| Wing
Span |
27.5
feet |
| Canard Span |
13.2 feet |
| Over-all Length |
22.0 feet |
| Over-all Height (top of fins) |
8.5 feet |
| Landing Gear Track |
7.0 feet |
| Landing Gear Wheelbase |
7.2 feet |
| Maximum Cockpit Width |
50 inches |
| Maximum Cockpit Depth (Floor to Canopy) |
42 inches |
| Cockpit Length |
85 inches |
| |
| AREAS |
|
| Wing |
57.68ft2 |
| Wing
Center Section |
34.68ft2 |
| Wing/Wing
Center Section Total |
92.36ft2 |
| Canard |
21.3ft2 |
| |
| SWEEP (quarter chord) |
|
| Wing |
-13.71degrees |
| Wing Center Section (Beaver) |
-8.93 degrees |
| Canard |
12.86 degrees |
| |
| AIRFOILS
|
|
| Wing |
NASA (MS(1)-0313) |
| Wing Center Section |
Modified (MS(1)-0313) |
| Canard |
NASA GAW-2 |
| Vertical Tails |
Modified (MS(1)-0313) |
| Ventral Fins |
Modified (MS(1)-0313) |
| |
| FLAP |
30% chord, single slot, wing and canard |
| |
| CONTROLS
|
|
| Pitch |
Elevators mounted on wing center
section |
| Roll |
Conventional ailerons |
| Yaw |
Conventional rudders |
| Cockpit |
Dual sticks and rudder pedals |
| Trim |
3 axis electric, stick mounted |
| |
| POWERPLANT |
Continental TSIO 360-DB |
| Take-off Horsepower |
225 BHP |
| Critical Altitude |
18,000 feet |
| |
| PROPELLER |
5.25 feet diameter, 4 blades, constant speed, advanced geometry |
