Letov Š-50
| Letov Š-50 | |
|---|---|
| Role | General utility monoplane |
| National origin | Czechoslovakia |
| Manufacturer | Letov |
| First flight | 1938 |
| Number built | 1 |
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The Letov Š-50 was a 1930s prototype Czechoslovakian military general purpose monoplane designed and built by Letov.[1]
Development
The Š-50 was an all-metal twin-engined low mid-wing monoplane that first flew in 1938.[1] Powered by two 420 hp (313 kW) Avia Rk.17 radial engines.[1] It had a fixed landing gear and twin fins and rudders. Following the German occupation development was stopped.[1]
Specifications
Data from [1]
General characteristics
- Crew: 3
- Powerplant: 2 × Avia Rk.17 radial piston engine, 310 kW (420 hp) each
Performance
- Maximum speed: 305 km/h (190 mph; 165 kn)
References
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Wikimedia Commons has media related to Letov aircraft. |
- Notes
- Bibliography
- The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
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