THOR 130 EVO

THOR-130-EVO-copia

Product Description

The Thor 130 EVO is born from a technical and innovative restyling of the Thor 130: performance, stability and compactness improve

The Polini THOR 130 EVO is an advanced engine that can adopt two different fuel systems: Ø24 float chamber carburettor or Walbro WG8 carburettor.

The engine was developed and manufactured with craftsmanship criteria through the most modern and advanced production processes, constantly monitored by highly specialized technicians.

TECHNICAL FEATURES
SPECIFIC CYLINDER GROUP
Cast in light aluminum alloy with barrel characterized by nickel-chrome coating for perfect piston sliding. The piston is cast in light alloy with a high silicon content and is complete with two segments of special nitrided and chromed steel.
EXHAUST SYSTEM
The exhaust system is made entirely by hand for greater product quality. Compact design and small dimensions. Reduced dimensions for better aerodynamics. Low noise levels.
COOLING
The forced air cooling system ensures better air flow, optimizing performance while maintaining stable temperatures.
CENTRIFUGAL CLUTCH
The centrifugal clutch is designed to guarantee maximum safety characteristics during all phases of preparation, take-off, flight and landing.
EASY STARTING
The THOR 130 EVO engine is equipped with the Polini “Flash Starter” starting system, extremely simple and very easy to start.
POWER OPTIMIZATION
Enormous power, low consumption, optimized performance at every speed.
ULTIMATE ADVANCED SOLUTIONS
The Polini THOR 130 EVO engine stands out for many other advanced solutions and safety features. Closed circuit system for fuel recovery during transport. 12 V output predisposition for any electrical uses. Very low propeller overturning torque ensured by the particular counter-rotating masses.

100% MADE IN ITALY

  • 928.000.061 – Carburetor Ø 24 – Euro 2,140.00 + VAT
  • 928.000.062 – Walbro WG8 carburettor – Euro 2,160.00 + VAT
Polini engine 2 stroke single cylinder
Cooling down Forced air
Bore per stroke 54 x 54
Displacement 125 cm3
Power 21.5HP
*Max. thrust 67 Kg with Ø 130 cm propeller
RPM max 8,800
Cylinder In aluminum with Gilnisil coating
Compression ratio 12.5:1
Piston Two chromed bands 1 mm
Aspiration Reed valve in the crankcase
Carburetor Walbro WG8 / Polini tray Ø24
Air filter Air boxes
Power on Electronics with possible battery charger
Battery charger preparation Output power 40W at 5500 rpm
Candle cap With 5K Ω resistor
**Diet E5 or LL 100 AV GAS petrol – 2.5% with 100% synthetic oil
*Consumption 2.9 Lh. at 30 kg of static thrust
Gear reducer Helical teeth in oil bath, reduction ratio 3.43
Goodwill Flash Starter
Clutch Oil bath centrifuge
Muffler Expansion with aluminum silencer
Engine weight 13.8 kg
Propeller rotation Clockwise
 

* The values ​​reported were measured at sea level in standard atmosphere. The thrust and consumption values ​​may vary depending on the air temperature and the density level.
** E5 defines the type of petrol that can be used. E5= 95 octane green petrol with maximum 5% ethanol. This symbol is shown on all petrol pumps in Europe.

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