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SZD-27

Polish two-seat glider, 1965 From Wikipedia, the free encyclopedia

The SZD-27 Kormoran (Cormorant) (Szybowcowy Zakład Doświadczalny - Glider experimental department) was a two-seat glider designed in Poland from 1961.

TypeGlider
National origin
Poland
Designer
Eng. Józef Niespał
Numberbuilt2
Quick facts General information, Type ...
SZD-27 Kormoran
General information
TypeGlider
National origin
Poland
Designer
Eng. Józef Niespał
Number built2
History
First flight2 January 1965
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Development

The SZD-27 Kormoran was designed to cater for the large demand from Polish aeroclubs for two-seat training machines, for basic training, advanced training and aerobatics. The SZD-27 was the first and only glider designed by SZD to be built entirely of metal, with light alloy skins, formers, ribs, frames etc., with steel high strength detail parts. The undercarriage comprises a semi-recessed mainwheel with skids under the nose and at the tail. Only two were built which both survive, one in the Kraków museum store-house and one restored to airworthiness in the 1990s by a private owner. The SZD-27 Kormoran resembles a cross between a LET L-13 Blaník and an SZD-24 Foka.[1]

Specifications (SZD-27 Kormoran)

SZD-27 Kormoran

Data from [1]

General characteristics

  • Crew: 2
  • Length: 8 m (26 ft 3 in)
  • Wingspan: 17 m (55 ft 9 in)
  • Height: 1.1 m (3 ft 7 in)
  • Wing area: 19.3 m2 (208 sq ft)
  • Aspect ratio: 15
  • Empty weight: 289 kg (637 lb)
  • Max takeoff weight: 517 kg (1,140 lb)

Performance

  • Stall speed: 64 km/h (40 mph, 35 kn)
  • Never exceed speed: 235 km/h (146 mph, 127 kn)
  • Maximum glide ratio: 28.1 at 93 km/h (58 mph; 50 kn)
  • Rate of sink: 0.8 m/s (160 ft/min) at 80 km/h (50 mph; 43 kn)
  • Lift-to-drag: +8 / -4 g
  • Wing loading: 28.6 kg/m2 (5.9 lb/sq ft)

See also

Aircraft of comparable role, configuration, and era

References

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