Mi-2 HOPLITE
Specifications | |
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Country of Origin | Russia |
Builder | MIL / PZL Swidnik |
Date of Introduction | 1965 |
Role | Transport, cargo, reconnaissance, trainer, search and rescue, liaison, armed support |
Similar Aircraft | Hirundo A109, Mi-8 Hip |
Blades | Main rotor: 3 Tail rotor: 2 |
Rotor diameter | 47 ft, 6 in (14.6 m) |
Length |
rotors turning: 17.4 m / 57 ft fuselage: 11.9 m |
Height | 3.7 m |
Weight |
Maximum Gross: 3,700 kg Normal Takeoff: 3,550 kg Empty: 2,372 kg |
Engines | 2x 400-shp PZL GTD-350 (series III and IV) turboshaft |
Maximum speed | 220 km/h |
Cruising speed | 194 km/h |
Fuel |
Internal: 600 liters Internal Aux Tank: N/A External Fuel Tank: 238 liters ea. |
Range |
Maximum Load: 580 km Normal Load: 340 km With Aux Fuel: 790 km |
Ceiling |
Service: 4,000 meters Hover (out of ground effect): 1,000 meters Hover (in ground effect): 2,000 meters |
Vertical Climb Rate | 4.5 m/s |
Standard Payload |
Transports 6-8 troops or 700 kg internal cargo or 800 kg external load on 4x external hardpoints. |
Armament |
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AVIONICS |
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Survivability | Main and tail rotor blades electrically deiced. |
Crew | 1 (pilot) |
Cost | |
User Countries | Azerbaijan, Burma, Bulgaria, CIS, Cuba, Czech Republic, Georgia, Germany, Ghana, Hungary, Libya, Nicaragua, Poland, Slovakia, Syria, Ukraine |
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