WATSON GW-1 WINDWAGON

 

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