From Wikipedia, the free encyclopedia
The Siemens-Halske Sh 14 was a seven-cylinder air-cooled radial engine for aircraft produced in Germany in the 1920s and 30s. First run in 1928, it was rated at 93 kW (125 hp).
[edit] Specifications (Sh 14A)
General characteristics
- Type: 7 clinder air cooled radial engine
- Bore: 108mm (4.25 in)
- Stroke: 120mm (4.75 in)
- Displacement: 7.69 L (469.7 cu in)
- Length: 975mm (38.39 in)
- Width: mm (in)
- Height: 936mm (36.85 in)
- Dry weight: 135kg (297.6 lb)
Components
- Valvetrain: 1 inlet and 1 exhaust valve per cylinder
- Fuel type: 80 octane
- Cooling system: air
Performance
[edit] Applications
[edit] References
Lists relating to aviation |
|
General |
|
|
Military |
|
|
Accidents/incidents |
|
|
Records |
|
|