top of page

Significance

Electroaerodynamic Thruster

Electroaerodynamic (EAD) propulsion aims to bridge a critical gap in current aerospace technologies. Conventional jet engines generate sufficient thrust but rely on combustion processes that produce greenhouse gases, while electrostatic ion drives offer clean, quiet propulsion yet remain practical only in the vacuum of space. Developing in-atmosphere EAD thrusters provides a pathway to zero-emission flight that could dramatically reduce noise pollution and carbon footprints. If EAD engines can be scaled to produce thrust sufficient for vertical takeoff and landing (VTOL), the aviation industry and broader transportation sector stand to gain transformative benefits in efficiency, sustainability, and operational flexibility.

Overcoming Challenges and Research Milestones

1

Enhancing Thrust-to-Weight Ratio

Employing asymmetric electrodes, refined spacing, and novel geometrical layouts to reduce energy losses.

2

Achieving Practical In-Flight Integration

Using computational fluid dynamics (CFD) and electrostatic simulations, followed by small-scale laboratory models to validate performance before full-scale prototypes.

Department of Electrical and Computer Engineering

University of Washington
185 E Stevens Way NE
Seattle, WA 98195

Connect With Us

  • LinkedIn

© 2025 by ARC Lab. All Rights Reserved.

bottom of page