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.
Preliminary Specifications | Units | |
Service Ceiling | FL | 250 |
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 |