MI-8 HIP Multi-role Transport Helicopter

The MI-8 HIP is a multi-role transport helicopter able of carring troops or food as able-bodied as administering armed attackes with rockets and guns. It is generally acclimated to resupply guerrillas, admit detachments or accommodate abutting air abutment to advancing units. Designed as a carriage helicopter, the Mi-8 accepted a multi-purpose machine. The cable alien suspension, able with the weight-measuring device, makes it accessible to backpack ample admeasurement cargoes belief up to three tons. If required, it became both combat, accomplishment and arms ascertainment helicopter.

The large, five-blade capital rotor is army over the engine at the physique midsection, while a weapon-carrying belvedere is army at the lower physique midsection. Alien food are army on weapons racks on anniversary ancillary of the fuselage. The HIP C has four alien hardpoints; the HIP E, HIP H, accept six; added variants accept none. Not all accessible ammunition are active at one time, mission dictates weapon configuration.

Twin turboshaft engines are army on top of the assembly with two annular air intakes just aloft the cockpit and angled bankrupt ports aft. It is powered by two TV2117A turboshafts (2 x 1120 kW, or 2 x 1250 kW over a abbreviate time). The Mi-8 is able of single-engine flight in the accident of accident of ability by one engine (depending on aircraft mission weight) because of an engine amount administration system. If one engine fails, the added engine's achievement is automatically added to acquiesce connected flight.

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Mi-42 Assault-Transport Helicopter rogram

The Mil Mi-42 was a projected assault/transport helicopter featuring the NOTAR concept, fit to replace the Mi-40 program. The Mi-42 program was launched in 1985, however the entire Mi-40 program, which include the Mi-42 program, was cancelled because Soviet Union's Collapse.

Starting in 1985 a further development along the lines of these Mil Mi-40 was sought Which would provide higher performance in the "Aerial Infantry Fighting Vehicle" category. Primary roles included landing troops, providing rapid redeployment, escort, close air support and tactical strikes. Its secondary roles would contain transport of equipment, medivac, SAR/CSAR, reconnaissance and communications.

A vectoring NOTAR system would replace the tail rotor. It was hoped that this could be far more durable and increase safety of people working in the vicinity of the tail. Finally, it was planned that, as the aircraft picked up speed and aerodynamic forces began to have a stabilising effect, the vectoring system would angle the NOTAR nozzle so that it faced straight backward - hopefully allowing the Mi-42 to attain its required top speed of 380-400kph.

The design was intended to be heavily armored and carry a mobile forward firing cannon and four hardpoints (equivalent armament to the Mil Mi-28 gunship). because of the complex requirements (essentially mixing those of a truck, transport helicopter, attack helicopter and strike aircraft) the design uncontrollably took on complexity and weight.

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Ka-52 Alligator Combat Helicopter

The multi-role all-weather combat Ka-52 "Alligator" helicopter is a genuinely twin-seat derivative of the Ka-50. It's intended to get a great deal of combat tasks in daytime and night conditions. This is a a commander helicopter of the army aviation aimed growing the efficiency of group combat helicopter operations.

Coaxial-type Ka-52 helicopter differs from one its predecessor by a wider nose part and twin-seat crew cockpit where the pilot ejection seats seem to be arranged side-by-side. Both pilots have full controls of these helicopter without having any limitations. The helicopter could be employed as a trainer. High flying qualities of these coaxial helicopter combined with distinctive manoeuvrability allow the helicopter to perform combat maneuvers within the minimum air region and with the shortest time to gain an advantageous attack position.

Numerous weapons choices for the helicopter seem to be achieved by arranging a movable high-speed firing gun starboard of the helicopter, and six available external wing stores with other various combination of anti-tank missiles, rockets, "air-to-air" missiles, gun ammunition of a container type and bombs of different caliber. from the point of view of these weapons power the "Alligator" is comparable With the "Black Shark" helicopter and it is superior to all or any existing combat helicopters.

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Mi-24 Hind Combat and Transport Helicopter

Mil Mi-24 is a twin-engined combat helicopter its meant for close support of ground forces, destruction of armored targets and transportation of persons or cargo. The Mi-24 isn't a direct counterpart to the US AH-64 Apache, since unlike this and different Western attack helicopters it's also capable of transporting up to eight troops. As a mix gunship and troop transport, the Hind combat helicopter has no direct NATO counterpart.

The helicopter has six suspension weapon units on the wingtips. The Mi24D (Mi-25) and the Mi-24V (Mi-35) are equipped with a YakB four-barrelled, 12.7mm, built-in, flexibly mounted machine gun, which has a firing rate of 4,000-4,500 rounds a minute and a muzzle velocity of 860m/s. The Mi-24P is fitted with a 30mm, built-in, fixed gun mount; the Mi-24VP with a 23mm, built-in, flexibly mounted gun.

The Mi-24P and Mi-24V have four underwing pylons for up to 12 anti-tank missiles. The Mi-24V (Mi-35) is armed with the Shturm anti-tank guided missile system. Shturm (Nato designation AT-6 Spiral) is a short-range missile with semi-automatic radio command guidance. The 5.4kg high-explosive fragmentation warhead is capable of penetrating up to 650mm of armour. Maximum range is 5km.

The helicopter is powered by two Isotov TV3-117VMA turboshaft engines, developing 2,200shp each. The air intakes are fitted with deflectors and separators to stop dust particle ingestion when taking off from unprepared sites. An auxiliary power unit is fitted.

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Mi-28N Night Hunter Combat Helicopter

The Mi-28N Night Havoc combat helicopter retains most of the structural style of the Mi-28. the most difference is that the installation of an integrated electronic combat system. other modifications include: new main gearbox for transmitting higher power to the rotor; new high-efficiency blades with swept-shaped tips; and an engine fuel injection control system.

The main sensors of the integrated electronic combat system are the microwave radar antenna, mounted on top of the rotor head, and a forward-looking infrared (FLIR) system. The system displays the helicopter location on a moving map indicator, and flight, systems and target info on liquid crystal displays. The crew are equipped with night-vision goggles.

The helicopter is powered by two TV3-117VMA turboshaft engines, fitted on either side of the fuselage. it's equipped with an auxiliary power unit for self-contained operation. The thermal signature of the helicopter has been reduced by an element of 2.5 times compared to its predecessor, the Mi-24.

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Mi-26 HALO Heavy-Lift Helicopter

The Mi-26 Halo is a twin-turbine heavy-lift helicopter. it's the world's largest production helicopter. The Halo's development started in the early 1970s. The designer's goal was to provide a helicopter with a load capability twice that of any contemporary helicopter. the firs Mi-26 Halo prototype flew in December 1977 and was first displayed at the Paris Air Show in 1981. In 1982, Russian squadrons received their first Halos, that weren't totally operational till 1983. In 1986, India was the first country to buy a Halo. Since then Halos have been sold to almost twenty countries. the value of a Halo is between $10 million and $12 million.

The Mi-26 is the helicopter with an eight-blade main rotor, that is mounted on top of the fuselage midsection on a hump. two turboshaft engines are mounted on top of the cabin with spherical air intakes above and behind the cockpit and exhaust ports at the sides of the engines. The long, bus-like body with fixed tricycle landing gear tapers to the nose and rear, with an upswept rear section and rounded nose and stepped-up cockpit. The tail is swept-back with a rather tapered fin with massive rotor on right side. The flats are forward-tapered and low-mounted on leading edge of the fin.

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Mi-28 Havoc Combat Helicopter

The Mi-28 combat helicopter has been developed by Mil Moscow Helicopter Plant and NATO codename Havoc. In August 1996 Mil rolled out a prototype of the day and night capable version, Mi-28 can fly at a most speed of 300km/h, can fly rearwards and sideways at accelerates to 100km/h and is able to hover flip at 45° a second.

The Mi-28 helicopter is a fighter whose performance is comparable to the US Apache. additionally to its ability to attack ground it would have a capability of air-to-air combat. This two-seater helicopter contains with 23 mm cannon below the nose, he takes on stumps wings of anti-tank guided laser as well as launching air-to-air missiles.

The Mi-28A helicopter is powered by two TV3-117VMA turboshaft engines, fitted on either side of the fuselage. it's equipped with an auxiliary power unit for self-contained operation. The thermal signature of the helicopter has been reduced by an element of 2|.5 times compared to its predecessor, the Mi-24.

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Ka-50 HOKUM Single Seat Attack Helicopter

The KA-50 is a powerful battle helicopter that is in restricted service with the Russian Air Force. This aircraft isn't fielded. only a handful of prototypes exist, and it's not yet been approved for full-scale production. There are 2 versions of the Hokum. The Ka-50 Hokum-A is a single seat close support helicopter and Ka-52 Hokum-B two seat trainer and combat version.

Ka-50 "Black Shark" is a single-seat attack helicopter for destroying armored vehicles, slow-speed air targets and manpower on the battlefield. The Mi-28N and Kamov Ka-50 are competing to fulfil the Russian Army Aviation demand for a night-capable anti-tank helicopter, a replacement to the Mi-24 created 25 years ago.

The Ka-50 has appeared in only a few variants and principally developmental types that attempted to shore up limitations in the original design. The V-80 represented the originals prototype designation and was followed by two V-80Sh-1 "Shturmovik-1" pre-production models. a night capable Ka-50 appeared in the form of the Ka-50N and Ka-50Sh varieties. The Ka-50-2 was to be an export product while the Ka-50-2 "Erdogan" was in competition for Turkish sale and represented a joint Kamov/Israeli attempt that includes a twin-tandem cockpit. The Ka-52 "Alligator" was a revised Ka-50 design with twin-seating in ade-by-side format and was an all-weather, day / night capable attack system.

The KA-50 features distinctive maneuvrability and operating characteristics because of the contra-rotating co-axial rotors. The coaxial counter-rotating rotor system negates the requirement for a tail rotor and its drive system. due to this, this aircraft is unaffected by wind strength and direction, has an unlimited hovering turn rate, and offers a smaller profile and acoustic signature, while allowing a 10-15% bigger power margin. The HOKUM is absolutely aerobatic. It can perform loops, roll, and "the funnel", where the aircraft will maintain a targeted point of fire while flying circles of varying altitude, elevation, and air speed round the target.

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