| CTLS Specifications |
Performance |
| Wing Span: |
28 Feet, 2 Inches |
| Length: |
21 Feet, 8 Inches |
| Height: |
7 Feet, 8 Inches |
| Wing Area: |
107 Square Feet |
| Aspect Ratio: |
7.29:1 |
| Empty Weight: |
770 Pounds |
| Gross Weight: |
1,320 Pounds |
| Fuel Capacity: |
34 Gallons |
| Fuel Economy: |
4.5 Gallons/Hour |
| Powerplant: |
Rotax 912S (100HP) |
| Propellers: |
Ground Adjustable Composite |
| Airfoil Type: |
C 180, 13.8% Thick |
|
| Cruise Speed (@ 75% power) |
115 kts |
| Stall Speed (VS0) |
39 kts |
| VNE |
145 kts |
| Climb Rate |
805 fpm |
| Max. Range; 34 Gal. no reserve |
830 miles |
| Takeoff Roll (@ Wg) |
800 feet |
| Glide Ratio (engine off) |
14:1 |
|
PDF of 3-view Drawings
Rotax® 912S
4 cylinder, 4 stroke liquid/air cooled engine with opposed cylinders, dry sump forced
lubrication with separate 3l (.8 gal US) oil tank, automatic adjustment by
hydraulic valve tappet, 2 CD carburetors, mechanical fuel pump, electronic dual
ignition, electric starter, integrated reduction gear i= 2.43.
KODIAK RESEARCH Rotax North American Website
| 912 S |
kW |
HP |
RPM |
Nm |
ft. lb. |
RPM |
Max RPM |
| Normal |
69.0 |
95 |
5500 |
128 |
94 |
5100 |
5800 |
| Max 5 minute (takeoff) |
73.5 |
100 |
5800 |
|
|
|
|
| |
| Units |
Bore |
Stroke |
Displacement |
Compression Ratio |
|
|
| Metric |
84 mm |
61 mm |
1,352 cc |
10.5:1 |
|
|
| American |
3.31 in |
2.40 in |
82.6 cid |
|
|
|
