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)