PZL Bielsko SZD-52: Difference between revisions
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m Robot - Moving category PZL gliders to PZL aircraft per CFD at Wikipedia:Categories for discussion/Log/2010 November 24. |
m Robot - Moving category Polish sailplanes 1980-1989 to Category:Polish sailplanes 1980–1989 per CFD at Wikipedia:Categories for discussion/Log/2011 September 20. |
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[[Category:PZL aircraft|SZD52]] |
[[Category:PZL aircraft|SZD52]] |
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Revision as of 04:13, 4 October 2011
| SZD-52 | |
|---|---|
| Role | Standard-class sailplane |
| National origin | Poland |
| Manufacturer | PZL Bielsko |
| First flight | 28 February 1981 |
The PZL Bielsko SZD-52 is a Polish single-seat standard class sailplane produced by PZL Bielsko.[1] It is a cantilever high-wing monoplane with a T-tail and has a retractable main landing gear and a fixed tailwheel.[1] The wings have integral water ballast tanks.[1]
Variants
- SZD-52 Jantar 15
- SZD-52-1 Jantar 15SI
- SZD-52-2 Krokus
- SZD-52-3 Krokus S
- SZD-52-4 Krokus C
Sepcifications (SZD52-3)
Data from [1]
General characteristics
- Crew: 1
- Length: 7 m (23 ft 0 in)
- Wingspan: 15 m (49 ft 3 in)
- Height: 1.55 m (5 ft 1 in)
- Wing area: 10.3 m2 (111 sq ft)
- Aspect ratio: 21.8
- Empty weight: 248 kg (547 lb)
- Gross weight: 370 kg (816 lb) without water ballast
Performance
- Never exceed speed: 255 km/h (158 mph, 138 kn)
See also
Related lists
References
Notes
- ^ a b c d "Type Certificate Data Sheet A-441 SZD-52 Krokus" (PDF). European Aviation Safety Agency. 14 February 2007. Retrieved 2009-12-26.