Hello everyone, new here. I want to share the results of our testing of a prototype electric propulsion unit for light aviation with a power of 80-100 hp. Our tests showed that the 190 kg thrust that we get from our electric setup is enough for the aircraft takeoff and ascent. ✈️✈️✈️ Since we're new to electric aircraft in general, I'm curious to hear some thoughts about our tests from people who have more experience in this area. P.S. English captions available
