SZD-45 Ogar
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(Redirected from PZL Bielsko SZD-45)
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| Type designation | SZD-45A SZD-45-2 "Ogar F" |
| Competition class | Two Seater |
| Number built | 65 |
The SZD-45 Ogar is a T-tailed cantilever high wing monoplane of wooden, aluminium and fibreglass construction designed in Poland. The prototype of this self-launching motorglider SP-0001 first flew on the 29 May 1973. With soaring capability and staggered side-by-side two-place seating. There were 64 examples constructed excluding the prototype with 41 of these being exported.
It has a Hoffmann twin-bladed pusher propeller. The landing gear is semi-retractable. The U.S. import is powered with the dual ignition, turbocharged, Revmaster engine. The "Ogar" is certified for simple aerobatics
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[edit] Specifications
Data from[citation needed]
General characteristics
- Crew: 2
- Length: 7.95 m ()
- Wingspan: 17.6 m ()
- Height: 1.51 m ()
- Wing area: 19.10 m² ()
- Aspect ratio: 16.2
- Empty weight: 470 kg ()
- Max. takeoff weight: 700 kg ()
- Powerplant: × Limbach SL-1700EC 1, 68 hp () each
Performance
- Maximum speed: 225 km/h
- Cruise speed: 165 km/h (89 kts) in rought air
- Stall speed: 78 km/h (42 knots)
- sink rate: 1.10 m/s () minimum at 85 km/h
- Wing loading: 36,6 kg/m² ()
[edit] Notes
[edit] References
[edit] External links
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