Letov Š-16
From Wikipedia, the free encyclopedia
| Letov Š-16 | |
|---|---|
| Type | er |
| Manufacturer | Letov Kbely |
| Designed by | Šmolík |
| Maiden flight | 1926 |
| Primary user | Czechoslovakian Air Force |
The Letov Š-16 was a Czechoslovak single-engined, two-seat biplane bomber. It was designed by Alois Šmolík at Letov Kbely. Š-16 first flew in 1926.
[edit] Variants
- S-16 : Two-seat bomber, reconnaissance biplane.
- S-16L : Export version for Latvia.
- S-16T : Export version for Turkey.
- S-16V : Seaplane version for Yugoslavia. One built.
[edit] Specifications (Š-16)
Data from[citation needed]
General characteristics
- Crew: 2
- Length: 10.22 m (33 ft 6 in)
- Wingspan: 15.30 m (50 ft 2 in)
- Height: ()
- Empty weight: 1,400 kg (3,080 lb)
- Powerplant: 1× Lorraine Dietrich inline engine, 331 kW (450 hp)
Performance
- Maximum speed: 230 km/h (124 kt, 142 mph)
- Service ceiling 6,500 m (21,320 ft)
Armament
- 1x fixed machine gun
- 1x twin machine gun on swiwel mount
[edit] See also
|
||||||||||||||
