Letov Š-25
| Letov Š-25 | |
|---|---|
| Type: | Trainer aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
1930 |
| Number of pieces: |
1 prototype |
The Letov Š-25 is a single-engine, two-seat biplane that was developed as a training aircraft . The first flight took place in 1930. The aircraft designed by Alois Šmolík was manufactured in the Letov factory in Letňany near Prague in Czechoslovakia.
Only a prototype was made.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 2 |
| length | 9.45 m |
| span | 11.35 m |
| height | k. A. |
| Wing area | 19.40 m² |
| Wing loading | 59.5 kg / m² |
| Empty mass | 960 kg |
| Takeoff mass | 1180 kg |
| drive | 1 × Škoda HS 8 Fb with 221 kW (300 PS) |
| Top speed | 197 km / h |
| Cruising speed | 165 km / h |
| Rise time | 25 min at 4000 m altitude |
| Service ceiling | 4700 m |
| Range | 600 km |
See also
Web links
- Letov Š-25 on vinar.cz (Czech)
- Letov Š-25 on airwar.cz (Russian)