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Mi-14 (Haze) Russian Anti-Submarine Warfare (ASW) Helicopter

Mi-14

Autonomous Unmanned Helicopter
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Basic Information
Name
Mi-14 (Haze) Russian Anti-Submarine Warfare (ASW) Helicopter
Designation
Mi-14
Alternate Designation
Mi-14; NATO: Haze
Equipment Type
Autonomous Unmanned Helicopter
Manufacturer
Kazan Helicopters
Date of Introduction
1975
Description

The Mi-14 (Haze) Russian Anti-Submarine Warfare (ASW) Helicopter is a naval land-based helicopter, derived from the Mi-8 Hip, which is configured primarily for anti-submarine warfare (ASW). It also serves in minesweeping and search-and-rescue (SAR) roles. Modifications from the basic Mi-8 configuration include the provision of a hull that has an upturned, scalloped front; a tail boom float; retractable landing gear; port-side anti-torque rotor; and shortened engine nacelles. A large radome holding a search radar is located under the nose and is fully submerged when afloat. The ventral weapons bay is enclosed by two sets of split doors separated by a narrow central keel. Formal development of anti-submarine warfare (ASW) version of the Mil Mi-8 transport helicopter was authorized by the Soviet Communist Party Central Committee and Council of Ministers in April 1965, with the objective of replacing the Mil Mi-4 in the short-range, shore-based anti-submarine role. The new helicopter was required to have an endurance of 2 hours on station at a radius of 222 kilometers (120 nmi; 138 mi) from the base. The new design (with the internal designation V-14) differed from the Mi-8 in having a boat-like hull similar to the Sea King, allowing it to operate off the water, and a retractable four-point undercarriage,[N 1] with the mainwheels retracting into large sponsons on the rear of the fuselage. The helicopter was to be powered by two Klimov TV3-117MT turboshaft engines. A watertight weapons bay is fitted to the centreline of the fuselage allowing internal carriage of a single torpedo or eight depth charges, while a radome housing a search radar is fitted beneath the nose. The first prototype V-14, converted from a Mi-8 and powered by the older and less powerful Klimov TV2-117 engines, flew on 1 August 1967. Development was slowed by problems with the helicopter's avionics and due to reliability problems with the TV3-117 engines, with production at Kazan not starting until 1973, and the helicopter (now designated Mi-14) entering service on 11 May 1976. In January 2016, Russian Helicopters confirmed to Russian News Agency TASS that no final decision to revive production had been taken, but market demand, feasibility studies – including with Moscow's defense ministry – and funding sources were under review. The program remains a “priority” for Russian Helicopters. The company suggested the Mi-14 would appeal to civil operators in Russia's far north and those supplying the oil and gas industry, alongside the nation's armed forces. Out of the almost 300 Mi-14s produced at Kazan Helicopters between 1973 and 1986, it is estimated that just 44 examples remain in active service.

Air & Air Defense Specifications
Crew 4
Engine Turboshaft (1950 hp)
Max Speed 230.0 km/h
Cruise Speed 205.0 km/h
Range 800.0 km
Variants
V-14 Prototype of the Mi-14 helicopter.
Mi-14PL Haze-A This is the anti-submarine warfare version. See above for electronics fits. It has an internal weapons bay that can carry a single AT-1 torpedo, PLAB series depth bombs, APR-2 high-speed torpedoes or nuclear weapons (the last two are only carried in Russian Mi-14s).
Mi-14BT Haze-B This is a mine countermeasures version, with a fuselage strake and pod on the starboard side of cabin.
Mi-14PS Haze-C This search-and-rescue variant has an enlarged entry door on the left side of the cabin; strake and fuselage pod; retractable rescue hoist; and a large retractable searchlight on the starboard side of the nose (some have a second central nose-mounted searchlight).
Mi-1413T Haze-B This variant was designed for mine countermeasures. Initial operational capability was reached in the early 1980s.
Mi-14PL/R This is a conversion to the Mi-14PL helicopter conducted by the Polish navy to adopt it for the search-and-rescue role.
System
Alternative Designation Mi-14; NATO: Haze
Type Anti-Submarine Warfare (ASW) Helicopter
Flight Crew 2 (pilot, co-pilot)
ASW Crew 2 (sonar operator, MAD operator, as needed)
Passengers 20 (during rescue operations, no ASW crew)
Blades, Main Rotor 5 ea
Blades, Tail Rotor 3 ea
Number of Engines 2 ea
Number of Hard Points INA
Dimensions
Length 25.30 m
Height 6.90 m
Main Rotor Diameter 21.29 m
Disc Area 356 m sq
Empty Weight 11,750 kg
Maximum Takeoff Weight 14,000 kg
Automotive
Engine Name 2 x Klimov TV3-117MT
Engine Type Turboshaft
Engine Power 1,950 shaft hp each
Maximum Speed 230 km/h
Cruise Speed 205 km/h
Ceiling Hover Out of Ground Effect 3,500 m
Ceiling Hover In Ground Effect 1,600 m
Maximum Range with Maximum Payload 305 km
Cruise Range 800 km
Maximum Range with Maximum Fuel 1,135 km
Communications
HF Radio 1 x R-842-M HF receiver
VHF Receiver 1 x R-860 VHF receiver
Anti-Submarine Warfare (ASW) System
Sonobouys 1 x Baku system (up to 36 RGB-NM buoys)
Magnetic Anomaly 1 x APM-60 detector
ASW Equipment Hydro-acoustic buoys and dye packs can be carried in the bomb bay and radar beacon buoys
Torpedo System
Torpedoes 1 x AT-1 or APR-2 torpedoes
Bombing System
Bombs 1 x nuclear depth bomb or 8 x depth charges in place of torpedoes
Radar Systems
Navigation Radar 1 x Initziativa-2M/ME Doppler navigation in radome underneath nose
Sonor System
Dipping Sonar 1 x Oka-2 dipping sonar
Protection
Stealth Properties None
Add on Armor INA
Heat Signature Reduction INA
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) INA
Details
Country of Origin Russia
Category Special Purpose Helicopters
Air > Special Purpose Helicopters
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
25.3 m
Width
21.29 m
Height
6.9 m
Weight
14000 kg
Operators (9)
Russia
Ukraine
Poland
North Korea
Congo, Republic of the
Georgia
Libya
Syria
Yemen
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