Speedy Mouse
Role Ultralight aircraft
National origin Germany
Manufacturer Ultra-Leicht Flugtechnik
Status In production (2012)
Developed from FMP Qualt 200

The Ultra-Leicht Flugtechnik Speedy Mouse is a German ultralight aircraft, designed and produced by Ultra-Leicht Flugtechnik of Braunschweig. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2]

Design and development

The aircraft was derived from the FMP Qualt 200 and designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit under a front-hinged bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.[1][2]

The Speedy Mouse is made from mixed wood and epoxy construction. Its 9.2 m (30.2 ft) span wing employs a GA-W 1 airfoil and has an area of 10.5 m2 (113 sq ft). The wings can be quickly removed for ground transport or storage. The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant. The aircraft was designed for aero-towing gliders.[1][2][3]

Specifications (Speedy Mouse)

Data from Bayerl and Ultra-Leicht Flugtechnik[1][3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 5.90 m (19 ft 4 in)
  • Wingspan: 9.2 m (30 ft 2 in)
  • Height: 1.70 m (5 ft 7 in)
  • Wing area: 10.5 m2 (113 sq ft)
  • Airfoil: GA-W 1
  • Empty weight: 298 kg (657 lb)
  • Gross weight: 450 kg (992 lb)
  • Fuel capacity: 47 litres (10 imp gal; 12 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 3-bladed composite

Performance

  • Maximum speed: 230 km/h (140 mph, 120 kn)
  • Cruise speed: 185 km/h (115 mph, 100 kn)
  • Stall speed: 64 km/h (40 mph, 35 kn)
  • Range: 650 km (400 mi, 350 nmi)
  • Rate of climb: 7 m/s (1,400 ft/min)
  • Wing loading: 42.9 kg/m2 (8.8 lb/sq ft)

References

  1. 1 2 3 4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 83. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 86. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  3. 1 2 Stephan Becker. "Ultra-Leicht Flugtechnik". Beier-bs.de. Retrieved 10 September 2012.
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