IVL C.VI.25
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| C.VI.25 | |
|---|---|
| Type | Fighter aircraft |
| Manufacturer | IVL |
| Maiden flight | June 11 1925 |
| Status | Destroyed on December 17, 1925 |
| Primary user | Finnish Air Force |
| Number built | 1 |
| Developed from | IVL C.24 |
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.
Contents |
[edit] Specifications (C.VI.25)
Data from Thulinista Hornettiin
General characteristics
- Crew: 1
- Length: 6.9 m (22 ft 6 in)
- Wingspan: 9.5 m (31 ft 2 in)
- Height: m (ft in)
- Wing area: m² (ft²)
- Empty weight: kg (lb)
- Loaded weight: kg (lb)
- Useful load: kg (kg)
- Max takeoff weight: 843 kg (1,854 lb)
- Powerplant: 1× Siemens-Halske Sh.IIIA radial engine, 119 kW (160 hp)
Performance
- Never exceed speed: km/h (knots, mph)
- Maximum speed: 210 km/h (113 knots, 130 mph)
- Cruise speed: km/h (knots, mph)
- Stall speed: km/h (knots, mph)
- Range: km (nm, mi)
- Service ceiling m (ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
[edit] References
[edit] Sources
- Heinonen, Timo: Thulinista Hornetiin, Keski-Suomen ilmailumuseon julkaisuja 3, 1992. ISBN 951-95688-2-4.
[edit] See also
Related lists
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