Thulin L
| Type L | |
|---|---|
| Role | Reconnaissance aircraft | 
| Manufacturer | AB Thulinverken | 
| Designer | Enoch Thulin | 
| First flight | April 1916 | 
| Primary user | Swedish Air Force | 
| Number built | 5 | 
| Variants | Thulin LA | 
The Thulin L was a Swedish reconnaissance plane built in the late 1910s.
Design and development
The Thulin L was a two-seat biplane derived from the unsuccessful Thulin E. It differed from the latter in that the wing surface was increased and the float location was made easier. Four production Thulin L floatplanes were ordered July 4, 1916, and they were delivered from November 1916 to March 1917.
Specifications
Data from [1]
General characteristics
- Crew: 2
 - Length: 7.5 m (24 ft 7 in)
 - Wingspan: 11.6 m (38 ft 1 in)
 - Height: 3.52 m (11 ft 7 in)
 - Wing area: 36.5 m2 (393 sq ft)
 - Gross weight: 965 kg (2,127 lb)
 - Powerplant: 1 × Thulin A 9-cylinder air-cooled rotary piston engine, 67 kW (90 hp)
 
Performance
- Maximum speed: 120 km/h (75 mph, 65 kn)
 - Cruise speed: 95 km/h (59 mph, 51 kn)
 
See also
Related lists
References
- ^ "Thulin L". www.airwar.ru (in Russian). Retrieved 1 March 2019.