| Aircraft: | LSA850-130 |
| Photo1: |  |
| CATEGORY | B3 Motors (Piston / Rotary / Turbine Engines) |
| DESCRIPTION (english): | Type 2-cylinder, 4 stroke inline parallel twin with balancer shaft, 4 valves per cylinder with OHC
Power 91 kW (130 hp) @ 7,500 rpm
Torque max. 130 Nm (100 Nm above 3,000 rpm)
Reduction Gear two stage, helical gear 3.33:1 |
| DESCRIPTION (french): | Torque max. 130 Nm (100 Nm above 3,000 rpm)
Reduction Gear two stage, helical gear 3.33:1
Fuel Requirement ? 93 RON
Displacement 850 cc
Bore x Stroke 89mm x 68mm
Fuel Management turbocharger, fuel injection, electronic throttle
Compression ratio 9:1
Alternator internal, 500 W nominal@12V (37A)
Cooling integrated oil cooler,
turbocharger with intercooler
Starter integrated electric-starter
Control electronic engine control system LSA 850
Lubrication System wet sump or dry sump
Weight 85 kg
TBO 1500 h |
| PRICE PRICE_EXCL_VAT | 18750 € |
| Cycle: | 4 stroke |
| Number of cylinders: | 2 |
| Bore (mm): | 89 |
| Stroke (mm): | 68 |
| Compression ratio (*/1): | 9/1 |
| Displacement (cm3): | 850 |
| Cooling: | Liquid |
| Ignition: | Electronic |
| Reduction type: | Mechanical |
| Reduction mechanism: | Helical Gears |
| Reduction ratio: | 1:3,33 |
| Weight (kg): | 85 |
| Max power (hp@rev/min): | 130@7500 |
| Max torque (Nm@rev/min): | 130@3300 |
| Fuel: | 95 |
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