Project Status: Research & Design Phase
We are exploring the possibility of building a small aircraft powered entirely by Electrohydrodynamic (EHD) thrust β commonly known as "ion wind" or "electrohydrodynamic propulsion." Instead of using propellers or jet engines, the aircraft would generate thrust by ionizing air molecules and accelerating them with a high-voltage electric field.
This project is inspired by the MIT ion wind aircraft research (Steven Barrett et al., 2018), which demonstrated sustained flight using this technology. Our goal is to build a smaller, DIY version using 3D-printed components and accessible electronics.
βοΈ How It Works
Electrohydrodynamic Thrust
The principle is simple in theory: a thin wire (the emitter) is charged to 20β40 kV. This ionizes the surrounding air molecules, stripping electrons to create positive ions. These ions are then attracted to a nearby surface (the collector) which is grounded or at a lower potential. As the ions travel from emitter to collector, they collide with neutral air molecules, transferring momentum and creating a net airflow β the "ion wind." This wind produces thrust that can propel an aircraft.
π Emitter Wire
Thin tungsten or steel wire (~0.5mm). Charged to 20β40 kV using a boost converter or flyback transformer.
π― Collector Strip
Smooth flat surface or tube at lower potential. Positioned ~25mm from the emitter for optimal ion collection.
π Power Source
Lightweight LiPo or 18650 battery. Boost converter steps up to 20β40 kV. Power consumption is surprisingly low.
πͺΆ Airframe
3D-printed lightweight structure. Wings designed to maximize thrust efficiency from ion wind flow.
π Project Specs (Target)
β οΈ Safety Warning
β‘ High Voltage Hazard β 20β40 kV can cause serious injury or death.
This project involves high-voltage electronics that are dangerous. If you attempt to replicate this project:
- Never power the system while handling exposed electrodes
- Maintain minimum 25mm clearance between emitter and collector at all times
- Use proper insulation and enclosure for all HV components
- Work with experienced supervision if you are new to high-voltage electronics
- This is a research/experimental project β not a finished product
Do not attempt to build this if you are not comfortable working with high voltage.
π¬ Research References
Key Papers & Resources
- MIT Barrett et al. (2018) β "Flight of an electrohydrodynamically powered aircraft" β Nature. First sustained EHD flight.
- MIT Barrett (2021) β Further refinements to EHD propulsion theory and scaling laws.
- FliteTest YouTube β Practical RC aircraft building techniques and 3D printing for RC planes.
π₯ Team
CN
Carlos Nogueira β Project Lead & Builder
F
Feiteira β Hardware & 3D Printing
AI-assisted design & research by Clawdia (OpenClaw AI Agent).
π¨οΈ 3D-Printed Components
All parts designed for Bambu Lab X1C/P1P (256Γ256Γ256mm build volume). Parametric Python scripts generate STL files β edit dimensions in code and regenerate.
βοΈ Fuselage (5 files)
π¦fuselage_shell.stl3.6KBDL
πbattery_bay.stl31KBDL
β‘hv_module_bay.stl14KBDL
π©internal_ribs.stl7.1KBDL
π Emitters (11 files)
πemitter_assembly.stl149KBDL
γ°οΈemitter_frame.stl17KBDL
πwire_support_array.stl74KBDL
πwire_support_post.stl8.3KBDL
βοΈtension_adjuster.stl20KBDL
π²insulator_spacer.stl3.0KBDL
πcollector_smooth_ring.stl57KBDL
β‘emitter_razor_ring.stl30KBDL
πperipheral_thruster_demo.stl99KBDL
πͺrazor_blade_array_demo.stl11KBDL
π thruster_housing_demo.stl66KBDL
π― Collectors (10 files)
π²collector_plate.stl3.0KBDL
πcollector_foil_array.stl4.8KBDL
πΌοΈcollector_with_frame.stl19KBDL
π²collector_mount_frame.stl17KBDL
πadjustable_mount.stl16KBDL
β‘streamer_suppressor.stl2.4KBDL
πcollector_foil_mount.stl5.6KBDL
β‘electroplated_collector.stl47KBDL
π§test_rig_mount.stl11KBDL
βοΈwing_integration_frame.stl3.6KBDL
π© Frame (6 files)
βnode_junction.stl15KBDL
βspine_segment.stl12KBDL
πspine_assembly.stl195KBDL
π΄spine_end_cap.stl3.6KBDL
βοΈwing_mount_plate.stl13KBDL
π²tail_fin_mount.stl6.0KBDL
π‘οΈ Guards / Ducts (3 files)
π²duct_with_struts.stl22KBDL
πwire_guard_mesh.stl28KBDL
πΈ Thrust Stand β 3D Model Previews
Parts for the DIY ion wind thrust stand. Build Option A first to validate the model. All parts are Bambu Lab X1C/P1P compatible.
Option A (EUR64): 35kV / 20mm / 169 mN β single-stage NACA collector. Option B (~EUR80 + PSU): 35kV / 8mm / 1355 mN β ducted tandem 2-stage. Full build guide: GitHub repo.

Emitter Wire Frame β acrylic structure for thin wire

Wire Support Post β one of 9 posts holding emitter wire

Collector Mount Frame β holds foil parallel to emitter

Adjustable Gap Mount β tune gap from 10-40mm

Spine Segment β structural node for acrylic base

Spine Junction Node β joins two spine segments

Fuselage Shell β battery bay + HV module enclosure

Collector Foil Plate β flat copper on acrylic (Option A)

Duct Ring β for ducted tandem Option B upgrade
π STL Files
Generate all STL files with: python3 generate_all.py
All files in the GitHub repo under ion-wind-plane/.
π¬ Ion Wind Simulator
Interactive simulation of Electrohydrodynamic thrust. Adjust parameters to explore performance envelopes.
Direct link: exapix.com/icarus/simulator.html