Langley Aerodrome No.8 (LA-8) Electric Vertical Take Off and Landing (VTOL) Aircraft
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
SUbsonic Single Aft eNgine (SUSAN) Power/Propulsion System Control Architecture Updates
Facility Effect Characterization Test of the BHT-6000 Hall Thruster
MISA Symposium: A Roadmap to Our Sustainable Aviation Future
Numerical Propulsion System Simulation (NPSS) Electrical Modeling Validation
Reinforcement Learning Approach to Flight Control Allocation with Distributed Electric Propulsion
Single Throttle Design for the Subsonic Single Aft Engine (SUSAN) Transport Aircraft
Exploring Synoptic Display Concepts for Hybrid-Electric Airliner Flightdecks
Testbed for Electrified Aircraft Propulsion Control Systems Verification
NASA EPFD Project's Progress Towards Reducing Barrier EAP Technology and Integration Risks
Electrified Powertrain Flight Demonstration (EPFD) Overview and Future
Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data
NASA Electrified Aircraft Propulsion Technologies: Infusing and Leveraging Flight Demonstrators
Design of an Open Rotor, Braced-Wing Electric Transport
Design Concepts to Meet EASA SC-VTOL-01 Single Failure Criteria
Development Of 12 Kw Hall Thrusters for Nasa Lunar Gateway Power And Propulsion Element
Power System Redundancy Design Trends for All-Electric eVTOL Quadrotors
1.9 MWe Nuclear Electric Propulsion-Chemical Propulsion Piloted Mars Opposition Vehicle
Ideas for Infusing OSAM into Nuclear Electric Propulsion Architectures
Evaluating the Performance of Hybrid Vehicles between LEO, Cislunar Space, and Mars
Space Superhighway: A Cost Analysis of an In-Space Logistics Resupply Network
Autonomous In-Space Servicing, Assembly, and Manufacturing (ISAM) at NASA Langley
Empirical Vehicle Speed Model for Tuning Throttle Controller Parameters
Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs
NASA Reference Motor Designs for Electric Vertical Takeoff and Landing Vehicles
Charge Mitigation Technologies for Aircraft Platforms
Summary of the NEXT-C Flight Thruster Proto-flight Testing