loop Retrofit Architecture for Intelligent Turbofan Engine Thrust Control
Test Rig for Active Turbine Blade Tip Clearance Control Concepts: An Update
Some Design Considerations for Two-Dimensional, Mixed-Compression Inlets for Mach 2.5 to 3.5.
H2 / DeCarbonization Studies: History and Ongoing
The General Aviation Propulsion (GAP) Program
Automated Power Assessment for Helicopter Turboshaft Engines