Windward Performance DuckHawk

DuckHawk
Role Glider
National origin United States
Manufacturer Windward Performance
Status In production (2012)
Unit cost
US$105,000 (2011)
Developed from Windward Performance SparrowHawk

The Windward Performance DuckHawk is an American mid-wing, single-seat, 15-metre class glider, designed and produced by Windward Performance of Bend, Oregon.[1]

Design and development

The DuckHawk is a development of the Windward Performance SparrowHawk and is intended as a higher performance glider than its predecessor, with very high structural limits and Vne. The DuckHawk has less than 10% parts commonality with the SparrowHawk. It features a cantilever wing, a single-seat enclosed cockpit under a bubble canopy and retractable monowheel gear.[1][2]

The aircraft is made from preimpregnated carbon fiber. Its 15 m (49.2 ft) span wing employs a Greg Cole-designed airfoil, has an area of 80 sq ft (7.4 m2) and an aspect ratio of 30:1.[1][3]

Operational history

By December 2012 two examples had been registered in the United States with the Federal Aviation Administration, the first in 2011 and the second in 2012.[4]

Variants

DuckHawk E
Electric motorglider version, first registered with the FAA in 2011.[5]
DuckHawk V (Veloce)
Base model with an empty weight of 390 lb (180 kg), a maximum gross weight of 960 lb (440 kg) and load limits of +7/-5g.[2][6]
DuckHawk SV (Super Veloce)
Model with a 64% thicker spar, thicker fuselage, an empty weight of435 lb (197 kg), a maximum gross weight of 960 lb (440 kg) and load limits of +11/-9g.[2][6]
DuckHawk VNX
Model with thicker wing skins, an empty weight of 455 lb (206 kg), a maximum gross weight of 1,150 lb (520 kg), maximum speed of 225 kn (417 km/h) and load limits of +11/-9g.[2][6]

Specifications (DuckHawk VNX)

Data from Bayerl and Windward Performance[1][2][6]

General characteristics

Performance

See also


Related lists

References

  1. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 138. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 1 2 3 4 5 Windward Performance (2011). "DuckHawk features". Retrieved 25 August 2015.
  3. Windward Performance (2011). "DuckHawk". Retrieved 4 December 2012.
  4. Federal Aviation Administration (4 December 2012). "Make / Model Inquiry Results". Retrieved 4 December 2012.
  5. Federal Aviation Administration (4 December 2012). "N-Number Inquiry Results - N10WP". Retrieved 4 December 2012.
  6. 1 2 3 4 Windward Performance (2011). "Specs" (PDF). Retrieved 25 August 2015.

External links

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