Letov Š-5
| Letov Š-5 | |
|---|---|
| Type: | Reconnaissance plane |
| Design country: | |
| Manufacturer: | |
| First flight: |
1923 |
| Number of pieces: |
1 |
The Letov Š-5 aircraft is a single-engine two-seat biplane that was developed as a reconnaissance aircraft. The first flight of the machine took place in 1923. The construction was carried out by Alois Šmolík .
At least one aircraft of this type was manufactured and delivered to the Czechoslovak Army .
Military use
Technical specifications
| Parameter | Data |
|---|---|
| crew | 2 |
| length | 8.30 m |
| span | 12.70 m |
| height | 2.62 m |
| Wing area | 35.9 m² |
| Wing loading | 40.3 kg / m² |
| Empty mass | 955 kg |
| Max. Takeoff mass | 1447 kg |
| Cruising speed | 152 km / h |
| Top speed | 195 km / h |
| Rise time | 18 min at 3000 m altitude |
| Service ceiling | 5000 m |
| Range | 614 km |
| Engines | 1 × 6-cylinder in-line engine Breitfeld & Danek Hiero L with 169 kW (230 PS) |
| Armament | ? |
See also
literature
- Václav Němeček: Československá letadla. Naše Vojsko, Prague 1968.
Web links
- LETOV Š-5 on vinar.cz (Czech)