Conceptual design of a high-performance light canard-configured airplane.
The project has been initiated by a North America based customer aiming to create a nicely looking canard-configured light airplane. The configuration implies a four full-size seat cabin. Also, the concept features carbon fiber composite structure, Lycoming TIO-540-A piston engine or TP100 small turboprop.
|Max Cruise Speed @ FL250||KTAS||250|
|Economy Cruise Speed @ FL220||KTAS||220|
|Stall Speed (or Min Speed)||knots||60|
|Range Full Fuel||NM||1,460|