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Mi-17 (Hip H) Russian Medium Transport Helicopter

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tiers
false
false
true
false
categories
"WEG"
"Aircraft"
"Rotary Wing Aircraft"
"Transport Helicopter"
"Russia (RUS)"
"PRO_Afghanistan"
"PRO_Algeria"
"PRO_Angola"
"PRO_Argentina"
"PRO_Bangladesh"
"PRO_Bolivia (Plurinational State of)"
"PRO_Bosnia and Herzegovina"
"PRO_Bulgaria"
"PRO_Burkina Faso"
"PRO_CFE Treaty"
"PRO_Cambodia"
"PRO_Cameroon"
"PRO_Chad"
"PRO_Chile"
"PRO_China"
"PRO_Colombia"
"PRO_Croatia"
"PRO_Cuba"
"PRO_Djibouti"
"PRO_Ecuador"
"PRO_Equatorial Guinea"
"PRO_Eritrea"
"PRO_Ethiopia"
"PRO_Ghana"
"PRO_Hungary"
"PRO_India"
"PRO_Indonesia"
"PRO_Iran (Islamic Republic of)"
"PRO_Iraq"
"PRO_Kazakhstan"
"PRO_Latvia"
"PRO_Libya"
"PRO_Mexico"
"PRO_Mongolia"
"PRO_Myanmar"
"PRO_Namibia"
"PRO_Nepal"
"PRO_Nicaragua"
"PRO_Niger"
"PRO_Nigeria"
"PRO_North Korea (Democratic People's Republic of Korea)"
"PRO_Pakistan"
"PRO_Peru"
"PRO_Poland"
"PRO_Russian Federation"
"PRO_Rwanda"
"PRO_Senegal"
"PRO_Serbia"
"PRO_Slovakia"
"PRO_Sri Lanka"
"PRO_Sudan"
"PRO_Syria"
"PRO_Tajikistan"
"PRO_Uganda"
"PRO_Venezuela (Bolivarian Republic of)"
"PRO_Viet Nam"
"PRO_Zambia"
"Air"
"Tier3"
notes"The Mil Mi-17 (NATO reporting name: Hip) is a Soviet/Russian helicopter in production at two factories in Kazan and Ulan-Ude. It is known as the Mi-8M series in Russian service. It is a medium twin-turbine transport helicopter. There are also armed gunship versions. The improved version of the Mi-8 is the Mi-17 Hip multipurpose helicopter, also known as the Mi-8TMB. It is specifically designed for improved capabilities at high altitudes and in hot weather conditions. The Mi-17 is identifiable from the Mi-8 by the additional air filters on the turbine air intakes, as well as the left-hand side mounted tail rotor, required by the more powerful TB-3-117A turboshaft engines it is fitted with. The Mi-17 can climb at the rate of 8m/s. The maximum and cruise speed of the helicopter is 250km/h and 225 km/h respectively. The range of the helicopter is 465 km and the service ceiling is 6,000m. The aircraft weighs around 7,489 kg and its maximum take-off weight is 13,000 kg. The Mi-8/17 has given rise to a bewildering range of versions that fulfill a wide variety of specialized roles. Dedicated combat support variants include airborne reserve command post, electronic countermeasures (with onboard jammers), Communications intelligence, and command relay. Other versions carry out delivery of fuel to front-line units, photo-reconnaissance, artillery fire-correction, reconnaissance, VIP transport, minelaying, and mine clearing."
dateOfIntroduction1975
countryOfOrigin"Russia (RUS)"
proliferation"Afghanistan, Algeria, Angola, Argentina, Bangladesh, Bolivia (Plurinational State of), Bosnia and Herzegovina, Bulgaria, Burkina Faso, CFE Treaty, Cambodia, Cameroon, Chad, Chile, China, Colombia, Croatia, Cuba, Djibouti, Ecuador, Equatorial Guinea, Eritrea, Ethiopia, Ghana, Hungary, India, Indonesia, Iran (Islamic Republic of), Iraq, Kazakhstan, Latvia, Libya, Mexico, Mongolia, Myanmar, Namibia, Nepal, Nicaragua, Niger, Nigeria, North Korea (Democratic People's Republic of Korea), Pakistan, Peru, Poland, Russian Federation, Rwanda, Senegal, Serbia, Slovakia, Sri Lanka, Sudan, Syria, Tajikistan, Uganda, Venezuela (Bolivarian Republic of), Viet Nam, Zambia"
selectedregions
"All Regions"
checkedregions
Empty array
checkedcountries
"Afghanistan"
"Algeria"
"Angola"
"Argentina"
"Bangladesh"
"Bolivia (Plurinational State of)"
"Bosnia and Herzegovina"
"Bulgaria"
"Burkina Faso"
"CFE Treaty"
"Cambodia"
"Cameroon"
"Chad"
"Chile"
"China"
"Colombia"
"Croatia"
"Cuba"
"Djibouti"
"Ecuador"
"Equatorial Guinea"
"Eritrea"
"Ethiopia"
"Ghana"
"Hungary"
"India"
"Indonesia"
"Iran (Islamic Republic of)"
"Iraq"
"Kazakhstan"
"Latvia"
"Libya"
"Mexico"
"Mongolia"
"Myanmar"
"Namibia"
"Nepal"
"Nicaragua"
"Niger"
"Nigeria"
"North Korea (Democratic People's Republic of Korea)"
"Pakistan"
"Peru"
"Poland"
"Russian Federation"
"Rwanda"
"Senegal"
"Serbia"
"Slovakia"
"Sri Lanka"
"Sudan"
"Syria"
"Tajikistan"
"Uganda"
"Venezuela (Bolivarian Republic of)"
"Viet Nam"
"Zambia"
dis
name"MI17 HIP H"
string"01.02.222.021.001.009.000"
images
"Mi-17_(A).jpg"
"Mi-17_(B).jpg"
"Mi-17_(C).jpg"
sections
name"System"
properties
name"Alternative Designation"
value"Mi-17; Mil Mi-17; Hip H"
name"Manufactuer"
value"Kazan Helicopter Plant Ulan-Ude Aviation Plant"
name"Primary Function"
value"Armed assault-transport"
name"Type"
value"Medium twin-turbine transport helicopter"
name"In Service"
value"1975-Present"
name"Crew"
value"3 (2x pilots, 1x flight engineer)"
name"Blades, Main Rotor"
value"5"
units"ea"
name"Blades, Tail Rotor"
value"3"
units"ea"
name"Day/Night Capable"
value"The Mi-8 is equipped with instruments and avionics allowing operation in day, night, and instrument meteorological conditions."
name"All Weather Capable"
value"The Mi-8 is equipped with instruments and avionics allowing operation in day, night, and instrument meteorological conditions."
name"Takeoff or Landing Limitations"
value"INA"
name"Vertical Climb Rate"
value"9"
units"m/s"
name"Number of Hard Points"
value"4"
units"ea"
name"Standard Payload"
value"HIP: 24 troops, or 3,000 kg internal or external loads on 4x hardpoints."
name"Landing Gear"
value"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"
name"Dimensions"
properties
name"Length, with Rotors Turning"
value"25.2"
units"m"
name"Length, Fuelage"
value"18.2"
units"m"
name"Width"
value"2.5"
units"m"
name"Height"
value"5.65"
units"m"
name"Main Rotor Diameter"
value"21.3"
units"m"
name"Tail Rotor Diameter"
value"3.9"
units"m"
name"Cargo Compartment, Length"
value"5.3"
units"m"
name"Cargo Compartment, Width"
value"2.3"
units"m"
name"Cargo Compartment, Height"
value"1.8"
units"m"
name"Weight, Maximum Gross"
value"13,000"
units"kg"
name"Weight, Normal Takeoff"
value"11,100"
units"kg"
name"Weight, Empty"
value"7,489"
units"kg"
name"Automotive"
properties
name"Engine Name"
value"2 x TV3-117VM"
name"Engine Type"
value"Medium twin-turbine"
name"Engine Power"
value"1,900"
units"hp"
name"Fuel, Internal"
value"445 liters"
name"Fuel, Internal Aux Tank"
value"915 liters ea"
name"Fuel, External Fuel Tank"
value"45 liters in port tank, 680 liters in starboard tank"
name"Speed, Maximum"
value"250"
units"km/h"
name"Speed, Average"
value"240"
units"km/h"
name"Service Ceiling"
value"4,500"
units"m"
name"Range, Maximum Load"
value"350"
units"km"
name"Range, Normal Load"
value"460"
units"km"
name"Range, with Auxilery Fuel"
value"950"
units"km"
name"Service Ceiling, Service"
value"6,000"
units"m"
name"Service Ceiling,Hover (out of ground effect)"
value"800"
units"m"
name"Service Ceiling,Hover (in ground effect)"
value"1,900"
units"m"
name"Vertical Climb Rate"
value"9"
units"m/s"
name"Standard Payload"
value"HIP H: 24 troops, or 3,000 kg internal or external loads on 4x hardpoints."
name"Door Mounted Gun"
properties
name"Note"
value"Loaded combat troops can fire personal weapons through windows from inside cabin."
name"Wing Mounted Weapons"
sections
name"Rocket System"
properties
name"Name"
value"UB-32 (rocket pod)"
name"Type"
value"57 mm, reusable, 32-salvo rocket pod"
name"Length, Launcher"
value"2,080"
units"mm"
name"Diameter, Launcher"
value"464"
units"mm"
name"Basic Load for the UB-32 Rocket Pod"
value"4, one on each hardpoint"
name"Number of Rockets in each UB-32 Rocket Pod"
value"32"
units"ea"
name"Rocket"
properties
name"Name"
value"S-5 Rockets"
name"Type"
value"Rocket"
name"Length, Rocket"
value"2,080"
units"mm"
name"Diameter, Rocket"
value"481"
units"mm"
name"Weight Empty"
value"103"
units"kg"
name"Weight Loaded"
value"264"
units"kg"
name"Warhead Types"
value"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"
name"Maximum Effective Range"
value"3-4 km depending on the warhead and fuze"
name"Basic Load"
value"32 S-5 Rockets per UB-32 Rocket Pod"
properties
name"Additional Armament that can be equipped on the Mi-8T"
value"2 x 7.62-mm or 1 x 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"
name"Fire Control"
properties
name"Fire Control System Type"
value"INA"
name"Fire Control Radar"
value"INA"
name"Digital or Analog Cockpit"
value"INA"
name"Direct Fire Control"
value"Yes"
name"Laser Designator"
value"INA"
name"Automated Helmet"
value"INA"
name"Position Location System"
value"Yes"
name"Weather Radar"
value"Type 8A-813"
name"Navigation"
value"DISS-32-90 Doppler navigation under tailboom"
name"Protection"
properties
name"Armor Type"
value"Bolt-on"
name"Fuselage"
value"semi-monocoque pod and boom fuselage has a nearly stepless front"
name"Cockpit Glass"
value"large, five-section windshield and lower nose windows"
name"Stealth Properties"
value"No"
name"Heat Signature Reduction"
value"IR over engine exhausts"
name"Add on Armor"
value"Available"
name"NBC Protection"
value"Yes"
name"EW"
value"INA"
name"EW Counter Measures/CCM"
value"INA"
name"Counter Measures (Chaff/Flares)"
value"Yes,ASO-3 and ASO-2 chaff/flare countermeasures system"
name"Jammer"
value"Hot Brick IR"
variants
name"Mi-17/Mi-8MT/Mi-8MTV/Mi-17V Hip-H"
notes"These designations refer to the mid-life upgrade given to the original Mi-8 (see "Description," above). Those with a V designation are the armed configuration and are equipped with bolt-on armor on the side and behind the pilot's seat, ASO-3 and ASO-2 chaff/flare countermeasures system (consisting of three banks of launchers on each side and underneath the tailboom), Hot Brick IR jammers and IR suppressors over the engine exhausts. It was first shown in August 1989"
name"Mi-17P"
notes"This is an improved electronic countermeasures (ECM) helicopter fitted for electronic warfare, communications jamming and intercept."
name"Mi-17PI"
notes"Similar to Mi-17P, but with one D-band jammer."
name"Mi-17PG"
notes"Similar to Mi-17P, but with H/I-band pulse and continuous wave jamming system."
name"Mi-17Z-II"
notes"This is an electronic warfare variant used by Czech and Slovak air forces. It is reportedly either an airborne early warning (AEW) or electronic warfare (EW) version."
name"Mi-17MD"
notes"This refers to the current Kazan production model. It is similar to the standard Mi-17 but has its passenger capacity increased to 40 and is fitted with built-in rear ramp that can rise to meet truncated clam-shell doors."
name"Mi-17KF"
notes"This is a new variant jointly developed by Kazan, Mil and Kelowna Flightcraft."
name"Mi-171"
notes"This Mi-17 variant is fitted with TV3-117VM engines (2,070 shaft hp) for improved lifting capability and performance."
name"Mi-171M/Mi-171A2"
notes"This is a new variant announced by Russian Helicopters in June 2010. It features a Klimov VK-2500PS-03 turboshaft engine, with full authority digital engine control (FADEC), modernized auxiliary power unit and main gearbox, as well as improved swashplate, main rotor head and transmission. A new X-shaped tail rotor and composite rotors are fitted."
name"Mi-17M/Mi-171V"
notes"This is the current production version from Kazan helicopters. It is nearly identical to Mi-171 except that it has options for armament, radar, flotation gear or fire-fighting equipment."
name"Mi-172"
notes"This version is also similar to Mi-171, but is equipped for civilian flight operations. It was developed under a July 2002 agreement among the Kazan plant, BAE Systems and Kelowna Flightcraft of Canada."
name"Mi-17 Pratap"
notes"This is the Indian air force designation for its Mi-17 aircraft."
name"Mi-17-1VA"
notes"This is an ambulance variant developed for Russian Ministry of Health for civilian disaster relief. It is equipped for in-flight emergency treatment."
name"Mi-17V5"
notes"This variant is equipped with a full glass cockpit, advanced avionics and navigation systems. It has onboard weather radar, state of the art autopilot and is compatible with third-generation night-vision goggles. A powerful winch is fitted for disaster relief operations."
name"Mi-171E"
notes"This helicopter is powered by VK-2500-03 engines and has a Safir 5K/G Mi auxiliary power plant to support high altitude operations."
name"Mi-171E2"
notes"This is an improved variant of the Mi-171E with VK-2500PS-03 high-altitude engines with increased power; full authority digital engine control (FADEC); new main rotor made of polymeric composite materials with an improved profile; an X-shaped tail rotor similar to that on the Mi-171A2; and an upgraded fuselage, modified tail and keel beams and a larger stabilizer."
name"Mi-171SH Storm"
notes"This is a modernized combat transport variant with upgraded engines; new rotor system with an improved profile composite main rotor and X-shaped tail rotor; and the latest variant of the President-S self-defense system. It features titanium and Kevlar armor protection."
type"WEG"
version1
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