Thulin L

From Wikipedia, the free encyclopedia
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[edit]

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[edit]

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[edit]

Related lists

References[edit]

  1. ^ "Thulin L". www.airwar.ru (in Russian). Retrieved 1 March 2019.