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.