Armstrong Siddeley Ounce
The Armstrong Siddeley Ounce was a small two-cylinder aero engine developed by Armstrong Siddeley in 1920.[1] The engine was originally conceived as a test piece but ran very well and was put into production for early ultralight aircraft and use in target drones. The Ounce used two cylinders from the preceding Jaguar I radial engine.
| Ounce | |
|---|---|
_engine_RAE-O1058.jpg.webp) | |
| Type | Piston engine |
| National origin | United Kingdom |
| Manufacturer | Armstrong Siddeley |
| First run | 1920 |
Specifications (Ounce)
Data from Lumsden.[2]
General characteristics
- Type: Two cylinder, horizontally-opposed air cooled piston engine
- Bore: 5.0 in (127 mm)
- Stroke: 5.0 in (127 mm)
- Displacement: 196 cu in (3.2 L)
- Length: 20.5 in (521 mm)
- Width: 39.5 in (1003 mm)
- Height: 24.5 in (622 mm)
- Dry weight: 170 lb (77 kg)
Performance
- Power output: 45 hp (33.5 kW) at 1,500 rpm
- Compression ratio: 5:1
- Power-to-weight ratio: 0.26 hp/lb (0.43 kW/kg)
See also
Comparable engines
Related lists
References
Notes
- Gunston 1989, p.18.
- Lumsden 2003, p.66.
External links
Wikimedia Commons has media related to Armstrong Siddeley Ounce.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.