Skat is used to accommodate the pilot and passenger, and is designed to fly with paragliding wing.
Skat was designed for the avia tourism and outgoing flights, provides easy takeoff and landing as well as comfort position of the pilot and passenger during the flight.
All power units of powered parachute are made from high-strength and lightweight titanium alloys. The advantage of the Skat is also in its compactness when folded. The process of assembly and disassembly takes less than 10 minutes.
Paraavis also offers an upgraded version - Skate 2. The main differencies of Skat-2 - it is increased fences diameter, which lets to install the propeller 1.6 m, which increases static thrust on the all modes on engine running.
Advantages:
- Well balanced composition with optimum weight distribution, ensures high stability and sustainability.
- Due to the fact that the lever unloaded with tape wing attachment has a large margin of safety, and contributes to the maintenance of stability in flight.
- Effective vibration damping of engine is due to energy-intensive damper motor and silent block mounting frame engine is the second level of protection against vibration.
- Easily demountable basic and nose gear.
- Engine composition cylinder heads up provides the best lubrication of the crank mechanism which increases its lifetime, and contributes to reliable starting of the engine as minimize the possibility of "Gulf" of spark plugs.
- Engine is equipped with electric and hand starter.
- Comfortable pilot's and passenger seats..
- Front landing gear equipped with pneumatic shock-absorber and as option with brake disc of the front wheel.
- Wide tires of the wheels make it easy take off the loose soil.
- Enhanced propeller fencing and energy intensive gear with the main pillars of the titanium alloy have high passive safety.
Technical data:
|
Engine RMZ 550 |
Two-cylinder, two-stroke, air-cooled |
|
Working capacity, сm3 |
553 |
|
Bore x stroke, mm |
76 / 61 |
|
Engine weight*, кg |
32 |
|
Compression ratio |
10,8 |
|
Capacity max., h.p |
50 |
|
RPM max/min |
6400 |
|
Petrol |
Petrol RON -95 with mixture with synthetic oil 2,5% |
|
Oil |
Synthetic, 2-cycle air cooling |
|
Fuel flow, lt/h** |
8...12 |
|
Gear unit |
ribbed |
|
Ratio reducing gear |
1:2,35 |
|
Sparkle |
NGK B9ES или NGK BR9ES |
|
Fuel system |
MIKUNI VM 34 2pcs. |
|
Engine system |
electronic «DUCATI» |
* Engine weight with resonator and exhaust.
** Fuel flow in horizontal flight.