CURTI AEROSPACE DIVISION ZEFHIR

CURTI AEROSPACE DIVISION

ZEFHIR

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Maximum takeoff weight: 600/650 kg Control system: FADEC Capacity: 2 passengers Speed: 102 knots Range: 318 nautical miles Engine type: Turbine Performance Maximum takeoff weight: 600 kg (1,322 lbs) Cruise speed: 161 km/h (87 kts) Maximum level speed: 185 km/h (100 kts) Never exceed speed VNE (sea level): 189 km/h (102 kts) Hovering ceiling OGE (600 kg): 4,000 m (13,100 ft) Best Endurance: 2h 21min @78 km/h (42 kts) (+10 min reserve) Range 182 km (98nm) in 150 ltr tank configuration Maximum range: 318 km (172 nm) @185 km/h (+10 min reserve) (100 kts), Endurance 1h 43 min in 150 ltr tank configuration Maximum range: 638 km (344 nm) (+10 min reserve) @185 km/h (100 kts) in 287 ltr tank configuration Transmission Primary transmission: Direct Main gearbox: Bevel spiral gear with a reduction ratio of 12/49 Tail gearbox: Bevel spiral gear with a multiplication ratio of 19/15 Features: Seating: 2 crashworthy seats (according to CS-27) Cabin width: 1.34 m (4.4 ft) Maximum luggage capacity: 320 dm³ / (11.3 ft³) Standard fuel capacity: 150 ltr / (40 Usgal) Maximum auxiliary fuel capacity: 137 ltr / (36 Usgal) Approved fuel type: JET A, JET A-1, JET B, according to DERD 2494. TS-1, T2, RT according to GOST 10227 Main Rotor Type: Teetering Number of blades: 2 Diameter: 7.6 m (24.9 ft) Chord: 195 mm (7.7 in) Speed: 528 rpm Tail Rotor Type: Teetering Number of blades: 2 Diameter: 1.2 m (3.9 ft) Chord: 120 mm (4.7 in) Speed: 3,062 rpm Engine Engine type: PBS TS100 Turboshaft Engine (gas generator turbine & power turbine) Maximum continuous power: 105 kW (141 shp) Output speed: 2,158 rpm Parachute Minimum deployment altitude: 150 m (450 ft)