PZL Bielsko SZD-52: Difference between revisions
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| type=Standard-class [[Glider aircraft|sailplane]] |
| type=Standard-class [[Glider aircraft|sailplane]] |
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| national origin=[[Poland]] |
| national origin=[[Poland]] |
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| manufacturer=[[PZL Bielsko]] |
| manufacturer=[[Państwowe Zakłady Lotnicze|PZL Bielsko]] |
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| designer=Adam Kurbiel |
| designer=Adam Kurbiel |
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| first flight=28 February 1981 |
| first flight=28 February 1981 |
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{{external media |
{{external media |
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| width = 312px |
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| image1 = [https://www.flickr.com/photos/26267225@N03/7520970462 SZD-52-2 ''Krokus'' in flight]}} |
| image1 = [https://www.flickr.com/photos/26267225@N03/7520970462 SZD-52-2 ''Krokus'' in flight]}} |
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The '''PZL Bielsko SZD-52''' is a Polish single-seat standard class [[Glider aircraft|sailplane]] produced by [[PZL Bielsko]].<ref name="tcds" /> It is a cantilever high-wing [[monoplane]] with a T-tail and has a retractable main landing gear and a fixed tailwheel.<ref name="tcds" /> The wings have integral water ballast tanks.<ref name="tcds" /> |
The '''PZL Bielsko SZD-52''' is a Polish single-seat standard class [[Glider aircraft|sailplane]] produced by [[Państwowe Zakłady Lotnicze|PZL Bielsko]].<ref name="tcds" /> It is a cantilever high-wing [[monoplane]] with a T-tail and has a retractable main landing gear and a fixed tailwheel.<ref name="tcds" /> The wings have integral water ballast tanks.<ref name="tcds" /> |
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==Variants== |
==Variants== |
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[[Category:PZL aircraft|SZD52]] |
[[Category:PZL aircraft|SZD52]] |
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[[Category:1980s Polish sailplanes]] |
[[Category:1980s Polish sailplanes]] |
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[[Category:Aircraft first flown in 1981]] |
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[[Category:SZD aircraft]] |
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Latest revision as of 18:05, 3 December 2023
| SZD-52 | |
|---|---|
| Role | Standard-class sailplane |
| National origin | Poland |
| Manufacturer | PZL Bielsko |
| Designer | Adam Kurbiel |
| First flight | 28 February 1981 |
| Number built | 8 |
| External image | |
|---|---|
 SZD-52-2 Krokus in flight |
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[edit]
- SZD-52 Jantar 15
- SZD-52-1 Jantar 15SI
- SZD-52-2 Krokus
- SZD-52-3 Krokus S
- SZD-52-4 Krokus C
Specifications (SZD52-3)[edit]
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[edit]
Related lists
References[edit]
Notes[edit]
- ^ a b c d "Type Certificate Data Sheet A-441 SZD-52 Krokus" (PDF). European Aviation Safety Agency. 14 February 2007.