Revmaster R-2100D
The Revmaster 2100D is a Volkswagen air-cooled engine modified for homebuilt aircraft with dual magneto ignition.[1][2][3]
| R-2100D | |
|---|---|
| Type | Horizontally opposed piston engine |
| Manufacturer | Revmaster |
| Designed by | Joe Horvath |
| Unit cost | $1,095 in 1971 |
| Developed from | Volkswagen air-cooled engine |
Specifications (variant)
General characteristics
- Bore: 92
- Stroke: 78
- Displacement: 2073cc
Components
- Valvetrain: Single overhead exhaust valve, single side inlet valve per cylinder
- Fuel system: Single carburettor
- Cooling system: Air-cooled
- Tillotson Floatless Carburetor
Performance
- Power output: 65hp
References
- Air Trails: 85. Winter 1971. Missing or empty
|title=(help) - Sport Aviation: 21. September 1977. Missing or empty
|title=(help) - "The Maloof Controllable Propeller". Sport Aviation. January 1978.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.