IVL C.VI.25 was a Finnish fighter aircraft designed by IVL. It was a further development of the IVL C.24.
The aircraft made its maiden flight on June 11, 1925. The aircraft was wrecked after a forced landing, due to engine trouble, on December 17, 1925.
The aircraft was under-powered, like its predecessor, and it was not considered possible to further develop the aircraft.
Operators
Specifications (C.VI.25)
Data from Thulinista Hornetiin – 75 vuotta Suomen ilmavoimien lentokoneita[1]
General characteristics
- Crew: 1
- Length: 6.9 m (22 ft 8 in)
- Wingspan: 9.5 m (31 ft 2 in)
- Max takeoff weight: 843 kg (1,858 lb)
- Powerplant: 1 × Siemens-Halske Sh.IIIA air-cooled geared rotary piston engine, 119 kW (160 hp)
- Propellers: 4-bladed wooden fixed-pitch propeller
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
See also
Related lists
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