Key Features
Specifications
Documentation
CAD Files
- Low Vibration: Opposed twin layout for reduced primary vibration compared to single cylinder engines.
- Isolation: custom focal isolation mount reduces airframe and payload vibration.
- Quiet: custom exhaust dramatically reduces sound signature compared to stock exhaust.
- Reliability: Four-bearing crankshaft and high rod/stroke ratio for reduced stress. FAR33 tested.
- Cooling: Integrated cooling ducts with cylinder-independent actively controlled cooling doors.
- Generator: PTO mounted in-runner sensored starter/generator.
- Compatibility: Readily integrates with flight control systems; available with Power4Flight IntelliJect EFI.
| Engine Type: | Forced air-cooled 2-stroke twin |
| Displacement: | 100 cc (6.1 ci) |
| Weight: | 3.7 kg (8.2 lbs) quiet exhaust |
| Power (6000 RPM): | 5.0 kW (6.7 hp) at 6600 RPM |
| BSFC (4000 – 5000 RPM): | 500 g/kW-hr (.82 lb/hp-hr) |
| Fuel Type: | Gasoline, 50:1 Premix |
| Starter/Generator: | 80 Amps starting current. 500W continuous electricity generation above 4000 RPM. |
Data Sheet: B100i-PRX UAV Engine Datasheet
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