Interesting progress has been made on the IPROP project in 2024, pushing the boundaries of ionic thruster technology for atmospheric and stratospheric applications. Here the project achievements so far:
鈻笍 饾悁饾悵饾惎饾悮饾惂饾悳饾悽饾惂饾悹 饾悁饾惌饾惁饾惃饾惉饾惄饾悺饾悶饾惈饾悽饾悳 饾悎饾惃饾惂饾悽饾悳 饾悡饾悺饾惈饾惍饾惉饾惌饾悶饾惈饾惉:
路 Development of 2D numerical models for ionization and drift simulations.
路 Promising preliminary results for testing innovative electrode geometries, tripling the thrust with respect to a wire-to-airfoil thruster of same size and voltage.
路 Laboratory experiments in a low-speed wind tunnel have been performed on a wire-to-airfoil thruster with the purpose of evaluating changes in performance due to simulated flight conditions and, for the first time, comparing them with a simple physical model of the drift region which is in good agreement with the laboratory data.
路 An experiment about ionization processes between electrodes in a cylindrical geometry is in progress with the aim of creating a reference for the theoretical and numerical ionization studies.
路 Different techniques for measuring thrust, electrical parameters and flow characteristic are being tested in this phase of the research program, also including particle image velocimetry measures on electrodes systems of different sizes, shapes and materials.
路 A testing campaign on the behaviour of ionic thrusters according to environmental conditions has just begun. different laboratory configurations are being prepared for testing the ion thruster鈥檚 performance against wide changes of the external conditions such as air pressure, temperature, humidity, radiations. These experiments will also include insulation tests and studies of the electrodes aging.
鈻笍 饾悞饾惁饾悮饾惀饾惀-饾悞饾悳饾悮饾惀饾悶 饾悁饾悽饾惈饾惉饾悺饾悽饾惄 饾悆饾悶饾惁饾惃饾惂饾惉饾惌饾惈饾悮饾惌饾惃饾惈, 饾悳饾悮饾惄饾悮饾悰饾惀饾悶 饾惃饾悷 饾悮饾惍饾惌饾惃饾惂饾惃饾惁饾惃饾惍饾惉 饾悷饾惀饾悽饾悹饾悺饾惌 饾悽饾惂 饾惉饾惌饾悮饾惂饾悵饾悮饾惈饾悵 饾悮饾惌饾惁饾惃饾惉饾惄饾悺饾悶饾惈饾悶 饾惏饾悽饾惌饾悺 饾悹饾惃饾惃饾悵 饾惄饾悶饾惈饾悷饾惃饾惈饾惁饾悮饾惂饾悳饾悶
路 Early design work on airships powered by ion thrusters.
路 A novel approach to integrating ultra-lightweight power systems for low-altitude missions.
鈻笍 饾悡饾惃饾惏饾悮饾惈饾悵饾惉 饾悞饾惌饾惈饾悮饾惌饾惃饾惉饾惄饾悺饾悶饾惈饾悽饾悳 饾悁饾悽饾惈饾惉饾悺饾悽饾惄饾惉 (饾悋饾悁饾悘饾悞):
路 Initial feasibility studies for full-scale ionic airships operating at stratospheric altitudes has already started.
路 A first application to the sizing of a high-altitude demonstration mission has been presented, working on data for a full-scale prototype.
For more information check the Research page on IPROP website: https://www.iprop-project.eu/research/
Our team is delighted about these promising results, which bring us closer to groundbreaking advancements in sustainable flight and high-altitude applications.