BRAND and MODEL
CAPELLA JAVELIN
TYPE
Single or two-seat ultralight aircraft
ORIGIN
United States of America
ENGINE
One 21 kw (28 hp) at 6,100 rpm Rotax 277 single-cylinder, two-stroke, air-cooled engine with a displacement of 2687 cc, weighing 29 kg (65 lb)
SPECIFICATIONS
Wingspan: 8.53 m (28 ft)
Length: 5.49 m (18 ft)
Height: 1.83 m (6 ft)
Wing area: 10.04 m² (112 sq ft)
Max speed: 101 km/h (63 mph)
Cruising speed: 97 km/h (60 mph)
Stalling speed: 42 km/h (26 mph)
Service ceiling: 3,810 m (12,500 ft)
Rate of climb: 122 m/min (400 ft/min)
Fuel capacity: 19 litres (4.17 Imp gals)
Range: 193 km (120 miles)
Take-off run: 23 m (75 ft)
Landing run: 30 m (100 ft)
Empty weight: 109 kg (240 lb)
Useful load: 138 kg (305 lb)
Loaded weight: 261 kg (575 lb)
PHOTO
ultraligero.net:Source of phothograph
