- Source: Zenoah G-25
The Zenoah G-25 is a single cylinder, two stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft
Development
The Zenoah G-25 is equipped with single capacitor discharge ignition and a single Mikuni slide-type carburetor. It is equipped with a recoil starter system or optionally electric start and a 2.5 or 2.8:1 belt reduction drive.
The engine runs on a mixture of unleaded auto fuel and oil.
Producing 22 hp (16 kW) at 6600 rpm, the G-25 competed in the early 1980s ultralight powerplant market against the similar Rotax 277. Production of the engine was completed in the late 1980s and today only used engines and parts are available.
Applications
Specifications (G-25B-1)
Data from Cliche & Tennessee Propellers
= General characteristics
=Type: Single cylinder, two-stroke aircraft engine
Bore: 72 mm (2.8 in)
Stroke: 59.5 mm (2.3 in)
Displacement: 242 cc (14.78 cu in)
Length: 11.81 in (300.0 mm)
Width: 11.57 in (293.9 mm)
Height: 14.84 in (376.9 mm)
Dry weight: 51 lb (23.1 kg)
= Components
=Valvetrain: piston ported
Fuel type: unleaded auto fuel
Oil system: pre-mixed
Cooling system: free air
Reduction gear: 2.5 or 2.8:1 belt system
= Performance
=Power output: 22 hp (16 kW) at 6600 rpm
Compression ratio: 6.5:1
References
Kata Kunci Pencarian:
- Zenoah G-25
- AmeriPlanes Mitchell Wing A-10
- ISON Airbike
- Personal Flight Sky-Bike
- Paramotor Inc FX series
- G25
- Phoenix Industries CV1 ParaFlyer
- US Aviation CAVU
- Tennessee Propellers
- Jet Pocket Top Must
