Letov Š-6
Š-6 | |
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Role | Bomber |
National origin | Czechoslovakia |
Manufacturer | Letov |
First flight | 1923 |
Number built | 35 |
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The Letov Š-6 was a bomber aircraft produced in Czechoslovakia during the 1920s. Derived from the Š-2, it was a large biplane of conventional design. The wing cellule was an all-new design with a thicker profile, and while it had been intended to build them with a metal structure, wood was used instead due to shortages. Performance during testing was so promising that in 1924 an Š-6 was used to set a new altitude record with a 500 kg payload, and (on another occasion) a national endurance record of 10 hrs 32 min.
The Š-6 enjoyed a long career in Czechoslovakian service, remaining in use until 1934. One example was given a civil registration (L-BORA) and evaluated as an airliner for the Prague-Gothenburg route, but nothing came of this.
Specifications
General characteristics
- Crew: Two
- Length: 8.85 m (29 ft 0 in)
- Wingspan: 15.69 m (51 ft 6 in)
- Wing area: 43.0 m2 (462 ft2)
- Empty weight: 1,152 kg (2,534 lb)
- Gross weight: 2,008 kg (4,417 lb)
- Powerplant: 1 × Maybach Mb.IV, 190 kW (260 hp)
Performance
- Maximum speed: 186 km/h (116 mph)
- Range: 780 km (490 miles)
- Service ceiling: 6,250 m (20,500 ft)
- Rate of climb: 2.6 m/s (520 ft/min)
References
Wikimedia Commons has media related to Letov aircraft. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 573.
- Němeček, Václav (1968). Československá letadla. Prague: Naše Vojsko.
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