Windward Performance DuckHawk
| DuckHawk | |
|---|---|
| General information | |
| Type | Glider |
| National origin | United States |
| Manufacturer | Windward Performance |
| Status | Production completed (2016) |
| History | |
| First flight | 2011 |
| Developed from | Windward Performance SparrowHawk |
The Windward Performance DuckHawk is an American mid-wing, single-seat, 15-metre class glider, that was designed and produced by Windward Performance of Bend, Oregon.[1] It first flew in 2011.[2]
Since 2016 the aircraft has been no longer advertised as available by the manufacturer.[3]
Design and development
[edit | edit source]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][4]
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][5]
Operational history
[edit | edit source]By December 2016 four examples had been registered in the United States with the Federal Aviation Administration, including three "V" models and one "E" model.[6]
Variants
[edit | edit source]- DuckHawk E
- Electric motorglider version, first example registered with the FAA in 2011.[7]
- 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. The first example was registered with the FAA in 2014 and three have been built.[4][6][8]
- DuckHawk SV (Super Veloce)
- Proposed model with a 64% thicker spar, thicker fuselage, an empty weight of 435 lb (197 kg), a maximum gross weight of 960 lb (440 kg) and load limits of +11/-9g. None completed.[4][6][8]
- DuckHawk VNX
- Proposed 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. None completed.[4][6][8]
Specifications (DuckHawk V)
[edit | edit source]Data from Bayerl and Windward Performance[1][4][8]
General characteristics
- Crew: one
- Length: 20.6 ft (6.3 m)
- Wingspan: 49.2 ft (15.0 m)
- Height: 3 ft 8 in (1.12 m)
- Wing area: 80 sq ft (7.4 m2)
- Aspect ratio: 30:1
- Airfoil: Greg Cole-designed
- Empty weight: 390 lb (177 kg)
- Gross weight: 960 lb (435 kg)
Performance
- Never exceed speed: 193 mph (311 km/h, 168 kn)
- g limits: +7/-5g
- Maximum glide ratio: 50:1
- Wing loading: 12 lb/sq ft (59 kg/m2)
See also
[edit | edit source]Related development
Related lists
References
[edit | edit source]- ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 138. WDLA UK, Lancaster UK, 2011. Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ a b c d e Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ a b c d Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
- ^ a b c d Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).