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Wega 180

From Wikipedia, the free encyclopedia

Wega 180
Role Amateur-built aircraft
National origin Brazil
Manufacturer Wega Aircraft
Introduction 2013
Status In production (2017)

The Wega 180 is a Brazilian amateur-built aircraft designed and produced by Wega Aircraft (Wega Industria Aeronautica) of Palhoça, Santa Catarina, introduced at the Sun 'n Fun airshow in 2013. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1]

Design and development

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The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from carbon fibre. Its 7.78 m (25.5 ft) span wing employs an NFL (1)-0215F airfoil at the wing root transitioning to a Wortmann FX-62-K-131 at the wing tip. The wing has an area of 9.06 m2 (97.5 sq ft) and mounts flaps. The wing is a separate structure and is attached to the fuselage with four bolts. The standard engines used are the 180 hp (134 kW) Superior XP-360 and the 180 hp (134 kW) Lycoming IO-360 four-stroke powerplants.[1]

Operational history

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Reviewers Roy Beisswenger and Marino Boric described the design in a 2015 review as "a modern, two-place, high-performance aircraft...[with] aerobatic features and claims a high 300 km/h (190-knot) cruise speed in a comfortable, ergonomic cabin...the aircraft's clean design, together with the retractable gear, helps Wega to reach a max airspeed of 350 km/h".[1]

Specifications (Wega 180)

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Data from Tacke and manufacturer[1][2]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.556 m (21 ft 6 in)
  • Wingspan: 7.86 m (25 ft 9 in)
  • Height: 2.315 m (7 ft 7 in)
  • Wing area: 9.06 m2 (97.5 sq ft)
  • Airfoil: Wing root: NFL (1)-0215F, wing tip: Wortmann FX-62-K-131
  • Empty weight: 550 kg (1,213 lb)
  • Gross weight: 910 kg (2,006 lb)
  • Fuel capacity: 214 litres (47 imp gal; 57 US gal)
  • Powerplant: 1 × Superior XP-360 four cylinder, air-cooled, four stroke aircraft engine, 130 kW (180 hp)
  • Propellers: 3-bladed constant speed propeller

Performance

  • Maximum speed: 352 km/h (219 mph, 190 kn)
  • Cruise speed: 306 km/h (190 mph, 165 kn)
  • Stall speed: 102 km/h (63 mph, 55 kn) flaps down
  • Range: 2,345 km (1,457 mi, 1,266 nmi)
  • Service ceiling: 5,000 m (16,000 ft)
  • g limits: +6/-4
  • Maximum glide ratio: 15:1
  • Rate of climb: 8 m/s (1,600 ft/min)
  • Wing loading: 100.0 kg/m2 (20.5 lb/sq ft)

See also

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References

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  1. ^ a b c d e Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 130. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ Wega Industria Aeronautica (2016). "Dados técnicos Wega 180". aerowega.com. Retrieved 26 May 2017.
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