CAPELLA JAVELIN

 

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