General characteristics

Crew: 3–4

Capacity:
26 troops (38 passengers) or 5 tonnes of payload or 4 stretchers (with sonar array removed) for Merlin HM1;

30 seated troops or 45 standing fully equipped combat troops, or 3,050 kg (6,724 lb) of internal payload, 5,520 kg (12,169 lb) of external payload, or 16 stretchers for AW101

Length: 19.53 m (64 ft 1 in) fuselage
Height: 6.62 m (21 ft 9 in)
Empty weight: 10,500 kg (23,149 lb)
Max takeoff weight: 14,600 kg (32,187 lb)
Powerplant: 3 × Rolls-Royce Turbomeca RTM322-01 turboshaft engines, 1,566 kW (2,100 hp) each (take-off power)
Main rotor diameter: 18.59 m (61 ft 0 in)
Main rotor area: 271.51 m2 (2,922.5 sq ft) root: RAE 9651 ; tip: RAE 9645/RAE 9634[188]
Performance

Cruise speed: 278 km/h (173 mph, 150 kn)
Never exceed speed: 309 km/h (192 mph, 167 kn)
Range: 1,389 km (863 mi, 750 nmi) [189]
Endurance: 5 hours
Service ceiling: 4,575 m (15,010 ft)
Armament

Bombs: 4× Sting Ray homing torpedoes or Mk 11 depth charges[190]
Avionics

Smiths Industries OMI 20 SEP dual-redundant digital automatic flight control system
Navigation systems:
BAE Systems LINS 300 ring laser gyro, Litton Italia LISA-4000 strapdown attitude and heading reference system
Radar:
Selex Galileo Blue Kestrel 5000 maritime surveillance radar
ECM
Racal Orange Reaper ESM
Sonar
Thomson Marconi Sonar AQS-903 acoustic processor
Active/passive sonobuoys
Thomson Sintra FLASH dipping sonar array

Specifications (Mil-171A2)

Data from Russian Helicopters

General characteristics

Crew: 3 (two pilots and one engineer)
Capacity: 24 troops / 12 stretchers / 4,000 kg (8,818 lb) cargo internally / 5,000 kg (11,023 lb) externally slung.
Length: 18.465 m (60 ft 7 in)
Height: 5.65 m (18 ft 6 in)
Empty weight: 7,489 kg (16,510 lb)
Gross weight: 11,100 kg (24,471 lb)
Max takeoff weight: 13,000 kg (28,660 lb) normal
13,500 kg (29,762 lb) with under-slung load
Powerplant: 2 × Klimov VK-2500PS-03 turboshaft engines, 1,800 kW (2,400 hp) each for take-off
2,000 kW (2,700 hp) emergency rating
Main rotor diameter: 21.25 m (69 ft 9 in)
Main rotor area: 354.7 m2 (3,818 sq ft) *Blade section: NACA 23012[230]
Performance

Maximum speed: 280 km/h (170 mph, 150 kn)
Cruise speed: 260 km/h (160 mph, 140 kn)
Range: 800 km (500 mi, 430 nmi)
Service ceiling: 6,000 m (20,000 ft) *Hover ceiling OGE: 4,000 m (13,123 ft)
Rate of climb: 8 m/s (1,600 ft/min)
Armament

Some variants such as Mi-8AMTSh and Mi-171Sh have disposable stores on six hardpoints, including rockets such as S-8 and gun pods such as UPK-23-250. Some variants such as Mi-171SH-HV and Mi-171SH-VN can be armed with anti-tank guided missiles such as Ataka and precision-guided munitions along with other armaments. Have one or two window-mounted machine guns such as the PK.

Zašto rabiš vrtolet (ruski)? Hrvatski je pun rusizama. Odvjetnik npr.

Zašto rabiš vrtolet (ruski)? Hrvatski je pun rusizama. Odvjetnik npr.