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    Mil Mi-8 (Hip) Multirole Medium Helicopter (1967)

    Mil Mi-8 (Hip) Multirole Medium Helicopter (1967)

    Use of the Mil Mi-8 Hip was worldwide with the type being utilized in its military and civilian guises.





    Staff Writer (Updated: 10/7/2015):

    Numbering well over 12,000 production examples, the Mil Mi-8 (NATO reporting name of "Hip") can be viewed as one of the most successful helicopter designs of all time. It has seen use as a passenger transport, troop transport, vip transport, reconnaissance, electronic warfare, assault, artillery spotter and airborne command post throughout its tenure with the various nations that have purchased the aircraft. Even today, the Mi-8 remains in use as an operational-level instrument in many of the air forces and army groups that have seen value in the type. As of this writing, production continues despite some 42 years since the first Mi-8 rolled off of the assembly lines at the Mil Moscow Helicopter Plant - then under the Soviet banner.

    The Mi-8 was developed as a replacement for the Mi-4 "Hound", a piston-engined transport helicopter appearing in 1953 that could seat up to fourteen personnel. Utilizing some of the successful internal workings of the Mi-4, the new Mil design featured a single Soloviev turboshaft engine of 2,700 shaft horsepower mated to an all-new enlarged fuselage. The prototype took on the name of Mi-8 ("Hip-A") and achieved first flight on July 9th, 1961. Follow-up developmental testing soon revealed the design to lack in power and, as such, the single engine idea was dropped in favor of a twin-engined design featuring two Isotov TV2 turboshaft engines. A five-blade main rotor was also used in this revision which produced the second prototype, first flying on September 17th, 1962. Minor revisions followed and the Mi-8 was fully introduced in Soviet Air Force service sometime in 1967. The initial production versions all fell under the NATO designation of "Hip-C" and constituted the base militarized model and a civilian model (noted for its square windows instead of round). Since then, the Hip series has been expanded to include a plethora of upgraded and specially-designed versions.

    Externally, the Mi-8 maintains a most utilitarian look about her. She sports a low-slung front crew area with extensive glazing that offers up excellent views from the cockpit. Immediately to the cockpit's rear is the spacious crew cabin with side-mounted sliding doors. On most versions, the tricycle undercarriage is static (one such Hip offered a retractable undercarriage) which adds to the types distinct look. Two engines are mounted above and to the rear of the crew cabin area and power a large five-blade main rotor system. The empennage is also a distinct feature of this rotorcraft as it sits high in the design and sports a single vertical tail fin, horizontal plane and a three-blade tail rotor mounted to the starboard side (the similar Mi-17 mounts the tail rotor to port). A modified Hip system features a rear-loading ramp. The crew consists of a pilot, co-pilot and a loadmaster.



    SPECIFICATIONS:
    Mil-Mi-8T (Hip-C)
    Type: Multirole Medium Helicopter
    National Origin: Soviet Union
    Manufacturer(s): Mil Moscow Helicopter Plant - Soviet Union / Russian Helicopters - Russia
    Introduction: 1967
    Production Total: 12,500


    OPERATORS
    Afghanistan; Albania; Algeria; Angola; Anguilla; Armenia; Azerbaijan; Turkey; Belarus; Bangladesh; Bhutan; Bosnia and Herzegovina; Bulgaria; Burkina Faso; Canada; Cambodia; China; Colombia; Croatia; Cuba; Czech Republic; Djibouti; East Germany; Ecuador; Egypt; Estonia; Ethiopia; Finland; Germany; Georgia; Ghana; Guinea-Bissau; Hungary; Israel; India; Indonesia; Iran; Iraq; Kazakhstan; Kenya; Kyrgyzstan; Laos; Latvia; Libya; Lithuania; Macedonia; Madagascar; Malaysia; Montenegro; Maldives; Mali; Mexico; Moldova; Mongolia; Mozambique; Myanmar; Nepal; New Zealand; Nicaragua; North Korea; North Vietnam; Pakistan; Peru; Poland; Romania; Russia; Senegal; Serbia; Sierra Leone; Sri Lanka; Slovakia; Somalia; South Africa; Soviet Union; Sudan; Syria; Tajikistan; Turkmenistan; Uganda; Ukraine; Uzbekistan; United States; Vietnam; Venezuela; Yemen; Yugoslavia; Zambia

    STRUCTURAL

    Crew: 3
    Length: 59.61 feet (18.17 meters)
    Width: 69.85 feet (21.29 meters)
    Height: 18.24 feet (5.56 meters)
    Weight (Empty): 16,006 lb (7,260 kg)
    Weight (MTOW): 26,455 lb (12,000 kg)


    POWER

    2 x Klimov TV3-117Mt turboshaft engines developing 1,950 shaft horsepower each and drivign a five-blade main rotor and three-blade tail rotor.


    PERFORMANCE

    Maximum Speed: 162 mph (260 kmh; 140 knots)
    Maximum Range: 280 miles (450 km)
    Service Ceiling: 14,764 feet (4,500 meters; 2.8 miles)
    Rate-of-Climb: 0 feet-per-minute (0 m/min)

    Compare Two Aircraft


    ARMAMENT

    Hardpoints: 6
    Armament Suite:
    Up to 6 x Hardpoints for rocket pods, anti-tank missiles and bombs. Ordnance can include a combination of the following:

    UV-16-57 rocket pods (S-5 rockets)
    UV-32-57 rocket pods
    AT-2 "Swatter" anti-tank missiles
    AT-3 "Sagger" anti-tank missiles
    9M17 Phalanga anti-tank missiles
    Nose-Mounted KV-4 12.7mm machine gun
    Mine Dispensers
    551lb drop bombs
    Side-Mounted PK machine gun(s)


    VARIANTS
    V-8 ("Hip-A") - Single-Engine Prototype


    V-8A - Twin-Engine Prototype; fitted with TV2-117 series turboshaft engines.

    V-8AT - Mi-8T Utility Prototype

    Mi-8 ("Hip-B") - Twin-Engine Prototype

    Mi-8TG - Converted LPG gas-capable Mi-8

    Mi-18 - Prototype based on Mi-8; lengthened fuselage; sliding starboard-side door added; retractable undercarriage.

    Mi-8T ("Hip-C") - Initial quantitative production model; provision for 4 x UV-16-57 rocket pods; side-facing PK machine gun.

    Mi-8TV - Armed version based on the Mi-8T model.

    Mi-8TVK / Mi-8TB ("Hip-E") - Gunship Variant; provision for 6 x UV-32-57 rocket pods, 4 x AT-2 "Swatter" anti-tank missiles and 2 x 551lb drop bombs; KV-4 machine gun fitted to nose.

    Mi-8TBK ("Hip-F") - Gunship Export Model; provision for 6 x Malyutka anti-tank missiles.

    Mi-8IV ("Hip-G") - Utility transport; provision for 4 x UV-16-57 rocket pods; side-facing PK-machine gun.

    Mi-9 - Export version of the Mi-8IV model.

    Mi-8PPA ("Hip-K") - Export Electronic Warfare / Airborne Command Post; fitted with 6 antenna structures.

    Mi-8PD - Polish Airborne Command Post

    Mi-8PS / Mi-8TPS ("Hip-D") - Command Post / Communications Platform.

    Mi-8SMV ("Hip-J") - Airborne Jamming Platform

    Mi-8VPK / Mi-8VZPU ("Hip-D") - Airborne Communications Platform.

    Mi-8AMT - Unarmed Transport

    Mi-8AMT(Sh) - Based on the Mi-8MTV; fitted with electro-optic sight and radar system; armed or unarmed version.

    Mi-8AV - Minelayer

    Mi-8VT - Mine Clearer

    Mi-8MB - MedEvac Version

    Mi-8MTO - Night Attack Model

    Mi-8R - Reconnaissance Platform

    Mi-8K - Reconnaissance / Artillery Observation Platform.

    Mi-8PT - Staff Transport; improved communications suite.

    Mi-8SKA - Photo-Reconnaissance Platform

    Mi-8T(K) - Photo-Reconnaissance Platform

    Mi-8TZ - Fuel Transport

    Mi-8T ("Hip-C") - Utility Transport; seating for 24; fitted with 2 x Klimov TV2-117A turboshaft engines of 1,677 shaft horsepower each.

    Mi-8P - Civilian Transport; seating for up to 32; in-flight galley and restroom facilities.

    Mi-8S "Salon" - Civilian VIP Transport; seating for up to 11; in-flight galley and toilet facilities.

    Mi-8M - Russian Service Designation for similar Mi-17 "Hip".

    Mi-8MPS - Search and Rescue (SAR) Variant

    Mi-8MA - Cold Weather Exploration Variant

    Mi-8MT - Aerial Crane Variant

    Mi-8MTV - Improved "hot and high" model; fitted with TV3-117VM turboshaft engines.

    Mi-8AT - Civilian Transport; fitted with revised and improved TV2-117AG series turboshaft engines.

    Mi-8ATS - Agricultural Sprayer

    Mi-8TL - Accident Investigation Model

    Mi-8TM - Transport Model; fitted with weather radar.

    Mi-8TS - Hot Weather Variant

    Mi-8VIP - Luxury VIP Transport; seating for up to 9.

    Mi-8PA - Heavy Material Transport; single production examples used by Japan.

    Mi-171 - Ulan-Ude export equivalent of the Mi-8AMT.

    Mi-171A - Civilian market passenger transport

    Mi-171A1 - Civilian market cargo transport

    Mi-171A2 - Digitally-controlled Klimov VK-2500PS-03 engines of 2,400shp; new rotor; glass cockpit.

    Mi-171C - Local Chinese-built variant of the Mi-171; under Sichuan Lantian Helicopter Company Ltd brand label; outfitted with twin radar configuration; single ramp door at rear.

    Mi-171E - Fitted with VK-2500-03 series engines for extreme weather service.

    Mi-171LL - Flying testbed for Mi-171 series

    Mi-171M - Modernized Mi-171; standard operating crew of two (from three).

    Mi-171S - Mi-171 completed with Western-minded avionics suite.

    Mi-171Sh - Export variant of the Mi-8AMTSh

    Mi-172 - Kazan export equivalent of the Mi-8AMT.

    Mi-8MTV-3 - Kazan export equivalent of the Mi-8AMT.

    Mi-17 ("Hip") - Developed from the Mi-8; known as the Mi-8M in Russian service; tail rotor mounted to port-side; fitted with TV3-117MT engines, larger rotor and transmission.

    Mi-17MD - Kazan-developed Mi-8 with rear ramp and dolphin-nose housing radar.

    Mi-17KF - Kazan-developed Mi-8 with Western-type electronics suite.




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