Thulin G
The Thulin G was a Swedish military reconnaissance aircraft built in the late 1910s.
Type G | |
---|---|
Role | Reconnaissance aircraft |
Manufacturer | AB Thulinverken |
First flight | 11 July 1917 |
Introduction | 1917 |
Retired | 1922 |
Primary user | Swedish Navy |
Number built | 7 |
Design and development
The Thulin G was a two-seat biplane of conventional configuration derived from the Albatros B.II that seated the observer and the pilot in separate cockpits in tandem. The upper wing was supported by 12 struts from the underwing and 4 supports from the aircraft body. The row motor was mounted in the aircraft's nose where it ran a wooden propeller . The exhaust gases from the engine were led via a manifold which ended at the upper side of the overhead. The pilot was sitting in the front cockpit which was placed under the wing while the scooter was sitting in a cockpit behind the wings to allow good visibility to the sides. The Type G used floats for takeoff and landing on water.
Operational history
Five Type G and two Type GA aircraft were built for the Swedish naval air force, serving from 1917-1922. All but two aircraft were lost in accidents or destroyed in hangar fires.
Variants
- Thulin G
- powered by a Benz Bz.III engine
- Thulin GA
- powered by Curtiss engine
Specifications (Type G)
Data from [1]
General characteristics
- Crew: 2
- Length: 9.4 m (30 ft 10 in)
- Wingspan: 17.2 m (56 ft 5 in)
- Empty weight: 1,538 kg (3,391 lb)
- Powerplant: 1 × Benz Bz.III 6-cylinder water-cooled in-line piston engine, 110 kW (150 hp)
Performance
- Maximum speed: 118 km/h (73 mph, 64 kn)
References
- "Thulin G". www.airwar.ru (in Russian). Retrieved 1 March 2019.