Specifications
Data from Yak-50 Flight Manual & Technical Description handbook
General characteristics
- Crew: one, pilot
- Length: 7.8 m (25 ft 7 in)
- Wingspan: 9.5 m (31 ft 2 in)
- Height: 3.2 m (10 ft 6 in)
- Wing area: 15.0 m² (161.5 ft²)
- Airfoil: Clark YH
- Empty weight: 750 kg (1653 lb)
- Max. takeoff weight: 910 kg (2006 lb)
- Powerplant: 1 × Vedeneyev M-14P, M-14PF or M-14R 9-cylinder air-cooled radial engine, 269/298/336 kW (360/400/450 hp)
Performance
- Never exceed speed: 450 km/h VNE (243 knots, 280 mph)
- Maximum speed: 400 km/h VA (216 knots, 249 mph)
- Cruise speed: 270 km/h VNO (146 knots, 168 mph)
- Stall speed: 100 km/h (54 knots, 62 mph)
- Range: 500 km (270 nm, 308 mi)
- Service ceiling: 4,000 m (13,123 ft)
- Rate of climb: 11.3 m/s sustained, 16.0 m/s initial (2,224 ft/min sustained, 3,145 ft/min initial)
- Wing loading: 60.7 kg/m² (12.43 lb/ft²)
- Power/mass: 0.295 kW/kg (0.179 hp/lb)
- G-loads: +9; -6 G dependent on tankage and smoke oil installation
- Take-off roll: 100 m (328 ft)
- Landing roll: 250 m (820 ft)
- Take-off speed: 130 km/h (81 mph, 70 kt)
- Landing speed: 110 km/h (68 mph, 59 kt)
Read more about this topic: Yakovlev Yak-50 (1975)