With two new engines, the R 80 and the R 120, HE Paramotores confirms its will to consolidate its technical know-how and to constantly innovate. In doing so, HE strives to offer its customers greater performance, durability, and more aesthetic engines.
With a purified design, all the lessons learnt in the past are concentrated in the R Series engines which do not cease to surprise us such the synergies restored are exceptional.
HE Paramotores proudly presents the first engine in the « R » series characterised by its great reliability and power at low regimes.
Click on the following link to download the user manual from the
manufacturer's website:
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Technical characteristics |
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C.c. |
cm3 |
80 |
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Compression rates |
cm3 |
8/1 |
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Power |
HP |
16 |
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kW |
11,19 |
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Revs/min |
9.400 |
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Weight of the engine including: the muffler, exhaust pipe, the air filter and the propeller. |
12 Kg. |
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Laminar aspiration with a carburettor Walbro WG 8-1 |
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Cylinder of aluminium with ceramic coating in Nikasil |
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System of unloading to resonance. Helicoďdal gear reduction |
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Manual pull start |
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In flight consumption with at 6400 turns, 3 litres/hour |
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Lubrication premix of 2,5% with petrol super and 3% with unleaded petrol |
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(*) depending on prop. size, material, shape and on meteorological conditions, altitude
With two new engines, the R 80 and the R 120, HE Paramotores confirms its will to consolidate its technical know-how and to constantly innovate. In doing so, HE strives to offer its customers greater performance, durability, and more aesthetic engines.
With a purified design, all the lessons learnt in the past are concentrated in the R Series engines which do not cease to surprise us such the synergies restored are exceptional.
HE Paramotores proudly presents its latest engine in the “R” range. The R 120 has been specifically designed for carrying people weighing around 100 kilos (+/- 20 kilos).
It’s main characteristics are:
Click on the following link to download the user manual from the
manufacturer's website:
|
Technical characteristics |
||
|
C.c. |
cm3 |
120 |
|
Compression rates |
cm3 |
11/1 |
|
Power |
HP |
20 |
|
kW |
15 |
|
|
Revs/min |
9.700 |
|
|
Weight of the engine including: the muffler, exhaust pipe, the air filter and the propeller. |
13 Kg. |
|
|
Laminar aspiration with a carburettor Walbro WG 8-1 |
||
|
Cylinder of aluminium with ceramic coating in Nikasil |
||
|
System of unloading to resonance. Helicoďdal gear reduction |
||
|
Manual pull start |
||
|
In flight consumption with at 6400 turns, 3 litres/hour |
||
|
Lubrication premix of 2,5% with petrol super and 3% with unleaded petrol |
||
|
|
|
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(*) depending on prop. size, material, shape and on meteorological conditions, altitude