Proposal for a small two-seater tandem ultralight aircraft, with thermal or electric engine, with folding wings* and towable without a trailer.
Wing area: 10.80m2
In thermal version, with a 25 to 30k* engine, 20 liters of petrol and 160k of crew: 330 k. That is a wing loading of 30.5 k/m2
In electric version, with a 35 to 45 KW motor + 90k of batteries* and the same crew of 160k: 390k. That is a wing loading of 36 k/m2
- Like a Hirth F23, 50hp or why not a Polini 303, 38hp if the aircraft is built very light??
- For approximately 1h autonomy
- The folding wing priciple is described in my previous articles
The plans have been scanned but the wingtips are missing!