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  Aircraft History, Specification and Information
Aerospool WT9 Dynamic
Aerospool Dynamic WT9 - D-MIJH
Aerospool WT9 Dynamic - D-MIJH (c/n DY319/2009)
Photo taken Sep. 15, 2011 @ Winzeln-Schramberg Airport, Baden-Württemberg - Germany (EDTW)
Photo © Marcel Siegenthaler

The Aerospool WT9 Dynamic is a Slovakian ultralight and light-sport aircraft, designed produced by Aerospool of Prievidza. The aircraft is supplied as a complete ready-to-fly-aircraft.

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules, US light-sport aircraft rules and UK BCAR Section "S". It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed or retractable tricycle landing gear and a single engine in tractor configuration.

The aircraft is made with carbon fibre sandwich construction. Standard engines available are the 100 hp (75 kW) Rotax 912ULS, the Rotax 912iS and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. A glider towhook is optional equipment.

Specifications (Aerospool WT9 Dynamic)

General characteristics
Crew: one
Capacity: one passenger
Length: 6.40 m (21 ft 0 in)
Wingspan: 9.0 m (29 ft 6 in)
Height: 2.00 m (6 ft 7 in)
Wing area: 10.35 m2 (111.4 sq ft)
Empty weight: 264 kg (582 lb)
Gross weight: 450 kg (992 lb)
Fuel capacity: 75 litres (16 imp gal; 20 US gal)
Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)

Maximum speed: 220 km/h (137 mph; 119 kn)
Cruising speed: 200 km/h (124 mph; 108 kn)
Stall speed: 65 km/h (40 mph; 35 kn)
Never exceed speed: 280 km/h (174 mph; 151 kn)
Range: 1,600 km (994 mi; 864 nmi)
Rate of climb: 7 m/s (1,400 ft/min)

Last updated May 14, 2012
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Aerospool WT9 Dynamic".
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