Mosler Red 82X
| Mosler Red 82X | |
|---|---|
| Type | Experimental aircraft engine |
| Manufacturer | Mosler Motors |
| Major applications | Luscombe 8A |
The Mosler Red 82X is an experimental four cylinder, four stroke engine developed as a low cost replacement for older aircraft.
Design and development[edit]
A Red 82X was tested in April 1992 on a Luscombe 8A certified in the experimental-exhibition category.[1]
Variants[edit]
- Red 82X
- Red 82DX
- Dual ignition
- Red 82LB
- No ignition packaged
Specifications (Red 82X)[edit]
General characteristics
- Type: 4-cylinder, air-cooled, horizontally opposed engine
- Bore: 94 mm
- Stroke: 78 mm
- Displacement: 2,165 cc
- Length: 24 in
- Width: 30 in
- Height: 18 in
- Dry weight: 182 lb
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder Hydraulic lifters
- Cooling system: Air
Performance
- Power output: 82 hp at 3,200 rpm
See also[edit]
Related lists
References[edit]
- ^ "Mosler Powered Luscombe Makes First Flight". Air Progress. March 1993.