DWLKK PW-2D

DWLKK PW-2D
PW-2
Role Glider
National origin Poland
Manufacturer DWLKK
Designer Warsaw University of Technology
Introduction early 1990s
Status Production completed

The Politechnika Warszawsks PW-2 (English: Warsaw Polytechnic PD-2D), also called the PW-2 Gapa and produced as the DWLKK PW-2D, is a Polish lightweight high-wing, strut-braced single-seat, glider that was designed and built at the Warsaw University of Technology and also produced by DWLKK in the early 1990s.[1][2]

Contents

Design and development

The PW-2 was designed as a lightweight glider of modest performance with an open cockpit. The aircraft was intended to be produced as both a completed aircraft and as a kit for amateur construction.[1]

The aircraft is made from composite material, with its control surfaces covered in doped aircraft fabric covering. Its 11.0 m (36.1 ft) span wing employs an American-designed NACA 4415 airfoil. The maximum glide ratio is 16:1 at 69 km/h (43 mph)[1][3]

Operational history

In August 2011 five PW-2Ds were registered in the United States with the Federal Aviation Administration. All were in the Experimental - Exhibition/Racing category and all produced in 1992 or 1993.[2]

Specifications (PW-2D)

Data from Sailplane Directory[1]

General characteristics

  • Crew: one
  • Wingspan: 11.0 m (36 ft 1 in)
  • Wing area: 12.7 m2 (137 sq ft)
  • Aspect ratio: 9.52:1
  • Airfoil: NACA 4415
  • Empty weight: 110 kg (243 lb)
  • Gross weight: 220 kg (485 lb)

Performance

  • Maximum glide ratio: 16:1 at 69 km/h (43 mph)
  • Rate of sink: 1.1 m/s (220 ft/min)
  • Wing loading: 17.32 kg/m² (3.55 lb/sq ft)

See also

Related lists

References

External links


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