Mi-2 HOPLITE
| Specifications | |
|---|---|
| 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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