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Mi-8T (Hip C) Russian Medium Transport Helicopter

Mi-8T

Utility Helicopter
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Basic Information
Name
Mi-8T (Hip C) Russian Medium Transport Helicopter
Designation
Mi-8T
Alternate Designation
Mi-8T; Mil Mi-8T; Hip C
Equipment Type
Utility Helicopter
Manufacturer
Date of Introduction
1980
Description

The Mi-8T (Hip C) is the basic civil and military transport version of the Hip. Civil versions lack armaments and can carry up to 32 passengers or 12 litter patients or cargo. The survivability features of the Mi-8 include crew cabin armor plating, explosive-resistant foam filling in the fuel tanks, a fire-fighting system and duplicated and standby hydraulic and power systems and main control circuits.

Air & Air Defense Specifications
Crew 3
Engine Turboshaft (1 hp)
Service Ceiling 4500 m
Variants
List of Variants - See Below Mi-8 Hip-A Mi-8 Hip-B Mi-8T Hip-C (Transportny, transport) Mi-8TM Mi-8TV Mi-8S Hip-C (Salon) Mi-8 VIP Mi-8VZPU Hip-D Mi-8TB Hip-E Mi-8TBK Hip-F ( Kommercheskiy, commercial) Mi-9 Hip-G Mi-8MPS Mi-8SMV Hip-J Mi-8P/PPA Hip-K Mi-8AMTSh/Mi-171Sh Mi-8AMTSh-V Mi-8AMTSh-VA Mi-8TG Mi-8 Rana Mi-8MTPR-1 Mi-17/Mi-8MT/Mi-8MTV/Mi-17V Hip-H Mi-17P Mi-17PI Mi-17PG Mi-17Z-II Mi-17MD Mi-17KF Mi-171 Mi-171M/Mi-171A2 Mi-17M/Mi-171V Mi-172 Mi-8MTV (Visotnii, high altitude) Mi-17 Pratap Mi-17-1VA Mi-17V5 Mi-171E Mi-171E2
System
Alternative Designation Mi-8T; Mil Mi-8T; Hip C
Manufactuer Kazan Helicopter Plant Ulan-Ude Aviation Plant
Primary Function This is the basic civil and military transport version of the Hip.
Type Medium twin-turbine transport helicopter
In Service 1980-Present
Crew 3 (2x pilots, 1x flight engineer) ea
Passengers Civil versions lack armaments and can carry up to 32 passengers or 12 litter patients or cargo.
Blades, Main Rotor 5
Blades, Tail Rotor 3 ea
Number of Hard Points 4 ea
Day/Night Capable The Mi-8T is equipped with instruments and avionics allowing operation in day, night, and instrument meteorological conditions.
All Weather Capable The Mi-8T is equipped with instruments and avionics allowing operation in day, night, and instrument meteorological conditions.
Vertical Climb Rate 9 m/s
Standard Payload 4.0 t cargo or armament instead of passengers
Landing Gear Fixed main gear struts run down and out from attachment points on the upper, rear fuselage. A second strut holds the wheel well away from the lower fuselage. The two-wheel nose gear is fitted under the fuselage just behind the cockpit
Takeoff or Landing Limitations INA
Dimensions
Length, with Rotors Turning 25.2 m
Length, Fuelage 18.2 m
Width 2.5 m
Height 5.65 m
Main Rotor Diameter 21.3 m
Tail Rotor Diameter 3.9 m
Cargo Compartment, Length 5.3 m
Cargo Compartment, Width 2.3 m
Cargo Compartment, Height 1.8 m
Weight, Maximum Gross 13,000 kg
Weight, Normal Takeoff 11,100 kg
Weight, Empty 7,489 kg
Automotive
Engine Name 2x Isotov TV2-117A
Engine Type Medium twin-turbine
Engine Power 1.700 shp each
Speed, Maximum 250 km/h
Speed, Average 240 km/h
Service Ceiling 4,500 m
Range, Maximum Load 350 km
Range, Normal Load 460 km
Range, with Auxilery Fuel 950 km
Fuel, Internal 1,870 liters
Fuel, External 980 liters
Service Ceiling, Service 6,000 m
Service Ceiling,Hover (out of ground effect) 800 m
Service Ceiling,Hover (in ground effect) 1,900 m
Vertical Climb Rate 9 m/s
Door Mounted Gun
Note Loaded combat troops can fire personal weapons through windows from inside cabin.
Wing Mounted Weapons
Additional Armament that can be equipped on the Mi-8T 2 - 7.62-mm or 1x 12.7-mm MG 4-6 - AT-2C Swatter or AT-3 Sagger ATGMs 4-6 - 57-mm rocket pods (16 each) 2 - 80-mm rocket pods (20 each) 4 - 250-kg bombs 2 - 500-kg bombs 2 - 12.7-mm MG pod 2 - Twin 23-mm gun pods 1,830 liters Additional fuel tanks
Rocket System
Name UB-32 (rocket pod)
Type 57 mm, reusable, 32-salvo rocket pod
Length, Launcher 2,080 mm
Diameter, Launcher 464 mm
Basic Load for the UB-32 Rocket Pod 4, one on each hardpoint ea
Number of Rockets in each UB-32 Rocket Pod 32 ea
Rocket
Name S-5 Rockets
Type Rocket
Length, Rocket 2,080 mm
Diameter, Rocket 481 mm
Weight Empty 103 kg
Weight Loaded 264 kg
Warhead Types produced in a variety of sub-types with different warheads, including HEAT anti-armour (S-5K), high-explosive fragmentation (S-5M/MO), smoke, and incendiary rounds
Maximum Effective Range 3-4 km depending on the warhead and fuze
Basic Load 32 S-5 Rockets per UB-32 Rocket Pod
Fire Control
Fire Control System Type INA
Fire Control Radar INA
Digital or Analog Cockpit INA
Navigation Radar DISS-32-90 Doppler navigation under tailboom
Direct Fire Control Yes
Laser Designator INA
Automated Helmet INA
Position Location System Yes
Weather Radar Type 8A-813
Protection
Armor Type The survivability features of the Mi-8 include crew cabin armor plating, explosive-resistant foam filling in the fuel tanks, a fire-fighting system and duplicated and standby hydraulic and power systems and main control circuits.
Fuselage semi-monocoque pod and boom fuselage has a nearly stepless front
Cockpit Glass large, five-section windshield and lower nose windows
Stealth Properties No
Heat Signature Reduction IR over engine exhausts
Add on Armor Available
NBC Protection Yes
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) Yes,ASO-3 and ASO-2 chaff/flare countermeasures system
Jammer Hot Brick IR
Details
Country of Origin Russia
Category Transport Helicopter
Air > Transport Helicopter
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
2.5 m
Height
5.65 m
Weight
13000 kg
Operators (55)
Russia
China
Poland
India
Iran
North Korea
Pakistan
Serbia
Afghanistan
Algeria
Angola
Argentina
Bangladesh
Bolivia
Bosnia and Herzegovina
Bulgaria
Burkina Faso
Cambodia
Cameroon
Chad
Chile
Colombia
Croatia
Cuba
Djibouti
Ecuador
Equatorial Guinea
Eritrea
Ethiopia
Ghana
Hungary
Indonesia
Iraq
Kazakhstan
Latvia
Libya
Mexico
Mongolia
Namibia
Nepal
Nicaragua
Niger
Nigeria
Peru
Rwanda
Senegal
Slovakia
Sri Lanka
Sudan
Syria
Tajikistan
Uganda
Venezuela
Vietnam
Zambia
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