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Mi-2 (Hoplite) Russian Light Utility Helicopter

Mi-2

Utility Helicopter
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Basic Information
Name
Mi-2 (Hoplite) Russian Light Utility Helicopter
Designation
Mi-2
Alternate Designation
Mi-2; NATO: Hoplite
Equipment Type
Utility Helicopter
Manufacturer
Mil
Date of Introduction
1965
Description

The Mil Mi-2 (NATO reporting name Hoplite) is a small, lightly armed turbine-powered transport helicopter that could also provide close air support when armed with 57 mm rockets and a 23 mm cannon. The MI-2 can conduct reconnaissance, resupply guerrillas, and provide close air support with 57mm rockets. It can also have a smoke generator mounted to provide a wide area smoke screen in front of units, screening their movements. Additional missions include; direct air support, antitank, armed reconnaissance, transport, medevac, airborne command post, minelaying, and training. Although the Mi-2 Hoplite was developed by the Mil bureau in the former Soviet Union, the aircraft was produced exclusively in Poland by the PZL Swidnik aircraft factory. Several thousand of these aircraft were built and they remained in production until 1985. The Hoplite has been one of the most widely produced helicopter designs. The three-blade main rotor is mounted on top of a large hump above the body's midsection. Two turboshaft engines are mounted side-by-side on top of the cabin, forming a hump, with round air intakes above the cockpit and oval exhausts on the sides of the engines. The small, bus-like fuselage with fixed landing gear features a stepped-up cockpit and rounded nose, and a tadpole-shaped body when viewed from the bottom. The tapered tail boom has small, unequally tapered flats and a thin, swept-back fin with a rotor on the right.

Air & Air Defense Specifications
Crew 1
Engine Turboshaft (400 hp)
Max Speed 210.0 km/h
Range 440.0 km
Variants
V-2V Armament prototype.
Mi-2 Platan Aerial minelayer version.
Mi-2B Upgraded export version for the Middle East, fitted with improved systems and navigational aids.
Mi-2Ch Chekla Chemical reconnaissance / smokescreen layer version.
Mi-2D Przetacznik Aerial command post equipped with R-111 radio.
Mi-2FM Survey version.
Mi-2P Passenger / cargo version, with accommodation for 6 passengers.
Mi-2R Agricultural version.
Mi-2RL Land rescue/ambulance version.
Mi-2RM Sea rescue version equipped with electric winch for two people and dropped rafts.
Mi-2Ro Reconnaissance version equipped with cameras.
UMi-2Ro Reconnaissance trainer version.
Mi-2MSB-V or MSB-2MO Modernized by Motor Sich for Ukrainian Air Force., Original engine replaced with AI-450M 465 HP engine, armed with Rocket and machine gun pods, IR-jamming system and flares dispenser for defense against MANPADS.
Mi-2MSB or MSB-2 Nadia ('Hope') Modernized by Motor Sich to passenger-transport version for the civil aviation.
Mi-3 Planned Mi-2 derivative that lacked suitable engines for the program to continue.
Mi-2 Plus Upgraded Mi-2 with uprated GTD-350W2 engines, all-composite rotor blades, new avionics and other modifications.
Mi-2URP-G Gniewosz ('Smooth snake') Mi-2URP with additional 4x AA missiles Strzała-2 (Strela 2) in two Gad rocket launchers.
Mi-2URP Salamandra ('Salamander') Gunship and anti-tank variant, armed with 23mm NS-23 gun, optional window-mounted 7,62mm PK machine gun, and 4x AT-3 Sagger (9M14M Malutka) wire-guided missiles on external weapons racks and 4x additional missiles in the cargo compartment.
Mi-2URN Żmija ('Viper') Armed reconnaissance variant armed with a fixed 23mm NS-23 gun and two 16x57mm S-5 unguided rocket pods Mars-2. Optional 7,62mm PK machine gun window-mounted.
Mi-2US Armed version fitted with a fixed 23mm NS-23 cannon, 4 x 7,62mm PKT machine gun pods and optional cabin PK machine gun.
Mi-2U Dual-control training version.
System
Alternative Designation Mi-2; NATO: Hoplite
Type Light Utility Helicopter
Manufacturer Mil Moscow Helicopter Plant
Primary Function Its military roles include anti-tank, liaison, air ambulance, training and scout. The Hoplite has been one of the most widely produced helicopter designs
In Service 1965-Present
Crew 1 ea
Cargo Capacity 8 passengers / 700 kg internal cargo / 800 kg external cargo
Blades, Main Rotor 3 ea
Blades, Tail Rotor 2 ea
Day/Night Capable The Mi-2 is primarily a daylight only aircraft
All Weather Capable INA
Takeoff or Landing Limitations INA
Number of Hard Points INA
Landing Gear A fixed tricycle gear has the main wheels extend on a tripod of struts from the lower rear of the cabin.
Tail Skid A fixed tail skid is fitted to the tail boom below the horizontal stabilizer.
Note The cabin can be reconfigured to take cargo, four litters and a medical attendant, or two sitting casualties and two litters.
Dimensions
Length 11.1 m
Height 3.75 m
Main Rotor Diameter 14.50 m
Disc Area 166.4 sq m
Weight, Empty 2,365 kg
Weight, Maximum Takeoff 3,550 kg
Weight, Maximum Internal Payload 700 kg
Weight, Maximum Payload, Total 800 kg
Automotive
Engine Name 2 x Isotov GTD-350
Engine Type Turboshaft
Engine Power 400 hp each
Speed, Never Exceed 210 km/h
Speed, Cruise 200 km/h
Speed, Maximum Range 190 km/h
Range, Maximum Payload 170 km
Ragne, Maximum Internal Fuel 440 km
Range, Maximum Internal and Auxiliary Fuel, No Reserves 797 km
Climb Rate 270 m/min
Time to 1,000 meters 5 min 30 sec
Time to 4,000 meters 26 min
Ceiling, Service 4,000 m
Ceiling, Hovering in Ground Effect 2,000 m
Ceiling, Hovering Out of Ground Effect 1,000 m
Armament
Note The Mil Mi-2's primary mission is as a transport helicopter, but the helicopter can be equipped with: Machine guns; cannons; up to 4x AT-3 Sagger missiles; 2 x SA-7 Grail missiles; or rocket pods on some military models.
Fire Control
Fire Control System Type INA
Fire Control Radar No
Digital or Analog Cockpit Analog
Direct Fire Control No
Laser Designator No
Automated Helmet No
Sensor Suite(s) Available INA
Position Location System INA
Protection
Fuselage The helicopter's fuselage is built in three sections to facilitate mission tailoring.
Cockpit Glass A stepped windshield and a short nose with large cheek windows for a better downward view.
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW No
EW Counter Measures/CCM No
Counter Measures (Chaff/Flares) INA
Note Main and tail rotor blades electrically deiced.
Details
Country of Origin Russia
Category Transport Helicopter
Air > Transport Helicopter
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
11.1 m
Width
14.5 m
Height
3.75 m
Weight
3550 kg
Operators (29)
Russia
United States
Germany
Ukraine
Poland
India
North Korea
Czech Republic
Belarus
Algeria
Armenia
Azerbaijan
Bulgaria
Cuba
Djibouti
Estonia
Georgia
Ghana
Hungary
Indonesia
Latvia
Libya
Lithuania
Mexico
Myanmar
Peru
Slovakia
Syria
United Arab Emirates
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