VAZ-416 is an aircraft rotor-piston engine , developed at the VAZ Scientific-Technical Center , intended for installation on light aircraft , as well as on amphibious hovercraft .
| VAZ-416 | |
|---|---|
| Manufacturer | AvtoVAZ |
| Specifications | |
| Volume | 2 x 0,654 |
| Power | 180 HP |
| Number of cylinders | 2 |
| Cooling system | liquid cooling |
| Dimensions | |
| Length | 877 mm |
| Height | 614 mm |
| Dry weight | 125 kg |
Construction
- Lubrication System - Depending on the purpose of the aircraft, the combined lubrication system may be wet or dry.
- The fuel system is electronically controlled distributed injection which is duplicated by a hydromechanical system.
- The ignition system is a two-channel, magneto contactless electronic and battery non-contact electronic-digital.