2023 Trendak Taurus

TECHNICAL DATA RST Cockpit Dimensions 1,25 m (49.21 in) Overall width 2,2 m (86.62 in) Length (airframe) 4,9 m (192.91 in) Height 2,8 m (110.24 in) Wheel Diameter 350 mm (13.78 in) Empty weight (depending on the configuration) 285 kg-350kg Max Payload 330 kg (727,5 lb) Max Take-off Weight (1) 600 kg (1234,6 lb) Powerplant AAT 912 (RSTi) Configuration 4 flat cylinders 4T Power 135hp / 140hp Starter Electric Intake Turbo + Injection System Static Thrust 280 kg (617.29 lb) Fuel Capacity 80 liters Proppeler Kaspar KA-2/3 Diameter 1740 mm (68.5in) Rotor Trendak Son aluminium Diameter 8,4 m (27 ft)/ 8,6 m (28 ft)/ 8,8 m (29 ft) Rotor Surface Area 55.38 m2 / 58 m2 / 60 m2 PERFORMANCE Minimum speed 50 km/h (31 mph) Cruise speed (75%) 140 km/h (87 mph) Maximum speed 170 km/h (109 mph) Vne 210 km/h (130 mph) Rate of climb 4,1 m/s (800 ft/min) Glide Ratio 3/1 Minimum distance T.O. (4) 150 m (492 ft) Minimum distance landing 15 m (48 ft) Operational ceiling 4000 m (13120 ft) Cruise fuel consumption 20 – 25 l/h Endurance in hours 3,5 h Theoretical maximum range 450 km (280 miles) * The data provided is for illustrative purposes only. The above offer is for information purposes only.