Czechoslovak multirole combat aircraft prototype
Letov Š-50
The Letov Š-50 was a 1930s prototype Czechoslovak military general-purpose monoplane, designed and built by Letov.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Letov
- First flight
- 1938-01-01
Specifications
- Cruise speed
- 150 kt
- Max speed
- 165 kt
- Range
- 650 nm
- Service ceiling
- 23,600 ft
- Max takeoff weight
- 9,024 lb
- Empty weight
- 5,456 lb
- Fuel capacity
- 240 US gal
- Powerplant
- 2 × Avia Rk.17
- Engines
- 2
- Seats
- 3
- Length
- 41.3 ft
- Wingspan
- 56.8 ft
- Height
- 12.5 ft
- Number built
- 1
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.