TOA-288 & TOW-288
Two cylinder horizontal opposed two cycle engine
Fuel efficient & powerful engine compare to dimensions and weight
Capable to fly under harsh environmental conditions, extreme coldness & high altitude
Fuel efficient & powerful engine compare to dimensions and weight
Capable to fly under harsh environmental conditions, extreme coldness & high altitude
Product Advantages
Optimized power-to-weight ratio (up to 20% better than comparable products)
Optimized fuel consumption
Constantly high production quality through the entire production series
Adaptable to customers’ requirements
Optimized fuel consumption
Constantly high production quality through the entire production series
Adaptable to customers’ requirements
TOA288
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TOW288
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Cooling:
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Air-cooled
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Water-cooled
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Performance:
(according to ISO 1585)
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17,6 kW (23,9 HP) at 6’500 rpm
27,2 Nm (20 lb ft) at 6'000 rpm |
20,0 kW (27,2 HP) at 6’500 RPM
29,2 Nm (21,5 lb ft) at 6'500 RPM |
Fuel efficiency:
(cruise along an propeller curve)
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317 g/kW/h @ 4'700rpm and 6,7 kW
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321 g/kW/h @ 5'100rpm and 12,0 kW
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Fuel efficiency:
(WOT - wide open throttle)
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446 g/kW/h @ 6'500rpm and 17,6 kW
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350 g/kW/h @ 6'500rpm and 20,0 kW
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Fuel efficiency:
(BSFC)
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315 g/kW/h
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306 g/kW/h
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Bore:
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56 mm / 2.20 Inch
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Stroke:
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58.5 mm / 2.30 Inch
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Displacement:
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288 cm³ / 17.58 cu. Inches
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Weight:
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Crankshaft:
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high strength steel, single piece connecting rods with needle bearings
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Throttle control:
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integrated SERVO, controlled via ECU
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Cylinders:
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Casted aluminum, nickel-silicon carbide coated barrel
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Altitude compensation:
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Automatic via ECU
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Fuel:
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min. 95RON (90AON MOGAS) or AVGAS LL100
Mixture: 1:60 (1.6%) 2-stroke oil API TC |
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Optional Equipment:
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Installation:
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Horizontal or vertical
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Helicopter and fix-wing applications
Horizontal or vertical |
Flying Altitude:
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20'000 ft
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TOA / TOW Product Flyer (PDF) |