AIRCRAFT SPECIFICATIONS
|
VALUE |
| Engine Type |
Fuel Injected two-stroke, single cylinder, air cooled |
| Power |
2.1 kW |
| Fuel Consumption |
400 g/kWh in cruise |
| Fuel type |
Automotive 95+ octane |
| Displacement |
28 cc |
| Speed range |
1600-8500 rpm |
| Engine Life |
>500 hours 1) |
| Oil / Gasoline Ratio |
1:50 / 2% mix |
| Recommended 2-bladed Propellers |
16x10, 18x8, 18x10, 19x11, 20x8 |
| Recommended 3-bladed Propellers |
16x8, 16x10 |
| Engine weight (including generator, cooling system, servo , air filter ) |
1500 grams |
| Muffler |
Combined reactive-dissipative, proprietary design |
| Sound level, measured from 30 m distance |
59 dB |
| Detectability range @ 5000 RPM |
<700m |
| FUEL PUMP SPECIFICATIONS |
|
| Fuel Pump Lifetime |
Over 2000 hours |
| Fuel priming |
Self-priming |
| Weight |
70 grams |
| ENGINE CONTROL UNIT (ECU) SPECIFICATIONS |
|
| Throttle control |
CAN (Piccolo autopilot compatible), RS232, PWM, Analog (0-5V) |
| Autopilot compatibility |
28 cc EFI |
| Pump control |
Integrated pump controller |
| Cylinder head temperature control |
Integrated controller with PWM output |
| Weight |
170 grams |
| Input Voltage |
10-24V |
| Power (ignition module, ECU, pump, servo , injectors) |
<15W @ maximum RPM |
| Environmental protection |
Fully sealed, IP64 |
| Size |
86x107x22.3 mm |
|
