IVL C.VI.25
| IVL C.VI.25 | |
|---|---|
.jpg)
|
|
| Type: | Fighter plane |
| Design country: | |
| Manufacturer: | |
| First flight: |
June 11, 1925 |
| Number of pieces: |
1 |
The IVL C.VI.25 was a fighter aircraft made by the Finnish manufacturer Ilmailuvoimien Lentokonetehdas .
History and construction
The IVL C.VI.25 is a further development of the IVL C.24 . The aircraft was designed by Kurt Berger as a high- wing aircraft with an open cockpit and tail wheel landing gear. It was driven by a Siemens-Halske-Sh.IIIA - radial engine . The aircraft completed its first flight on June 11, 1925. However, it was destroyed on December 17, 1925 after an emergency landing due to engine damage.
Military use
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| length | 6.9 m |
| span | 9.5 m |
| height | 2.93 m |
| Wing area | 16.3 m² |
| Empty mass | 655 kg |
| Max. Takeoff mass | 843 kg |
| Top speed | 210 km / h |
| Service ceiling | 6500 m |
| Engine | 1 × Siemens-Halske-Sh.IIIA star engine with 119 kW (162 PS) |
| Armament | 2 × MG Vickers 7.7 mm |
See also
literature
- Timo Heinonen: Thulinista Hornetiin. 75 vuotta Suomen ilmavoimien lentokoneita. Keski-Suomen ilmailumuseon julkaisuja 3, Jyväskylä 1992, ISBN 951-95688-2-4 .
Web links
Commons : IVL C.25 - Collection of Images, Videos and Audio Files
