BRAND and MODEL
WATSON GW-1 WINDWAGON
TYPE
Single-seat light sporting monoplane
ORIGIN
United States of America
ENGINE
One 28 kw (37 hp) two-cylinder horizontally-opposed air-cooled conversion of a Volkswagen four-cylinder engine
SPECIFICATIONS
Wingspan: 5.48 m (18 ft)
Length: 4.05 m (13 ft 3 in)
Height: 1.21 m (4 ft)
Wing area: 5.85 m² (63 sq ft)
Max speed: 235 km/h (140 mph)Max cruising speed: 185 km/h (115 mph)
Cruising speed: 161 km/h (100 mph)
Stalling speed: 61 km/h (38 mph)
Take-off roll: 76 m (250 ft)
Landing roll: 76 m (250 ft)
Service ceiling: 3,658 m (12,000 ft)
Range: 402 km (250 miles)
Fuel capacity: 15 litres (3.3 Imp gals)
Empty weight: 124 kg (273 lb)
Useful load: 95 kg (210 lb)
Loaded weight: 220 kg (486 lb)
PHOTO
Airliners.net:Source of phothograph
