BRAND and MODEL
HARMON ROCKET II
TYPE
Two-seat sport monoplane
ORIGIN
United States of America
ENGINE
One (250 hp) Lycoming IO-540-c4b5 six-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 6.67 m (21 ft 10 in)
Length: 6.55 m (21 ft 6 in)
Height: 1.67 m (5 ft 6 in)
Wing area: 10.12 m² (109 sq ft)
Never exceed speed: 443 km/h (275 mph)
Cruising speed at 75% power: 370 km/h (230 mph)
Economical cruising speed at 55% power: 346 km/h (215 mph)
Rate of climb: 945 m/min (3,100 ft/min)
Stalling speed: 89 km/h (55 mph)
Fuel capacity: 159 litres (35 Imp gals)
Endurance: 3 hrs
Empty weight: 516 kg (1,138 lb)
Useful load: 292 kg (643 lb)
Loaded weight: 907 kg (2,000 lb)
PHOTO
abpic.co.uk:Source of phothograph
