History

Thulin K

The Thulin K was designed in 1916 by Dr. Thulin of the Swedish AB Thulinverken.
It was a single seat fighter.
The shoulder plane had a wooden construction and no flaps. It had a Thulin A rotary engine of 90 horsepower. This was derived from the French Gnome rotary engine.
Two examples were built for Swedish Flygvapnet and twelve examples for the Dutch Navy.

Also a two-seat version was built, in which the instructor and the pupil sat in tandem.
Three examples were built for the Dutch Navy.

Thulin LA

The Thulin LA, a biplane trainer, was designed in 1917 and was based on the earlier Thulin E and Thulin L. These were derived from the Albatros B.I

The Thulin LA had a custom fuselage, empennage and another engine.

Fifteen examples were built, of which ten of the Dutch Navy.

 

Technical information Thulin LA
Dimensions:
Length: 6,60 m Wingspan: 11,5 m
Height 3,4 Wing area: 36 m2
Weight:
Empty weight: - kg Max. Start weight - kg
Performance:
Max. Speed: 120 km/hr Climbing speed: - m/min
Range: - km Service ceiling: - m
Miscellaneous:
Engine type: One Thulin A rated 80 hp
Crew: Two men: one instructor plus one pupil
Armament: None

 

Technical information Thulin K (two seat)
Dimensions:
Length: 6,6 m Wingspan: 11,55 m
Height 2,83 m Wing area: - m2
Weight:
Empty weight: - kg Max. Start weight - kg
Performance:
Max. Speed: 135 km/hr Climbing speed: - m/min
Range: - km Service ceiling: - m
Miscellaneous:
Engine type: One Thulin A rated 80 hp
Crew: Two men: one instructor plus one pupil
Armament: None

 

Technical information Thulin K
Dimensions:
Length: 6,6 m Wingspan: 11,55 m
Height 2,83 m Wing area: - m2
Weight:
Empty weight: 522 kg Max. Start weight - kg
Performance:
Max. Speed: 135 km/hr Climbing speed: - m/min
Range: - km Service ceiling: - m
Miscellaneous:
Engine type: One Thulin A rated 80 hp
Crew: One aviator
Armament: Eventually one machine gun