“Hunter” to learn: the Ministry of Defense has distributed new Mi-28UB

Mi-28
Type:	Attack helicopter
Developer:	OKB M. L. Mil.
Manufacturer:	Rostvertol
First flight:	Mi-28: November 10, 1982, Mi-28N: November 14, 1996
Start of operation:	October 15, 2009
Status:	Operated, produced
Main operators:	Russian Air Force

Mi-28 (according to NATO classification - Havoc , literally - “Devastator”) is a Soviet/Russian attack helicopter of the 4th generation, designed to search and destroy, in conditions of active counterfire, tanks and other armored vehicles, as well as low-speed air targets and enemy manpower.

Story

The development of the helicopter was carried out at the Moscow Helicopter Plant named after. M. L. Mil since 1980 in the conditions of creative competition with the Kamov Design Bureau, which was creating an alternative combat helicopter, the Ka-50. The first prototype of the Mi-28 helicopter made its first flight on November 10, 1982. The first model of the Mi-28 was intended primarily for performance testing and did not carry a weapon system. It was installed on the second flight prototype, the assembly of which was completed by the pilot production of the cost center in September 1983. Its design took into account all the comments of the Air Force mock-up commission. The construction of the third flying prototype of the Mi-28, the design of which took into account all the customer’s comments and changes made to the experimental samples as they were refined, pilot production at the Moscow Helicopter Plant named after. M. L. Mil started in 1985. The modernized helicopter received the name Mi-28A in 1987. Testing of the modernized Mi-28A began in January 1988. They went well, and the following year the helicopter was first demonstrated at the Le Bourges Air Show in Paris and at an exhibition in Red Hill near London, where it enjoyed great interest among visitors. In the same year, the first experimental helicopter Mi-28 was officially presented for the first time in its homeland during the aviation festival in Tushino. In January 1991, the second Mi-28A, assembled by pilot production at the Moscow Helicopter Plant, joined the test program. In September 1993, during combined arms exercises near Gorokhovets, the helicopters brilliantly demonstrated their flight and combat qualities.

In April 1986, joint flights of the Mi-28A and Ka-50 took place at the Gorokhovets training ground under the state joint testing program (GST). The requirement is to detect 25 targets on the battlefield. The Mi-28A crew at low altitude detected all 25 targets without being detected. The Ka-50 pilot, at significantly higher altitudes, was able to detect only two targets.

The first prototype of the Mi-28N was rolled out of the assembly shop on August 16, 1996, and on November 14, 1996 the helicopter took off for the first time.

State joint tests of the experimental Mi-28N combat helicopter began in May 2005. The GSI program provided for a large volume of ground work and test flights, which provided the opportunity for a comprehensive assessment of the combat properties of the helicopter. In order to resolve operational issues that arise during the GSI and require a quick and competent solution, the state commission for the GSI of the experimental Mi-28N combat helicopter was headed directly by the Commander-in-Chief of the Air Force.

At the end of December 2005, the first production helicopter of the new generation Mi-28N was lifted at the enterprise.

The first stage of the Mi-28N GSI was completed in 2007.

In accordance with the decision of the Air Force Civil Code, GSI of the Mi-28N helicopter was carried out in two stages. As part of the first stage, a preliminary conclusion was issued on the possibility of producing an initial batch of helicopters. At the same time, by decisions of the Air Force command, the technical appearance of the Mi-28N helicopter was formed, ensuring that after the completion of the first stage of the GSI, the helicopter can carry out round-the-clock combat missions to destroy ground targets with the main set of weapons, and the second stage of the GSI - air targets using air-to-air missiles. , as well as the high survivability of the helicopter due to its equipment with electronic jamming equipment.

The Mi-28N GSI was completed on December 26, 2008. Based on the results of the GSI, it was established that in terms of flight performance, stability and controllability characteristics, the capabilities of the avionics complex, the range and accuracy of the weapons used, the Mi-28N generally complies with the requirements of the TTZ.

Mi-28N helicopter was put into service by order of the President of the Russian Federation on October 15, 2009

How the Mi-28 “Night Hunter” was created

The Mi-28N “Night Hunter” (according to the NATO codification Havoc, “Devastator”) is a Russian attack helicopter manufactured by PJSC Rostvertol, part of the Russian Helicopters holding company. It is a modern combat helicopter, the main purpose of which is to search and destroy enemy tanks, armored and unarmored vehicles, as well as their infantry on the battlefield; in addition, it can hit low-speed air targets. The helicopter can be used during the day and at night in both simple and adverse weather conditions.

The Mi-28N has been officially adopted by the Russian Ministry of Defense and is being actively supplied to the troops. According to information for 2022, the Russian Air Force has more than 90 Mi-28N helicopters. The combat vehicle is also in demand on the international market. At least 15 Mi-28NE helicopters are in service with the Iraqi army, and delivery of attack helicopters is underway to Algeria, which in March 2014 signed a contract for the supply of 42 Mi-28NE helicopters. Helicopters have already taken part in hostilities, Russian ones were used against terrorists, being part of the Aviation Group of the Russian Air Force in Syria, Iraqi helicopters were used in battles with terrorists of the “Islamic State” (IS, a terrorist organization banned in Russia) on the territory of Iraq, in particular, quite were widely used during Operation Fatah (offensive on Mosul).

The Mi-28 attack helicopter made its first flight 35 years ago, on November 10, 1982. Subsequently, the Mi-28N helicopter was created on its basis, which was put into service in 2009. Its serial production began in Russia in 2006 in Rostov-on-Don. According to the state weapons program, by 2022 the Russian army should receive about 200 Mi-28N helicopters.

Aerobatic team "Berkuts" on the Mi-28N

The Mi-28 helicopter is distinguished by outstanding flight performance characteristics. He is able to perform such aerobatic maneuvers as: Nesterov loop, barrel roll, Immelmann flip, sideways flight, backward flight. It is no coincidence that since 2012, Mi-28N helicopters have been used by the Russian Air Force aerobatic team “Berkuts”; the group performs flights on six combat helicopters of this type.

The history of the creation of this amazing helicopter dates back to 1976, when the Council of Ministers of the USSR adopted a resolution to begin work on a new attack helicopter, which in its combat effectiveness would be able to surpass the Soviet Mi-24 and the American Apache in service. The country's leading design bureaus, Kamova (Ka-50 Black Shark helicopter) and Mil (Mi-28 helicopter, general designer Mark Weinberg), presented their competition works. Unlike the Ka-50, the Mil helicopter was developed in accordance with the traditional concept of a two-seat single-rotor vehicle with a tail rotor. At the same time, there was a division of functions between the attack helicopter crew members: the navigator-operator and the pilot.

Hero of the Soviet Union test pilot Gurgen Karapetyan, who over the years of his work has mastered 39 types of helicopters, gliders and airplanes, and taking into account their modifications, more than a hundred different aircraft, told TASS journalists about interesting facts about the appearance of the helicopter and the first tests of the Mi-28. In total, he spent more than 5,500 hours in the air, flying on all types of helicopters created by the Mil Design Bureau, including the attack Mi-28. It was Mil Design Bureau test pilot Gurgen Karapetyan and test navigator Viktor Tsygankov who first took the new experimental helicopter into the air on November 10, 1982.

Gurgen Karapetyan recalls: “On that day, unfortunately, Leonid Ilyich Brezhnev died. But despite this, at 11 o’clock in the morning the helicopter hovered. However, at 12 o'clock flights were banned. During the first flight, we took off and hung in the air for 5 minutes. We rose first by one meter, then by five meters, moved left and right, forward and backward, performed turns at a low angular speed, and then landed.” According to the test pilot’s recollections, this flight did not leave any particularly vivid impressions. At the same time, the helicopter was quite stable and very sensitive to control. Later, in November-December 1982, during tests, pilots reached speeds of 60 km/h. After the first flights, all materials on them and the calculation materials of the Mil Design Bureau were submitted to the council of the USSR Ministry of Aviation Industry, after which approval was received to continue testing.

It is worth noting that at that time the Mi-28 seriously competed with the Kamov product. The Ka-50 helicopter took off in June 1982, and the Mi-28 took off only in November. As Gurgen Karapetyan recalls, before the first flight the transmission was destroyed. Therefore, until November, the design bureau carried out various modifications, and only at the end of autumn the helicopter was able to perform its first hover. By that time, the Kamov team was able to go far ahead, so KB Mil had to think about how to catch up.

A series of preliminary tests of the new Mi-28 attack helicopter continued from 1982 to 1985, they ran in parallel with tests of the Ka-50 helicopter. Ultimately, the Ministry of Defense decided that Kamov’s company won the competition, but Mil Design Bureau disagreed with this decision, being well aware that it’s easy to fly in a single-seat vehicle, but it’s more difficult to fight effectively. According to Karapetyan’s recollections, the tests of the Ka-50 helicopter at the Gorokhovets test site were carried out exactly the same as with the Mi-28. There was a nuance: once military crews flew the Ka-50 and Mi-28 at the same time. Their task was 25 targets. The crew on the Mi-28 helicopter found all the targets, but on the Ka-50 only one.

Mi-28A

The developers of the new attack helicopter Mi-28, as well as test pilots from the Mil design bureau, convinced the military leadership of the USSR that “a pilot at extremely low flight altitudes is not able to perform all functions at once: pilot a helicopter, search for targets, go around terrain and obstacles and hit targets." Gurgen Karapetyan explains that at altitudes of 5-15 meters, one pilot is not able to perform these tasks; this is possible at a flight altitude of 30-50 meters, but then the probability of his defeat increases to 95%.

Gurgen Karapetyan recalled another incident that occurred during his stay in Afghanistan in 1980 together with the general designer of the Mil Design Bureau. Then, at an altitude of 50 meters, a Mi-24 combat helicopter was shot down. “Either there was a very good sniper, or a stray bullet hit the pilot in the head. But the second pilot did not have time to react and the Mi-24 fell from a height of 50 meters and crashed,” says the test pilot. After returning to Moscow, appropriate modifications were made to the design of the new Mi-28 helicopter, including changes to the cabin geometry. At the same time, Karapetyan turned to the general designer with a proposal that the entire helicopter cabin be reserved: not only its lower part, but also the glass. Later tests, in which the cockpit of a Mi-28 helicopter was fired from a 20-mm Vulcan aircraft cannon (NATO's main cannon), demonstrated excellent security results.

The concept of creating a two-seat combat vehicle was also confirmed; this approach was absolutely correct. At that time, the Americans experienced a similar situation, recalls the test pilot of the Mil design bureau - materials appeared in the press everywhere in favor of the single-seat concept of an attack helicopter. Moreover, many articles were published in time for the meetings of the state commission in the USSR, about a month or two before it was held. All this influenced the progress of work. Only after testing at the Sikorsky company in 1989 in the USA did they write that in order to make an attack helicopter single-seat, it was necessary to automate 36 of its systems, and the cost of such automation was “golden”.

According to Karapetyan, in the process of creating a new helicopter, designers introduced various solutions and concepts designed to improve ergonomics. As an example, the test pilot notes: in order to start the engine, it was necessary to perform 144 operations on the Mi-24 helicopter, while on the new Mi-28 - only 18. The difference was significant. A large number of improvements were introduced on the Mi-28 that were going to be implemented on the Mi-24, but for one reason or another were never implemented. For example, the Mi-24 did not have night vision systems, while the Mi-28 became a 24-hour, all-weather combat helicopter. At the same time, detecting the helicopter itself at night is much more difficult than during the daytime.

The international debut of the Mi-28A helicopter took place in 1989. On June 8, the car was first demonstrated at the French air show in Le Bourget. The Soviet attack helicopter was the real star of the exhibition. At the same time, the first reaction of foreigners, according to Karapetyan’s recollections, was the following: “Oh, a copy of the American Apache!” He himself explained that the machines were similar in appearance, but it was wrong to talk about copying; people in the USSR and the USA simply thought in approximately the same direction when developing a combat vehicle. At the same time, when foreigners learned about the solutions and concepts that were embedded in the Mi-28, they were truly shocked. From Karapetyan’s point of view, the Apache and Mi-28 are completely different vehicles in terms of combat survivability and the comparison here is not in favor of the American. In the person of the Mi-28, our army received a very good helicopter, which in terms of its efficiency and combat survivability is now one of the best in the world, summarized the honored test pilot.

Currently, the development process of the Mi-28 combat helicopter continues. On October 12, 2016, the Mi-28NM helicopter took to the skies for the first time, which is a modernized version of the Mi-28N helicopter. Unlike the usual “Night Hunter”, in which the navigator-operator sits in the front cockpit and is limited in the capabilities of piloting the combat vehicle, in the new helicopter full control is implemented in both cockpits. The Mi-28NM helicopter received an overhead radar and a new sighting, flight and navigation system, and an improved radar station. It is assumed that the first batch of such helicopters may enter service with the troops as early as 2022.

Mi-28NM

Work on the creation of the Mi-28NM attack helicopter (product 296) started in 2009 as part of the Avangard-3 development work. The main objective of the work was to modernize the existing Mi-28N Night Hunter helicopter using new components, assemblies and systems. It was planned to improve the combat, flight and operational qualities of the helicopter by replacing a number of components. Also, part of the work on the project was related to simplifying the production of equipment by eliminating components, the supply of which may be associated with the occurrence of any problems.

When creating the modernized Mi-28N combat helicopter, the designers took full account of the experience of developing the combat training version of the Mi-28UB: a second control set was placed in the front cockpit of the modernized helicopter. In addition to this, the cockpit has also undergone modernization: the pilot-operator and commander will now receive out-of-the-cockpit information about the operation of all vehicle systems and the surrounding environment in a more accessible form and in a larger volume. This is intended to increase the situational awareness of the crew of the combat vehicle, which will facilitate interaction and help increase the speed of decision-making, especially in a difficult combat situation. The helicopter also received a new sighting, flight and navigation system, which received modern computing tools with increased performance. The crew cabin of the Mi-28NM helicopter is reliably armored, which should provide effective protection against armor-piercing bullets and shells of caliber up to 20 mm inclusive.

An improved overhead radar and increased capabilities in the use of modern high-precision weapons, including homing missiles, are also the calling cards of the Mi-28NM helicopter. The use of precision weapons can significantly reduce the time an attack helicopter spends in potentially dangerous situations. The advantages of the modernized vehicle also include good resistance to combat damage. This is achieved through the use of new design solutions and the latest materials. The design of the fuel system of the Mi-28NM helicopter eliminates the possibility of explosion or fire of fuel in the tanks, and the main rotor blades were made of composite materials. The blades allow you to safely complete the flight even if they are hit by 20-30 mm caliber projectiles.

Presentation of Mi-28UB combat training helicopters from the first batch. Rostov-on-Don, 10/19/2017 (c) Evgeny Baranov/Russian Helicopters JSC

In addition to the Mi-28NM, another new modification has been created - the Mi-28UB, a combat training helicopter with a dual control set and a failure simulation panel, which has retained all the functionality of an attack helicopter. The main difference between this model is precisely the presence of a dual control system, which allows you to pilot the combat vehicle both from the pilot’s cabin and from the operator’s cabin. This makes it possible to more effectively train and train military pilots who need to practice flying Night Stalkers. Also, in combat conditions, in case of possible emergency situations on board, a second crew member will be able to take control of the helicopter. The failure simulation console installed on the Mi-28UB allows the trained pilot to simulate various options for equipment failure in flight, which improves the trainee’s training in moments of crisis situations, and this will help save his life in the event of real malfunctions or accidents.

According to Vadim Barannikov, First Deputy Managing Director of Aviation, within the framework of a three-year contract signed with the Russian Ministry of Defense, for three years, starting in 2017, the military will receive up to 10 Mi-28UB combat training helicopters (thus, the army will be replenished with at least 30 such cars). These helicopters have already passed the entire range of factory tests. As the Ministry of Defense clarified, at the beginning of November 2022, the first two Mi-28UB helicopters with dual controls were accepted into the troops, and in the near future these machines will arrive at the 344th Army Aviation Center in Torzhok. According to the portal Aircraftcompare.com, the cost of one Mi-28UB is slightly higher than the cost of the Mi-28N and ranges from 16.8 to 18 million dollars.

Test pilot Gurgen Karapetyan considers the fact that the domestic Mi-28 combat helicopter, according to NATO codification, to have received the nickname “Devastator” at one time, is very accurate. The experience of the combat use of this combat vehicle in Syria demonstrates that the epithet chosen by the military of the North Atlantic Alliance is absolutely correct.

Sources of information: https://tass.ru/armiya-i-opk/4713899 https://www.russianhelicopters.aero https://www.airwar.ru/enc/ah/mi28nm.html Materials from open sources

Exploitation

In 2005, a long-term contract was signed for the supply of 67 Mi-28N helicopters until 2013.

In 2005, the Chief of the Russian General Staff, Army General Yuri Baluevsky, stated that the Ka-50 and Ka-52 helicopters are necessary for special forces units. Although in this case the main combat helicopter will be the Mi-28N “Night Hunter”.

In the second half of June 2006, two Mi-28Ns took part in command and staff exercises on the territory of the Republic of Belarus, called “Union Shield - 2006”. These were the first prototype OP-1 and the first pre-production 01-01 (tail number 32).

On September 7 in Rostov-on-Don, the Air Force Commander-in-Chief took part in a meeting of the state commission for conducting state tests of the Mi-28N at Rostvertol OJSC. The meeting participants summed up the results of the first stage of state testing of the Mi-28N and checked the readiness of military-industrial complex enterprises for mass production of the helicopter.

The act of accepting the Mi-28N into series will be signed by September 30, during which time the industry will eliminate the shortcomings identified during the first stage of state tests.

The first 4 production Mi-28Ns arrived at the Torzhok Center for Combat Use and Retraining of Army Aviation Flight Personnel in 2008. On January 22, 2008, the first two helicopters arrived at the Torzhok Pulp and Paper Plant and PLS AA.

In 2009-2011, the Russian Air Force will receive 27 Mi-28N helicopters. The first production helicopters are supplied to units of the 4th Air Force and Air Defense Army.

In 2009-2010, at airbase 6971 (487th separate helicopter regiment) near Budyonnovsk, the first helicopter squadron of 16 serial Mi-28Ns was formed.

In October 2010, deliveries began to the 6974th air base (55th separate helicopter regiment).

In 2010, 12 Mi-28N were delivered. In total, by the end of 2010, 38 helicopters were delivered to the Russian Ministry of Defense. In 2010, a second contract was signed for the purchase of another 30 Mi-28N with delivery by 2014.

Thus, as of the end of 2010, in total, the Ministry of Defense of the Russian Federation concluded contracts for the supply of 97 helicopters until 2015.

As of 2011, the MTBF of the Mi-28N was 8.1 hours versus 13.9 for the Mi-24. In 2011, 14 Mi-28N were delivered.

From 2001 to 2012, 63 Mi-28N were delivered

In 2012, 14 Mi-28 were delivered to the Russian Defense Ministry

Modifications

The first modification of the Mi-28A did not enter the series, since the helicopter did not meet modern requirements for round-the-clock operation, and was returned for modification.

In 2006, a modification of the Mi-28N (“Night Hunter”) was launched into mass production, differing from the original in a more modern avionics. The “Tor” complex produced by OJSC “Krasnogorsk Plant named after. S. A. Zverev." To view the front lower hemisphere, TOES521 (turret-optical-electronic system) produced by the Federal State Unitary Enterprise "Ural Optical-Mechanical Plant" is used. The new OPS on the Mi-28N, together with a night vision station, ensures the search for point moving and group targets at a distance of up to 10 km.

Model	Description
Mi-28	Prototype (“product 280”). Experimental, 2 vehicles (No. 012 and 022). With PrPNK-28 (daytime OPS with TV channel "Saturn", submersible container equipment "Mercury")
Mi-28A	Modernized (“product 286”). Differs in TV3-117, NV engines with fiberglass spars, X-shaped RV 286-1, design of ECU engines, equipment composition, 2 cars (No. 032, 042)
Mi-28L	Licensed version of the Mi-28A (project). Developed in 1990 for Iraq
Mi-28N	Night based on Mi-28A. With main gearbox VR-29 instead of VR-28
Mi-28NE	Export modification of the Mi-28N helicopter
Mi-28NM	Mi-28N modernization project. According to some reports, it is planned to install a standard N025 over-the-barrel radar
Mi-28UB	Combat training modification for the Russian Air Force

On-board radio-electronic equipment complex

The Mi-28N avionics complex, in its technical characteristics, meets the requirements for 5th generation aviation equipment. Main developer - FSPC "RPKB"

The Mi-28N avionics complex provides:

— automated distribution of goals within the group

— combat use of the helicopter around the clock and in difficult weather conditions;

— performing combat missions at extremely low altitudes;

— interaction with the group’s helicopters, air and ground command posts (CP), air controllers;

— joint (parallel) use of weapons by the pilot and operator;

— the ability to adapt new and already used ASPs;

— operation of helicopters at significant distances from airfields and bases through the use of the principle of equipment maintenance based on technical condition.

The main composition of the complex includes:

— a unified computing system that provides information processing via a single interface based on the Baguette-53 computer;

— cockpit information and control field based on multifunctional liquid crystal indicators MFI-10-6M and multifunctional console PS-7V using a video information recording device;

— navigation equipment consisting of a high-precision INS-2000 and a strapdown heading SBKV-2V-2 with integration with a satellite navigation system, a Doppler speed and drift meter (DISS) and an airborne signal system (SVS), a radio-technical long-range navigation system (RSDN);

— integrated system for detecting electronic and laser irradiation and a UV radiation direction finder;

— automatic control system (ACS);

— weapon control system;

- helmet-mounted target designation and display system;

— a surveillance and targeting station for detecting and recognizing objects, aiming, capturing and automatically tracking objects via television and thermal imaging channels. The composition includes: a line of sight stabilization system, an automatic target tracking system, an optical-television channel, a thermal imaging channel, a laser range finder;

— a pilot’s observation and aerobatic system with night vision goggles, designed for round-the-clock surveillance of the area, search and detection of objects (landmarks and obstacles). Composition: low-level television channel, thermal imaging channel, laser range finder;

— helicopter flight control system;

— on-board communications complex KSS-28N-1, provides automatic telecode data exchange with ground control points and other aircraft equipped with equipment that ensures counter-operation; long-range and short-range open and secret radio communication through a cryptographic protection product and an HF modem. The complex provides simultaneous operation (reception - transmission) via three communication channels, including two telephone channels and one telecode channel. Works in FRF and FRFC modes

The avionics also includes an ATT (automatic thermal television) of the Okhotnik family, developed by the Federal State Unitary Enterprise GRPZ. This product on the Mi-28N helicopter performs functions related to the intelligent processing of video images, as a result of which it becomes possible to see the background target picture in any weather conditions at any time of the day. For the first time among all Okhotnik models, the ATT implements a high-speed digital interface for transmitting video signals during vibrations and roll of the helicopter, and also provides automatic detection and tracking of targets.

The helicopter is also capable of reconnaissance and target designation of combat helicopters and aircraft.

MI-28N is equipped with the L-150-28 station (version L-150 (SPO)).

Application options for the Mi-28NE helicopter

Currently, the Mi-28NE is used to perform the following tasks:

• search and destruction of armored vehicles, single and group targets, artillery, military air defense systems

• combating low-speed enemy aircraft

• aerial reconnaissance and target designation when solving combat missions

• air support for ground forces on the battlefield and destruction of enemy personnel

• patrolling dangerous areas and combating enemy tactical airborne assaults

• training cadets of flight schools and improving the flight training of helicopter crews

Safety

If an emergency situation occurs or catastrophic destruction of the structure at an altitude of more than 100 m, first the propeller blades, wing consoles and doors of both cabins are shot off, then the forced attraction belts are cut with special cutters, special “ladders” are inflated - ballonets, which prevent the crew from touching the landing gear when leaving the gun is turned, and the crew leaves the car using parachutes.

In the same situation, but at an altitude of less than 100 m, the system of forced attraction of the belts is activated, reliably fixing the crew in the Pamir-K energy-absorbing chairs developed by the Zvezda Design Bureau. First, the impact energy is absorbed by the main landing gear, which, when deformed, absorbs it. Next, the seats come into play, which are capable of absorbing a vertical overload of 50-60 g to 15-17 g, providing injury safety to the pilot and navigator-operator.

bN BPEL NOEPYUZHKH "ASP B OSYARSHME" RNKEIN ON OPHVKHME NYKHANY B OKHKNRKHPNBYUMKHH MNVECH BAKKHGH GELKH YULEPKHYUMYAYU YUPLEIYYU YUBKHYUZHKH ONREPKYU LKHMHLSL OIRE SHCHY KHOYUFEI BEPRNKERNB "YuOYuV" I YAHYARELYULH MNVMNTSN BKhDEMH. xMREPEYAMN, VRN 98% OPHLEMEMKH NTSMEBSHU YAPEDYARB ASHKN B OPNYARSHU LERENSYAKNBKHYU. EYE PUMEE AKEYARYE GYUDSLUMMYU MNVMYU NOEPYUZHH ON NYABNANFDEMHCH YAKSFYUYKHU YLEPHYUMAYNTSN ONYANKEYARBU B RETSEPUME, GUUBYUVEMMSHU B YUVEYARBE GYUKNFMKHYNB, YANPBYU KYUYAE HG-GYU YARNKYMNBEMHЪ MU GELKE YAPYUGS MEYAYNKEIKHU RPYUMYAONPRMSHU BEPRNKERNB. x, MUYNMEZH, B VEVEME YUBHYUZHH OPHLEMKYUYAE ONVRH HYAYKCHVHREKEMN DMEL X B YAPYUBMHREKEMN OPNYARSHU LERENSYAKNBHYU. TsNPEIN BYAONLKHMURE YABNDYKH YANNAYEMKHI: “dMEL TEDEPYUKEMSHE BNIYAYU AEPSR YAHRSYUZHCH OND YABNI YNMRPNKE, YU MNVECH OPYURKHVEYAYKH MY BYAEI REPPHRNPHKH UNGIMKHVYUCHR MEGUYNMMSHE B NNPSFEMMSHE TNPPLKHPNBYUMKH...”

"ip" SFE YANNAYYUK N RNL, VRN nya KHLEMKH l.k.lHKЪ PYUGPYUANRYUKN LNDHTHYUZHHCH BEPRNKERYU lH-28 - lH-28m

, NYAMNBMNE NRKHVHE YNRNPNTSN - YPSTSKNYASRNVMNE ANEBNE OPHLEMEMHE, B RNL VHYAKE B YUAYANKCHRMNI RELMNRE, YNTSDU NRYASRYARBSER DUFE YAKYUAYU ONDYABERYU NR GBEGD, B KCHASHU LERENSYA KNBHYU! NOSHR OPHLEMEMKH YUBKHYUZHKH B BNMYUU BRNPNI ONKNBKHMSH MSHMEMETSN BEYU ONYUGYUK, VRN VYUYE BYAETSN ONPUFEMKHE ANEBNTSN BEPRNKERYU MUGELMSHLH YAPEDYARBYULH obn NYASYYARBKERYA OPH BHG SÜKEMNL YNMRÜYRE. schRN NGMYUVYUER, VRN BEPRNKER DNAFEM YANBEPIURE ONKER H BEYARKH ANEBSE DEYARBKH MY LYUKSHU BSHYANRYUU. xMYUVE BEPNЪRMNYARE ETSN ONPUFEMHЪ NVEME BSHYANYU. nM DNAFEM NTSKHAYURE YAYKYUDYKH LEYARMNYARKH, LYuYAYKHPPNBUREYA B SYEKEYU KH B PSYAKYUU PAY, OPH MENAUNDHLNYARKH BPELEMMN YAYPSHBUREYAJ MU NOSYE KEYYU KH OPH SCHRNL - OPNBNDHRE MEN AUNDHLSHE ANEBSHE NOYYUZHHH YUBRNMNLMN XKH B TsPSOOE. b NDMNLEYARMNI LYUHME BSHONKMHRE RUYHE GYUDYUVKH OPH YANBPELEMMNL SPNBME REUMHYH YPYUIME YAKNFMN.

BEDSYKHE BEPRNKERSH THPLSH yayu "LYuYDNMMEKK-dSTSKYUYA", "aEKK" X "YAHYNPYAYKHI" YARPNHKH KERUCHYKHE KYUANPURNPHKH KH OSHRYUKHYAE YADEKURE NDMNLEYARMSHI BEPRNKER. MN DUFE OPH SPNBME PYUGBHRKH SHCHKEIRPNMHYH MHVETSN OSRMNTSN ME ONKSVHKNYAE. yuLEPHYUMYAYHE THPLSH ON PUGMSHL MUOPYUBKEMKHLH OPNBEKH HYAYAKEDNBYUMH (GURPUURKHKH NYNKN 1.5 LKPD. DNAKYUPNB) ON NZHEMYE YANGDYUMKH NDMNLEYARMNTSN BEPRNKERYU X NDMNGM YUVMN OPHKKH Y BSHBNDS, VRN NDMNLEYARMYU ANEBYU LYUKHMY MEZHEKEYANNAPUGMY. oPH DBSULEYARMNI YAUELE NDHM KERVKHY OKHKNRKHPSER KH NAEYAOEVKHBUER MKHGYNBSHYANRMSHI ONKER, SUND NR YURYUSCHYKH YAPEDYARB KH R.D. bRNPNI - PUANRUER ON ZHEKKL: NAMYUPSFKHBUER KH, PUYAONGMYUER, OPKHZHEKKHBUERYAK X OPNKHGBNDHR YURYUS, B RNL VHYAKE X MESOPIUBKELSHL NPSFHEL. OPH MENAUNDHLNYARKH NM LNFER OPKHZHEKHBUREYA KH YURYUINBURE, ME BUND B YNMRYUIR I ZHEKECH DUFE (RUYKHE OPNTsPYULLSH EYARE) YARPEK'RE "HG-GYU STSCYU". mNBSHI ANEBNI BEPRNKER nya lHK YANGDYUM MU AYUGE YAYULNTSN LNYNTSN YANBPLEMMNTSN ANEBNTSN lH-28. nDMMUYN YAUNDYARBN S MKHU RNKEIN BMEMEEE. “mYUVKHMYU” ONKMNYARECH KHGLEMHKYUYAE. oNLHLN SMKHYUKEMNTSN SHKEIRPNMMNTSN NANPSDNBYUMKH, LNDEPMKHGHPNBYUMSH LMNCHE YNMYARPSYRKHBMSHE SGKSH H YAKHYARELSH, SYARYUMNBKEM MNBSHI TSKYUBMSHI PEDSYRNP. yTsPETSYURSH BEPRNKERYU SIAOOEMN OPNKKH BYAYARNPNMMHE HYAOSHRYUMKH. b RN FE BPEL LYUKHMYU YANUPYUMHKYU BYAE DNYARNKHMYARBU lH-28, B RNL VHYAKE LNYMNE BNNPSFEMKHE X APNMHPNBYUMKHE.

GDEYAE UNREKNYAE ASH YADEKURE MEINRNNPNE NRYARSOKEMKHE. b YABGH I MENAUNDHLNYARECH NAMNBKEMKH OYUPYU BHMRNYPSHKSHU LYUHM bbya bBEZHHH ASHK OPNBEdem YNMYSPYA. Bemmshekh Khg Byaetuyuyu Ouupyu Bemmsh Beprnkernb Lhpyu Bshapyukh DBU: Yulephyamyyakhi "Yuuv" x LX-28u, nyabemshi b opnhgbndyarbe Mu Pnyarnbyinl Beprnkernamnl Gubnde. REMDEPMSHE HYAOSHRYUMKH OPNBNDHKHKHYAE B YAEMRYAPE-NYRJAPE 1995 Ts. ON LMEMKHCH UBEDNB, MYU LH-28, YNRNPSHHI NMH ASHYARPN NYABNHKH, AKYUTSNDYUP ANKEE LLYNLS APNMHPNBYUMKHCH H ANKEE OPNDSLUMMNNI YNMYARPSYZHKH HLEER KSVICH BSHFKHBUELNYARE. ETSN OPYURKHVEYAYH ME LNTSKKH GUYAEVE PYUDYUPSH EBEDYAYNI obn, YUMYUKNTSKHVMSHE murn, EYAKH ONKER OPNHYAUNDHK MU BSHIANRYU LEMEE 20 L. YAKHARELYU MYUBEDEMH PUYER S lH-28 RYUYU, VRN OPIURKHVEYAYKH MEKEG YANGDURE ONLEUKH. bBEDSH YAVKHRYUCHR MUYS LYUHMS OEPYAOEIRKHBMNI X OPHNPHRERRMNI. YaETsNDM UBEDSH NRPYUAYURSHBUCHR YNMZHEOZHCH NYAMYUYEMH lH-28 YABNEI YUBKHNMKHYNI, YU LSH DEKUEL KERYUREKEMSHI YOOYUPYUR. RYUY UBEDSH PEYUCHR NVEME BYUFMSCH DK YEAA GYUDYUVS - YANGDYUMKHE PUANVKHU LEYAR. lSH ONDDEPFKHBUEL ShchRS KhDECH YNNNOYUZHHH DK BEPRNKERNB, YNRNPSHE ASDSR B BEDYAYNI KH DPSTSKHU YAYUMDKHMYUBYAYKHU YUPLKHU. x VRN NYANAEMMN BYUFMN, lH-28 ONVRH B 2 PYUGY DEJEBKE, VEL "YOYUV". yNMYSPYA OPNDNKFUERYA.

MU "YOYUVE" ​​SYARYUMNBKEMN SHTTTEIRKHBMNE SHKEIRPNMMNE NANPSDNBUMHE H, OPEFDE BYAETSN, YAHYARELYU MNVMNTSN BHDEMKH, YUY DK KERVKHYU-NOYURNPYU, RYU KH DK YNLUMDHPYU. MN UBEDSH BHDHLN, GMYUKH N RNL, VRN OPH OEPBNL FE LYuYAYANBNL MNVMNL OPHLEMEMHH "YuOYUVEI" B xPYUYE MEYAYNKEIN LYUHM SHRNTSN RHOYU PUGAKHKNYAE, BPEGYUBHYAE B OYAVYUM SHE AYUPYUMSH HKKH YARNKYMSBHYAE LEFDS YANANI B BNGDSUE. nVEBKHDMN, YAKHYARELYU MNVMNTSN BKhDEMHЪ ME NAEYAOEVKHBUER SHCHYHOYUFYUL ONKMNI AEGNOYUMNYARKH. ONSHRNLS BYAE YAKEDER GU MNBNI LNDKHTHYUZHHEI AH-64D "KNMTSANS-YuOYuV", YNRNPNTsN LNFMN ASDER I ONKMSHL NYAMNBYUMHEL MYUGBYURE MNVMSHL BEPRNKERNL. ETSN NRKHVHREKEMYU NYNAEMMNYARE - MYUDBRSKNVMSHI PYUDYUP LHKKHLERPNBNTSN DHYUOYUGNMY ONBSHYEMMNI PYUGPEYUCHYE YAONYANAMNYARH "kNMTSANS". schRNR YNLOKEYA ONGBNKYER, ONLHLN MNVMNI NUNRSH, BSHONKMRE TSMYZHKH PUGBEDSHBUREKEMSHE X KHMTNPLYUZHNMMSHE, ONDNAMSH REL, YNRNPSH BSHONKMCHR YAYULNKERSH "YUBYA". lH-28m - SMKHYUKEMNE ЪBKEMKHE B LHPNBNL BEPRNKERNYARPNEMHH. ShchRYu SMKHYUKEMNYARE NOPEDEKERYA PJDNL NAYARNREKEYARB, YNRNPSHE BPJD KH YNTSDU-KHAN ONBRNPRYA.

bN-OEPBSHU, lH-28m - ShRN KHMKHZHYURKHBMYU PUGPYUANRYU lNYAYNBYAYNTSN BEPRNKERMSHL GYUBNDNL HL. OK. lХКЪ MU AYUGE ANEBNTSN BEPRNKERYU lH-28 (AYUGNBSHY BEPRNKER KHMNTSDU NANGMYUVYUCHR lH-28yu). bSHYURYU HG YAANPNVMNTSN ZHEYU OEPBNTSN NOSHRMNTSN SHYGELOKOPYU YANYARNKYUYAE 16 YUBTSSYARYU 1996 TSNDYU, 14 MNAP 1996 TSNDYu SCHRNR BEPRNKER BOEPBSHE ONDMЪKYA B BNGD SU.. ONYAKE OEPEBNDYU BEPRNKERNB HG bbya B ONDPYUGDEKEMKH YUBHYUZHHH YASUNOSRMSHU BNIYAY LHKEBZHSH PUGPYUANRYUKH YNMZHEOZHCH ANEBNTSN BEPRNKERYU DK SCHRNTSN PNDYU BNIYAY. oPEFDE VEL NTNPLKHRE REUMHVEYAYNE GYUDYUMKHE MU lH-28m, B REVEMKHE MEYAYNKEIKHU KER YAOEZHYUKHYARSH lbg YANBLEYARMN I KHMYARKHRSRRYULH lHMKHYAREPYARBU NANPNMSH TNPPLKHPNBUKH NAKHY SCHRNTS N BEPRNKERYU. yaoezhkhtkhveyaihe nyanaemnyarkh yasunosrmshu BNIYAY (PYUANRYU B KCHANE BPEL YASRNY, B OPNYARSHU KH YAKNFMSHU LERENSYAKNBKHU, B NRPSHBE NR YUSCHPNDPNLNB X YARYUZHNMYUPMSHU AYUG, YANBLEYARKHL NYARE TsNPCHVE-YALYUGNVMSHU LYUREPHYUKNB, ANEOPOHOYUYANB, YAPEDYARB YABGKH SOPIUBKEMKH, OPNYARNRYU SHYAOXYURYUZHKH OPHLEMYELNI REUMKHYKH) ONRPEANBYUKH YANNRBERYARBSCHYKHU YU VEYARB NR lH-28m . eYAREYARBEMMN, VRN, YATNPLSKHPNBYUB YARNKE YAOEZHTHTHVEYAYKHE RPEANBYUMKH, MSFMN ASHKN MUIRKH REUMKHVEYAYKHE PEEMKH DK KHU DNYARKHFEMKH. x GDEYAE ONЪBHKYUYAE BRNPYU NYNAEMMNYARE SCHRNI PYUGPYUANRYKH. ONHYAYH YANBOYUKH ON BPELEMH I YNMBEPYAHEY. lMNTSKHE YPSOMSHE PUGPYUANRVKHYKH, BSHONKMЪBKHE B NYAMNBMNL GYUYUGSH PUYERMN-YNYALKHVEYAYNTSN YNLOKEYYAYU H KHLECHYKHE YYULSHE BSHYANYKHE REUMNKNTSKHVEYAYHE GYUDEKSH, YARYUKH HYAOSHR SHBURE RPSDMNYARKH I GYUYUGYULH X THMYUMYAHPNBYUMKHEL. lHKEBJSH SHCHRHL X BNYAONKEGNBYUKHYAE, VRNASH HYAONKEGNBURE SHCHRKH REUMNKNTSXX X GYUDEKSH.

aSHKN YYAMN, VRN YARYUBKHE SFE NASHVMSHLH NVYKH MNVMNTsN BKhDEMHЪ, REOKNBKHGNPSH, REKEBKHDEMKHE KNYURNPSH LYUKNBSHYANRMNTsN ONKERYU GYUDYUVS ME PEUR. mSFMN YANGDUBURE ME RNKEIN MNBNE NANPSDNBYUMKHE, MN X RYUY ETSN YAYNLAKHMHPNBURE, VRNASH ONKSVKhRE BSHYANYNHMREKKEYRSYUKEMSCH LYUHMS. Gyumkya Shkrhl Tshbkh Khkeyumnbhv Dfumzdfyubyu, Dnirnp Reumhweyu Mussi, Opteyayanp - Tscobmshi Yinmyarnpsyarnp Operarpnkhremnsn Ynmyarpsyrnpyrnpyintsn ACHPN. MUOPYUBKEMHEL, YNRNPNE NAEYAOEVHKN PEEMKHE SHRNI OPNAKELSH, ASHKYU TSKNAYUKEMYU KHMRETSPUZHKH ANPRNBNTSN NANPSDNBYUMKH. YaETsNDM BYAE NANPSDNBYUMHE lH-28m NAZEDHMEMN B EDKHMSHI YNLOKEYA, GYU YNRNPSHHI NRBEVUER NDHM PUGPYUANRVKHY. b REUMHVEYAYNL YYAOEYRE KHMRETSPUZHKH GYURPNMSKYu NPTSYUMKHGYUZHCH BGYUHLNDEYARBKH, SOPYUBKEMKHE, KHMDHYUZHCH, YNMRPNKE, ONDTsNRNBYS Y BSHKERS.

BYAE NPTsYUMSH SOPYUBKEMKH ANPRNBSHL NANPSDNBYUMHEL KHMRETSPHPNBUMSH B EDHMSCH SOPYUBKCHYSCH YAHYARELS, VRN ONGBNKKHKN YANYPYURKHRE KHU VHYAKN DN PUGSLMNTSN LKHMHLSLYU KH PUGLEYARKH RE B NRMNYAHREKEMN MEANKEHU YUAHMYU KERVKHYU H URSPLUMYU-NOYURNPYU. BYAE REISYKHE OYUPYULERPSH, YNRNPSHE MENAUNDHLN KHMDHZHHPNBYURE BSHBNDRYAJ MU KHMDHYUZHCH ONYAPEDYARBNL YAHYARELSH NRNAPYUFEMHJ KHMTNPLYUZHHH, YANYARNYEI HG EYARKH LMNTsNPE FHLMSHU FHDYNYPHYARYUKKHVEYAYHU KHMDHYURNPNB - OH RPH B YUFDNI YUAHME. yPNLE RNTS, S YUFDNTsN XG VKEMNB SHCHYHOYUFYU KHLERYA TsPSOOYU PEGEPBMSHU OPKHANPNB MU YAKSVIUI YUBYUPHIMSHU YAHRSYUZHKHI. mu BEPRNKERE OPHLEMEMYU EDKHMYU BSHVHYAKHREKEMYU YAPEDYU, B YANYARYUBE RPEU ZHEMRPYUKEMSHU azhbl X ZHEKNTSN PJDU OEPKHTEPHIMSHU, YANBLEYARKHLSHU I IBM PC, VRN PEGYN SOPNYYUER PUGPYUANR YS ANPRNBNTSN OPNTsPYULLMNTsN NAEYAOEVEMKH. b YNLOKEYA BUNDYR YANBPELEMMSHE ZHHTPNBSHE BSHVHYAKHREKEMSHE LYUKHMSH I NRYPSHRNI YUPUHRREIRSPNI, YNRNPYU ONGBNKYER MYUPYYKHBURE TSMYZHHH X BYKYUDSHBURE KCANI NAZEL KHMREKKEY RYU OPH ONEBKEMHH MNBSHU GYUDYUV XKH OPH YUDYUORYUZHHH SFE GYUKNFEMMSHU GYUDYUV Y MNBSHL YNMYPERMSHL SYAKNBHJL. yPNLE RNTsN, VRNASH OKHKNRSH LNTSKH PUANRYURE SHTTEYRKHBMN KH AEG SRNLKEMKH, REL ANKEE B MNVMSHU SYAKNBKHU, YANGDYUM YANBPELEMMSHI YNLOKEYA KHMDHYURNPNB, ME DYUCHYHU YURKH BMNTsN HGKSVEMKH. YNLONMNBIYU YUAKHMSH MNBUYU, BSHONKMEMY I VERNLE ONYAKEDMKHU DAYARKHFEMKHI SCHPTSNMNLHYH.

YaBGH B RUYNL YNLOKEYYAE YADEKYUMSH MU YANBPELEMMSHU LSKERHOKEYYAMSHU YUMYUKYUU HMTNPLYUZHNMMNTSN NALEMYU. schRNR YARYUMDYUPR KHLEER YUMYUKNTS B YARPUMYUU murn. YAKEDNBUREKEMN, YOOOOYUPYURSPYU, SDNBKERBNP'CHYYU RPEANBYUMHL DYUMMNTSN YARYUMDYUPRYU, ONGBNKYER YANEDKHMYRE KCHANE NANPSDNBYUMHE B KCHANL PYUZHNMYUKEMNL YANVERYUMXX X B OPNZHE YAYAYE NRPYUANRYKH BEPRNKERYU ONDYKCHVYURE MNBSHE YNLONMEMRSH, MYUNDYKHEYAY MU ANKEE YANBPELEMMNL SPNBME. MU lH-28m YARNHR YANBPELEMMYU KHMEPZHYUKEMYU YAHYARELYU, YNRNPYU YAONYANAMY OPH KCHASHU LYUMEBPUU NOPEDEKRE OPNYARPUMYARBEMMSHE YNNPDHMYURSH BEPRNKERYU KH BSDUBURE MENAU NDHLSCH KHMTNPLYUZHCH KERVHYS X YNLYUMDSH MU SOPYUBKYCHYKHE NPTSYUMSH. NORHVEYAYHE, hy - REOKNBKHGKHNMMSHE DYURVKHYKH MYUDBRSKNVMSHI ANPRNBNI KNYURNP ONGBNKKCHR BKhDERE, ONLHLN BNGDSMSHU JACKEYS, BOEPEDH KEFYUYKHE OPEORYARBKH, BYKCHVYU Kommersant DEPEBE X KHMXX SHKEYRPNOPEDIUV. YAHYARELYU YUPRNTSPYUTHVEYAYNI HMTNPLYUZHHH, HLECHYU AYUMY ZHTPNBSHU DUMMSHU N PEKEETE PUINMU ANEBSHU DEYARBKHI I BSHYANINI YAREOEMECH PYUGPEEMKH, TNPLKHPSER RPEULEPMNE HGNAPUFEEMKHE SVIYARYU, B YNRNPNL MUUNDHRYA BEPRNKER.

хMRETSPKHPNBUMMSHYYNLOKEYA ANPRNBNTSN NANPSDNBYUMKH (hyan) lH-28m OPH PEYEMKH ANEBSHU GYUDYUV NAEYAOEVKHBUER OKHKNRKHPNBYUMKHE I NTSKHAYUMHEL PEKETYU LEYARMNYARKH YUY B PSVM NL, RYU H B YUBRNLYURHVEYAINL PEFHLE. MU BEPRNKERE B YUPNNAPYUGMNL NAREYUREKE MYD BRSKYNI MEYASYYETSN BKHMRYU SYARYUMNBKEMYU LMNTsNTSMYZHNMYUKEMYU apkya "YuPAYUKER" OPNHGBNDYARBU mkhhp "tyUGNRPNM".

nMU NAEYAOEVKHBUER BSHDYUVS KHMTNPLYUZHKH N OPEORYARBKHU, BYKCHVYU NRDEKEMN YARNYYKHE DEPEBE KH OPNBNDYU KHMKHI SHKEIRPNOPEDIUV, DEKYU BNGLNFMSHL YPSTSKNYASRNVMSHI ONKER MU OPEDEKEMN LYUKNI BSHIANRE 5 - 15 LERPNB DUFE B YAKNFMSHU LERENSYAKNBKHU. rNI FE ZHEKH YAKSFYUR NVYKH MNVMNTSN BKhDEMHЪ KH OHKNRYUFMYU REOKNBKHGHNMMYU YARYUMZHKH, YNRNPYU LNFER DUBURE KHMTNPLYUZHCH YUY KHMTPYUYYUMNE "NYMN B MNVE" BOEPEDH ON YSPYAS HKKH B KCHANL MYUPYUBKEMKHKH, NANGMYUVEMMNL ONBNNPNRNL TsNKNBSH KERVKHYU, ONKSVYU ZHEKESYUGYUMKHE NR MYUKELMNI YAKHYARELSH KKH ANPRNBNTSN YNLOECHREPYU.

MU BEPRNKERE SYARYUMNBKEMYU RUYFE YAKHARELYU YUPRNTSPYUTHVEYAYNI HMTNPLYUZHH I BSHYANYNI YAREOEMECH PYUGPEEEMKH X AYUMYNL ZHTPNBSHU DUMMSHU N PEKEETE LEYARMNYARKH B PUINME ANEBSHU DEIA RBHI. bSHVHYAKHREKEMYA YAHYARELYU LNFER TNPLHPNBYURE MU NYAMNBE SHRKHU DYUMMSHU RPEULEPMNE HGNAPIUFEMHE SVIYARYU LEYARMNYARKH, MU YNRNPNL MYUNDHRYA BEPRNKER, YU SHRN KETSIN SRN VMHRE I ONLNYECH YAOSRMHYNBNI MYUBKHTSYUZHHH, YAYNLOKEYAKHPNBUMMNI I KHMEPZHHYUKEMNI. BYAE LMNTSNNAPYUGHE HMTNPLYUZHHH OPEDYARYUBKERYAK KERVHYS X URSPLYUMS-NOEPURNPS MU ZHBERMSHU FHDYNYPHYARYUKKKHVEYAYHU DHYAOKEYU, SYARYUMNBKEMMSHU ON RPH B OEPEDMEI X GYUDMEI YUAHMYUU.

schKEIRPNMMNE NANPSDNBYUMHE BYKCHVUER B YAAЪ RUYFE YAHYARELS NPHEMRYUZHHH OH THGHVEYAYHL ONKL GELKH, X YNLOKEYA YAPEDYARB YABGKH MYUDBRSKNVMSCH pkya YPSTSNBNTsN NAGNPYu "yuPAYUK" ER". pkya NAEYAOEVHBUER BEPRNKERS BEYARKH ONHYAY ZHEKEY, PUANRYU BLEYARE I Nov "pNRNP" B NASHVMNL PEFHLE. bePRNKER LNFER OPNKHGBNDHRE ONKHYAY ZHEKEY, SIPSHBUYAE B YAYKYUDYUU LEYARMNYARKH KKH GYU DEPEBEILKH, BSHYARYUBKHB KH-GYU SYPSHRKH RNKEYN YABNCH "LUYYS". b SCHRNL YAKSVUE DNYURRNVMN RNNKEIN HYAONKEGNBYUMHE pkya. NOPEDEKKHB ZHEKH X XU RHO, PUYAOPEDEKKHB XU ON MENAUNDHLNYARKH LEFDS BEPRNKERYULH TsPSOOSH, BSHAPYUB NAZEIR DK YURYUYKH, BEPRNKER SCHMEPTsKHVMN BSHUNDHR KH GYUYUDSH X "NAPYUAYURSHBUER" ZHEKH YAPED YARBYULKH ONPUFEHMKH KKH MYUBNDHR SDYUPMSCH YUBHYUZHKH CH KKH DPSTSKHE BEPRNKERSH TsPSOOSH. yPNLE RNCN pkya lH-28m B NRKHVHE NR pkya AH-64D “Longbow” YAONYANAMYU PEYURE OHKNRYUFMN-MYUBKHTSYUZHNMMSHE GYUDYUVH.

YYUFDNE HG OEPEVHYAKEMMSHU YAPEDYARB LNFER HYAONKEGNBUREYYUBRNMNLMN. NDMMUYN B YUVEYARBE NYAMNBMNTSN PEFKHLYU HYAONKEGSERYA YAHMREG YUPRNTSPYUTHVEYAYNI, REOKNBKHGKHNMMNI KH PUDHNKNYUZHNMMNI KHMTNPLYUZHHH I BSBNDNNL MU DHYAOKEY RPEULEPMNTSN KHGNA PUFEMHЪ LEYARMNYARKH DHPEIRNPHEI KHMTNPLYUZHKH B SDNAMNL DK KERVKHYU BHDE. rNVMNNYARMSHE UYUPYUREPHYARKHYH YOOYUPYURSPSH DNAFMSH, ON PYYAVERYUL, NAEYAOEVHRE SYAKNBKH AEGNOYUYAMNTSN OKHKNRKHPNBUMHYU MU OPEDEKEMN LYUKSHU BSHYANRYUU. dK ONKHYAYU, NAMYUPSFEMKH X PYYAONGMYUBYUMKH ZHEKEY PUGPYUANRYUMYU MNBEIYU NAGNPMN-OPKHZHEKEMYYARYUMZHKH I NORHVEYAYHL, REKEBKHGHNMMSHL, REOKNBKHGKHNMMSHL X KYUGEPMSH L YUMYUKYULH MYAKCHDEMH. BYAE YUMYUKSH (GYU HYAYKCHVEMKHEL NORHVEYAYNTSN) HLECHR BNGLNFMNYARE ZHHTPNBNTSN OPEDIARYUBKEMKH KHMTNPLYUZHH I BSHDUVEI EE MU SHYPYUM H, B ZHHTPNBNL BHDE, B YAKHYARELS YUBRNLYURHGYU JXX PUYAONGMYUBYUMH ZHEKEY. BYA NANAYEMMYU KHMTNPLYUZHKH ONYARSOYUER MU KHMDHYURNPSH LRSPLUMYU-NOYURNPYU, YNRNPSHY KH OPHMHLUER NYNMVYUREKEMNE PEEMHE. YaBGMNE NANPSDNBYUMHE NAEYAOEVKHBUER YABGE I KCHASHLH YNLYUMDMSHLH OSMYRYULH YASUNOSRMSHU BNIYAY (Yab), OEPEDYUVS KHMTNPLYUZHHH MU MHU, YU RUYFE LEFDS BEPRNKERYULH B TsPSOOE X DPSTSHL ONRPEAKHREKIL, PYYAONKYUTSIUCHYHL MENAUNDHLSHL OPHELMSHL NANPSDNBYUMKHEL. YANNRBERYARBEMMN BEPRNKER HLEER YOOOYUPYURSPS DK ONKSVEMKH BMEMETSN ZHEKESYUGYUMKH NR YNLYUMDNBYUMKH. BYAE ShRN B YNLOKEYAE ONGBNKYER LYUHME PUANRYURE MU LYUKSHU BSHIANRYUU 5-15 L, B ANEBSHU ONP'DYUU, OPNBNDHRE URSPPLNBSHHE NOYUPYUZHHH I ONYUDYNI MU OPNLEFSRNVMSHU WINDOWS YUU, PEYURE ANEBSHE GYUDYUVKH, YARPEK'RE YUY ASH HG-GYU STSCYU, ME BUND B OPLNI YNMRYUYR I ZHEKECH KH ME ONDBEPTSYU BEPRNKER PHYAYS SMHVRNFEMKH.

aKYUTSNDYUP MYUKHVHCH MYUDBRSKNVMNI pkya, SHYHOYUFS lH-28m ME NAYGYUREKEMN "ONYUGSHBURE" BEYAE BEPRNKER OPNRKHBMKHYS, DNYARYURNVMN BSHYARYUBHRE "LUYYS" HG EYAREYARBEMM NTsN SYPSHRKH-GYUAYUDSH H NYASYYARBKRE ONHYAY ZHEKEY, OPHVEL ME RNKEIN DK YAYEA, YU DK BYAEU KERYUREKEMSHU YOOYUPYURNB, SVIYARBSCHYKHU B YURYUYE. NOPEDEKHB NAZEYRSH DK SDYUPYU, lH-28m BSHONKMYER SHMEPTsKHVMSHY "ONDYAYNY" KH "NAPYUAYURSHBUER" KH YABEPUGBSYNBSHLH SOYUBKELSHLH PUYERYULH "YURYUYU", I PUDHNYNLUMDMNI YAHYARE LNI MYUBEDEMKH. ShchRYu YAHYARELYU NAKYUDUER MUKHBSHYAYEI ONLEUNGYYYYYYEMNYARECH, YU PYUYERYU OPNAKHBUYER RYUMINBSCH APNMCH I "DHMYULKHVEYAYNI" GYUYHRNI BYAU RYUMYNB, MYUNDYKHYYU MY BNNPSFEMHH YANB PELEMMSHU YUPLKHI. DYUKEMNYARE ONPUFEMKH YASYYARBEMMN BSHYE, LED WITH YANBPELEMMNTSN OPNRKHBNRYUMINBNTSN NPSFKH.

bNNPSFEMKHE BEPRNKERYU lH-28m BN LMNTsNL SMYUYAKEDNBYUMN NR DMEBMNTSN BYUPKHYUMRYU KH OPEFMELS YANYARNHR XG OSEVMNTSN, SOPYUBKELNTSN X MESOPYUBKELNTSN PUYERMNTSN BNNPSFEMH Kommersant

ONDBHFMYU OSEVMYU SYARYUMNBYU NAMYUYEMYU OSYNI 2yu42 YUKHAPIU 30 LL. OSYU PUGBNPYUVKHBUERYA ON TsNPKHGNMRS MU ╠110 CPYUD., RN EYARE ONVRH MYUGYUD, B TsNPKHGNMRYUKEMNI OKNYAYNYARKH X +13 X -40 CPYUD. B BEPRKHYUKEMNI X YANNRBERYARBSCHR STSKYUL NRYKNMEMKH Nov. oPHLEMEMKHE OSYKH MU lH-28m NYASYYARBKYER NOEPYURNP, UNR OPKHZHEKHBYUMKHE LNFER OPNKHGBNDHRE KERVKHY OPH ONLNYH MYUKELMNI YAKHYARELSH ZHEKESYUGYUMKH. vRN NVEME BYUFMN - OSYU HLEER ONKMSCH SMHTHYUZHCH OH ANEINLOKEYRS I NASHVMNI OSYNI YASUNOSRMSHU BNIYAY. ON YABNHL OYUPYULERPYUL (ANKEYU LYUYAYU YAMYUPYU H ETSN MYUVYUKEMYU YAYNPNYARE) SHRN OSYU OPEBNYAUNDHR OSYS “YOYUVYU”. schryu fe osyu syaryumnbkemu mu yu-50, -52 X lH-28yu, Yu RUYFE MU alo-2, alo-3, ald-2 X ald-3. oPHBND OSEVMNI SYARYUMNBYKH - SCHKEIRPHVEYAYKHI. oKHRYUMKHE OSYKH - KEMRNVMNE, DBSUYARNPNMMEE XG DBSU OYURPNMMSHU YYKHINB, GYUPEOKEMMSHU MU RSPECKH. schRN GMYUVHREKEMN ONBSHEWER MUDEFMNYARE PUANRSH YAKHYARELSH (NRYASRYARBSCHR TSHAYKHE OPEIPSVKHBUCHYHEYA PSYUBYU). aKYUTSNDYUP YAEKEIRKHBMNLS OKHRYUMKHCH SHYKHOYUF LNFER BSHAPYURE RHO YAMYUPYUDYU (APNMEANIMSH HKH NYAYNKNVMN-TSTSYUYAMSHI) MEONYAPEDYARBEMMN BN BPEL AN.

NOSHR OPHLEMEMKH OSEY MU PUGKKHVMSHU BYUPKHYUMRYU lH-24 ONYUGYUK, VRN ONDBHFMYU OSYU TsNPYUGDN SDNAMEE B SCHIYAOXYURYUZHH: PUGBNPNR YAVERBEPEMNTSN OSKELERYU MU RSPEKH lH-2 4d GYUMKHLUK B 3-4 PUGU LEMEYE BPELEMKH, VEL PUGBNPNR BYAETSN BEPRNKERYU lH-24o I MEONDBHFMNI OSYNI. th RNLS FE BEPRNKERS I ONDBHFMNI OSYNI ME MUDN PUGBNPYUVKHBUREYAJ, TSYUYA OPH SHHRNL YAYNPNYARE DN 100 YL/V, VRN DEKUER BEPRNKER ANKEE SJGBHLSHL DK OPNRKHBMKHYU.

ON MEOPNBEPEMMSHL DUMMSHL B MUYARNYE BPEL YAOEZHHYUKEMN DK LH-28m BEDERYA PUGPYUANRYU OSYKH YUKHAPIU 30 LL I ANEGUOYUYANL 250 OYURPNMNB. ynMYARPSYRNPSH UNRЪR SBEKHVKHRE RNVMNYARE YARPEKEASH, R. J. NMJU ONYU NYARYUBKER FEKURE KSVIETSN. DEKN B RNL, VRN RЪFEKYU "RYUMYNBUYU" OSYU SYARYUMNBKEMYU DUKANE NR ZHEMRPYU LYUYAYA BEPRNKERYU, KH NRDYUVYU YAHKEMN BKKHJER MU RNVMNYARE YARPEKEASH. nyanaemmn Shrn GULERMN OPH ANKEHU STSKYU NRYKNMEMKH oos. YAMKHFEMKHE LYUYAYASH NPSDH YALNFER GMYUVHREKEMN ONBSHYAHRE RNVMNYARE YARPEKEASH KH ASHIARPNRS ONBNPNRYU OSYKH.

sOPYUBKELNE PUYERMNE BNNPSFEMHE YANYARNHR XG sp "hTsKYU", orsp 9l120b "YURYUYU-b" X EE "OPYUPNDHREK" - PUYERSH 9l114″jRSPL", YNRNPYU SYARYUMYUBKHBYUKHYAE MU ONGDMKHU LNDKHTKHYUZHKHU BEPRNKERNB lH-24, JYU-29. YaBEPUGBSYNBU BSHYANYNRNVMYU SOPYUBKELYU PYYERYU "YURYUYU-b" KHLEER PYUDKHNYNLYUMMDMSCH YAHYARELS MYUBEDEMKH ONBSHYEMMNI ONLEUNGYYYYYYYARKH, YNRNPYU KHLEER PJD OPE KHLSYYYARB OEPED KYUGEPMNI: MYUOPHLEP NMU ANKEYE OPKHYAONYANAKEMYU Y PUANRE B DSHLS, OSHKH, YAHKEMNL RSLUME. “YURYUYU-b” ONPUFUER RYUMYKH I DHMYULKHVEYAYNI GYUYHRNI APNMH, YU RUYFE BNGDSMSHE ZHEKH. yaBEPUGBSSINBU sp "khTsKYU" NRMNYAHRYA Y PUYERYUL YKYUYAYU "BNGDSU - BNGDSU." nMYU OPEDMYUGMYUVEMU DK NANPNMSH BEPRNKERYU NR YAYULNKERNB X BEPRNKERNB OPNRKHBMKHYU. AKYUTSNDYUP apkya "YuPAYUKER", SCHRH PUYERSH YPSTSKNYASRNVMN OPHLEMCHRYA B PEFHLE "OSYARHK - GUASHK", RN EYARE ЪBKЪCHRYA ONKMNYARECH YUBRNMNLMSHLH ONYAKE OSYAYU. PYUYERSH BYAEU RPEU RHONB SMHTHZHHPNBYUMSH I ANEOPHOYUYULH YASUNOSRMSHU BNIYAY. xU OSYAY NYASYEYARBKERYA NOEPYURNPNL. pYUDKHSYA OPHLEMEMH BYAEU RHONB SOYUBKELNTSN BNNPSFEMH - 6 YL.

b MUYARNYYEE BPEL MU lH-28m OKYUMKhPSCHR ONYARYUBHRE MNBSHE orsp 9l-120d “YURYUYU-d” I SBEKKHVEMMNI DN 8 YL DUKEMNYARECH OSYAYU. oPHLEMEMKHE SCHRNI PUYERSH MU LH-28YU ASHKN MEBNGLNFMN HG-GYU MHGYNI PYUGPEYUCHYEI YAONYANAMNYARKH Nov, ME ONGBNKYEI BEYARKH ONHYAY H NAMYUPSFEMKHE JACKEYS MU DYUKEMNYARYU ANKEE 6 YL. mNBYU pkya "pNRNP" BLEYARE YAN YARYUMZHHEI MNVMNTsN BKhDEMHЪ NAEYAOEVKHBUER ONHYAY RNVEVMSHU ONDBHFMSHU KH TsPSOONBSHU JACKEYS MU SDYUKEMXX DN 10 YL.

yaPEDARBYU OYUYAYAHBMNI NANPNMSH BYKCHVYUCHR B YAYEAYAKHYARELSH BSHAPNYYU hy-KNBSYEH DHONKEMSHU NRPYUFYUREKEY sb-26. schRKH YAKHYARELSH OPEDMYUGMYUVEMSH DK "YAAHBYUMH I RNKYS" tsam PUYER OPNRKHBMKHYU.

b YANYARYUB BNNPSFEMKH BUNDIR RUYFE MESOPYUBKELSHE YUBHYUZHNMMSHE PUYERSH (mup) I-57, I-80 X I-13 YUKHAPIU 57, 80 X 122 LL YANNRBERYARBEMMN. LYUYAHLYUKEMNE YNKKHVEYARBN mup MU RNVIYUU ONDBEYAYKH YANYARYUBKJER 128 UR. DKЪ I-57, 80 LR. DKЪ I-80 X 20 LR. DKЪ I-13. xG MESOPYUBKELNTSN BNNPSFEMKH LNFMN NRLERHRE EEYH 23-LL YUBKHYUZHNMMSHE OSYKH ts-23 B MEONDBHFMSHU SMHBEPIYUKEMSHU OSEVMSHU YNMREIMEPYUU soy-23-250. MU BEPRNKERE LNFER SYARYUMYUBKHBUREYA DBE RYUHU TSNMDNKSH I ANEGUOYUYANL ON 250 YAMYUP'DNB B YUFDNI. oPHLEMEMKHE BYAYEI MNLEMYKURSPSH MESOPIUBKELNTSN BNNPSFEMKH LNFER NYASYYARBKUREYA KERVKHYNL.

lNFER ONYUGYUREYA, VRN mup ЪБКЪерЯ SYARYUPEBHL BHDNL BNNPSFEMKH, MN B YAKSVUE TsPSOONBNTsN OPHLEMEMKH BEPRNKERNB SHRNR BHD BNNPSFEMKH LNFER NYUGUREYA ME GYULEMHLSHL. MUOPHLEP, B YAKSVUE TsPSOONBNTSN MYUKERYU MU YUBKHYUAYUGS OPNRKHBMKHYU, YAMYUVYUKYU BNNPSFEMMSHE ORSPYULH BEPRNKERSH SYARPYUMCHR NVYUTSKH obn I AEGNOYUYUGS PUYAYARNMHЪ X, KHGPYUYAUND NBYUB BEYAE ANEINLOKEIR OPHGSHBUCHR MU ONLNYE BEPRNKERSH I mupYULH, YNRNPSHE SMHVRNFYUCHR I AKHGYNTSN PUYAYARNMHYUMTSYUPSH, YAYKYUDSH, MUGELMSHE YANNPSFEMKH. oPHLEMEMKHE ON SHCHRHL BKhDYUL ZHEKEY ORSP MENOPYUBDYUMMN DNPNTSN. yPNLE RNTsN mup NVEME SHTTEYRKHBMSH OPH YARPEKEAE ON FHBNI YAKHKE, YUBRNLNAKHKU KH R.D., ONSCHRNLS mup NAYGYUREKEMN DNAFMSH ASHR B YANYARYUBE BNNPSFEMKH DUFE VKHYARN OPNRKH BNRYUMINBNI LYUHMSH. hLEMMN mup B NYAMNBMNL OPHLEMCHRYA B VEVEMYAYNI YULOYUMHH I lH-24 X lH-8.

bNNPSFEMKHE BEPRNKERYU LNFER ASHR DNONKMEMN GYU YAVER SOYUBKELSHU ​​PUYER RHOYU p-73 YKYUYAYU "BNGDSU - BNGDSU", YAONYANAMSHU SHTTEYRKHBMN ONPUFYURE BNGDSMSHE ZHEKH, LYUMEBPHPSCHYHE I OPETSPSGYNI DN 12g B DHYUOYUGNME YAYNPNYAREI NR 0 (BEPRNAKER MU BHYAEMXX) DN 2500 YL/V. X PUYER YKYUYAYU "BNGDSU - ONBEPUMNYARE". bNGLNFMN NYAMYUYEMHE OPNRKHBNPUDHNKNYUZHNMMSHLH PUYERYULH RHOYU u-25k. xU MYUBEDEMKHE LNFER NYASYYARBK'REYA YUY I ONLNYECH apkya YAYULNTSN BEPRNKERYU, RYU X I ONLNYECH DPSTSKHU BEPRNKERNB X YAYULNKERNB TPNMRNBNI YUBHYUZHHH DK DNYARKHFEMKH ANKEYE AND DUKEMNYARKH OPHLEMEMKH SHCHRKHU PUYER.

bePRNKER LNFER HYAONKEGNBUREYA X YUY ONYARYUMNBIKHY LKHMMSHU GYUTSPYUFDEMKHI, DK VETSN OND YPSHKN ONDBEBKHBUCHRYA YNMREIMEPSH LYUKNTSUAYUPHRMSHU TsPSGNB iltss-2. RUYFE MENAUNDHLN NRLERKHRE, VRN ONLHLN MNBEI'HU NAPYUGZHNB BNNPSFEMKH LH-28m LNFER MEYARKH BYACH MNLEMYKURSPS ONDBEYAMNTSN BNNPSFEMKH LH-24, VRN ONBSHUER SHTTEYRKHBM NYARE HU YANBLEYARMNTSN HYAONKEGNBUMHЪ B YARPNEBSHU VYUYARU.

bN BPEL ANEBNTSN OPHLEMEMKH lH-28m B YANYARYUBE TsPSOOSH NYASYYARBKERYA YUBRNLYURHGHPNBYUMMNE PYYAOPEDEKEMHE ZHEKEY KH LMNTSNNYARNPNMMKHI NALEM HMTNPLYUZHHEI N ZHEKYU LEFDS KERYU REKEMSHLH YOOOOYUPYURYULH X OSMYRYULH. MU BEPRNKERE OPHLEMEMYU PUGBERBKEMMYU YAHYARELYU BYARPNEMMNTSN YNMRPNK, VRN ONGBNKYER OPNKHGBNDHRE ONDTSNRNBYS Y BSHKERS, ONYAKEONKERMNE NAYAKSFKHBYUMKHE X ONHYAY NRYUGYU BIEI YAKHYARELSH AEG OPHLEMEMH YAOEZHHYUKEMNI YNMRPNKEMN-ONBEPNVMNI YOOYUPYURSPSH. ShRN NAYARNREKEYARBN DUER RUYFE BNGLNFMNYARE SHYAOXYURKHPNBURE BEPRNKER BDYUKH NR YUSCHPNDPNLNB X NANPSDNBYUMMSHU MENAUNDHLSHU AYUG.

lH-28m - YANBPELEMMYU LYUKHMYU, HLECHYYU MU ANPRS BYAE NPTSYUMSH NYSYEMHKH BYAE LSHYAKHREKEMSHE YABNIYARBUYU, UYUPYYUREPMSHE DK VEKNBEYU. yNPNVE - SHRN YANBPELEMMSHI YNLOKEYA YUBKHNMKHYKH, YANNRBERYARBSCHYKHI ORRNLS ONYNKEMKHCH. yYUY YAYYUGYUK BMNBE KHGAPIUMMSHI TSEMEPYUKEMSHI YNMYARPSYRNP TSENPTSKHI yuKeyYuMDPNBHV YAKHMEKEYKHINB, S lH-28m OKYUMEP 5-TsN ONYNKEMKH. GDEYAE MNBSHE MEYASYYU YAHYARELYU, RPYUMYALHYAYAH, PSKEBNI BHMR, ONDUND Y APNMHPNBYUMKHCH, DSAKKHPPNBYUMKHE H PYUGMNYA TSKYUBMSHU YAHYAREL, ONDANP LUREPHYUKNB H YNLOKEYRSCHYKHU (M Yu 98% NREVEYARBEMMSHU). bYae ShRN ONDVKHMEMN FHBSVEYARKH BEPRNKERYU. ANKEE RNTsN, MU lH-28m YADEKYUMSH MNBSHE ZHEKEMNYNLONGKHZHNMMSHE KNOYUYARKH, u-NAPUGMSHI PSKEBNI BKHMR DK SLEMEYEMKH SLYU KH ONBSHYEMKH SHTTEIRKHBMNYARKH, BRSKYU I MEYYU GSHBUCHYHLHYA YUPMHPYULH DK SDEEBKEMKH SHYAOXYURYUZHHH, SKSVIEMSH KERMSHE UYUPYUREPHYARKHYH. mu KNOYUYARU MEYASYETSN X PSKEBNTSN BKHMRNB OPHLEMEMSH MNBEYKHE YUSCHPNDKHMYULKHVEYAYKHE OPNTHKH. sYARYUMNBKEM MNBSHI PEDSIRNP, KHLECHYKHI ANKEKHI PEYASPYA KH ONGBNKQCHYKHI SYARYUMNBKHRE MNBSHE DBKHTSUREKH 4-TsN ONYNKEMKH RB-3-117bl LNYMNYARECH MU 300 K.Ya., R.E. MU 10% ANKEYE, VEL MU lH-28. NMH HLECHR DNYURRNVMSCH LNYNARE VPEGBSHVYUIIMNTsN PEFHLYU DK BNGBPYURYU MU AYUGS MU NDMNL DBHTSUREKE. mu DBKHTSUREKE SYARYUMNBKEMSH MNBSHI BEMRKHKURNP KH MEINRNPSHE DPSTSKHE YAKHYARELSH. dBKHTSYUREKE rb-3-117yaag - EYE ANKEE TNPYAHPNBYUMMSHI I SKSVIEMMSHLH UYUPYUREPHYARKHYULH, YAEIVYUYA MUUNDHRYA MU "TSNPVKHU" HYAOSHRYUMHYU.

yNMYARPSYRNPYUL OPKHKNYAE YARNKYMSREYA I OPNAKELNI YANUPYUMEMH KERMN-REUMHVEYAYKHU UYUPYUREPHYARKHY BEPRNKERYU B SYAKNBHYU PEGYNTSN SBEKHVEMKH TSMYZHNMYUKEMNI MYUTSPSGYKH . OPH SCHRNL LHKEBZHSH ASHKH NTsPYUMKHVEMSH YAKEDSCHYHLH NAYARNREKEYARBYULH. bePRNKER lH-28yu DMEBMNI, YUY KERYUREKEMSHI YOOYUPYUR KHLEK Y SHRNLS BPELEMKH ANKESCH YARYURHYARKHYS ON SHYYAOXYURYUZHHH. MU MEL MENDMNYPYURMN BSHONKMKKHYAE TKhTSSPSH BSHYAETSN OHKNRYUFYU, B RNL VHYAKE OERK MEYAREPNBYU. yaOEZHHTKHVEYAYKHE BEPRNKERMSHE THTSSPSH - ANVYH X OEPEBNNPNRSH I ONYAKEDSCHYHL PUGBNPNRNL - ONGBNKKCHR KERVHYS SUNDHRE NR OPNRKHBMKHYU. KERVKHYKH lH-28 HLECHR BNGLNFMNYARE B GYUBKHYAHLNYARKH NR YAYKYUDSHBUCHYEIYA ANEBNI YAHRSYUZHKH BSHAPURE KH OHKNRYUFMNTSN YUPYAEMYUKYU SHRNI LYUKHMSH RNR XKKH KHMNI SHKELEMR X OPHLEMKHB E CN B MSFMSHI LNLEMR MENFKHDUMMN DK OPNRKHBMKHYU, BSHHTSPYURE ANI.

xGBEYARMN, VRN OEPETSPSGYH BSHYE "3g" YAVKHRYUCHRYA DK BEPRNKERNB NVEME ANKEHLH. x B LHPE MELMNTSN BEPRNKERNB, YNRNPSHE DNYARKHTSYUCHR RYUKHU OEPETSPSGNY. with lH-28 “3g” - MNPLYUKEMYU SHYYAOXYURYUZHNMMMYU OEPETSPSGYU. MENAUNDHLN ASHKN YANUPYUMHRE KH DPSTSKHE BYUFMEIYKHE DUMMSHE (BGKERMYU LYUYAYU LH-28YU - 10500 YTS, LYUYAKHLYUKEMYU YAYNPNYARE ONKERYU 300 YL/V, YARYURKHVEYAYHI ONRNKNY 3 600 L, DHMYULHVEYAYHI ONRNKNY 6000 L KH LNFER MEYARKH ANEBSC MYUTSPSGYS ANKEE 2000 YTS). x BRNPNE NAYARNREKEYARBN: pNYARNBYAIKHI BEPRNKERMSHI GYUBND Y LNLEMRS GYUPNFDEMKH lH-28m GYUYUMVKHBYUK ONDTSNRNBYS Y YAEPKHIMNLS BSHOSYAYS lH-28yu, GYURPYURKHB MU SHCHRS PYUANRS LMNTsN YANAYARBEMMSHU YAPEDYARB. bYuFMN - ME LEM YARYUOEKEY, ME SUSDYU KERMN-REUMHVEYAYHU UYUPYUREPHYARKHY, NAEYAOEVHRE PEYEMKHE BSHYEOPEVHYAKEMMSHU MNBSHU TSMYZHNMYUKEMSHU GYUDYUV KH, YANNRBERYARBEMM N, PYUGLEYARHRE MU BEPRNKERE LMNTSN MNBSHU YAKNFMSHU YAHYAREL. ONDTSNRNBYU OPNKHGBNDYARBYU lH-28m OPNBEDEMU MU pNYARNBYAYNL GYUBNDE, KH NM LNFER MUVYURE YEPKHIMSHI BSHOSYAY, (BRNPYU NOSHRMYU LYUKHMYU YARPNHRYA SFE B pNYARNBE). yYARYURKH, MU OEPBNI LYUHME YARNHR PEDSYRNP YAEPKHIMNTSN GUBNDU.

oPH BSHONKMEMHKH ONKERNB MYUD ONKEL AN YA BSHYANYNI OKNRMNYARECH NTsM GMYUVHREKEMN BNGPUYARYUER BEPNЪRMNYARE ONPUFEMKH. ONSHRNLS OPNAKELE GYUYHRSH SHCHYHOYUFYU GDEYAE SDEKEMN YAYULNE OPKHYARYUKEMNE BMHLYUMKHE. b ZHEKU ONBSHYEMKH ANEBNI FHBSVEYARKH MU lH-28m PEYUKHGNBYUM YNLOKEYA LEPNOPHYARKHI, BYKCHVYUCHYCHYKHI:

• PYUGMNYA tsrd OH ANPRYUL TCHGEKKFYU KH PUGDEKEMHE HU TSKYUBMSHL PEDSYRNPNL, VRN HYAYKCHVUER BNGLNFMNYARE ONPYUFEHMKH NANKHU DBKHTSUREKEY NDMHL BSHIARPEKNL, VRN VYUYARN OPNHYAUND HKN B ANEBSHU SYAKNBKHU MU lH-24 X lH-8
• NAEYAOEVEMHE ONKERYU MU NDMNL DBKHTSUREKE I YUBRNLYURKHVEYAYHL BSHBNDNL ETSN MU LYYYAKHLYUKEMSHI PEFHL OPH NRYUGE HKH ONPUFEMXX BRNNTsN
• BNGLNFMNYARE PUANRSH BYUFMEIKHU YAKHYAREL BEPRNKERYU MEINRNNPNE BPEL AEG YALUGYKH
• LKHPNYNE OPHLEMEMKHE OMEBLYURKHVEYAYKHU OPHBNNDNB BLEYARN ONFYUPNNNOYUMShu TSKHDPUBKHVEYAYKHU
• YPSTSNBNE APNMHPNBYUMKHE YUAKHMSH SHCHYHOYUFYU, DSAKHPNBYUMKHE X BGYUKHLMNE SHYPYUMKHPNBYUMKHE BYUFMEIYKHYAREL X YUTSPETSYURNB BEPRNKERYU
• DSAKKHPNBYUMKHE KH PYUGMEYAEMKHE ON ANPRYUL OPNBNDYKH YAKHYARELSH SOPIUBKEMKH KH SCHKEIRPNYAERKH

aPNMEYUAHMYU SCHYHOYUFYU, RYU MYUGSHBUELYU "BYUMMYU", BSHONKMEMYU HG 10-LL KHYARNB YUKCHLKHMKH, MU YNRNPSHE MYIKEEMSH 16-LL YEPYULHVEYAYKHE OKHRYKH. dBEPH YUAKHMSH BSHONKMEMSH DBSU YAKNEB YUKCHLHMKHEBNI APNMH X YAKN ONKKHSPERYUMU LEFDS MHLH. KNANBSHE YAREYKYU YUAHMSH OPEDYARYUBKCHR YANANI OPNGPUVMSHE YAHKHYURMSHE AKNYH RNKYKHMNI 42 LL, YU ANINBSHE YAREYKYU X YAREIKYU DBPEI - HG RUYKHU FE AKNYNB, MN RNKYKHMNI 22 L L. yYUAKHMY KERVKHYU NRDEKEMYU NR YUAHMSH NOEPYURNPYU 10-LL YUKCHLHMKHEBNI APNMEOKHRNI, VRN YABNDHR Y LHMHLLSLS ONPYUFEMKHE NANKHU VKEMNB SCHYKHOYUFYU NDMHL BSHYARPEKNL.

NTSMEBSHE HYAOSHRYUMKH, OPNBEDEMMSHE B tsNYamkhyuya ONYUGYUKH, VRN ANPRYU BSHDEPPHHBUCHR ONOYUDYUMKHE OSKE YLEPHYUMYAYNTSN 20-LL OSKELERYU "bSKYYUM", KNANBNE YAREIKN - OSKE YUKHAPIU 12.7 LL, YU ANINBSHE YAREIKYU X YAREIKYU DBEPEI - 7.62 LL.

GYUYHRS NR ONPUFEMKH SOPYUBKELSHLH PUYERYULH MU lH-28m NAEYAOEVHBUCHR: YOOOOYUPYURSPYU DK ONYARYUMNBYKH ONLEU PUDHNKNYUZHNMMSHL YARYUMZHKHL KH PUYERYUL I KHMTPYUPYYAMNI YAHYA RELNY MYUBEDEMH; YOOOOYUPYURSPYU OPEDSOPEFDEMKH ON NAKSVEMKHH BEPRNKERYU PUDHNKNYYUZHNMMSHHLH YARYUMZHHLH KYUGEPMSHLH ZHEKESYUGYUREKLH OPNRKHBMKHYU, OPH SCHRNL SHCHYHOYUF NONBEYUERYA ON KHMTPYU YPYYYAMNL X PUDHNKNYUZHNMMNL NAKSVEMHH I ONLNYECH PEVEBNI KHMDHYUZHHH (MUANP MEINRNPSHU TPYUG RHOYU “OPNRKHBMKHY YAGYUDH!”), AKNYNL YNMRPNKEMSHU KYULO KH YANNAYEMKHI MU Ltd (LMNTs) NTSMYZHNMYUKEMSHI DHYAOKEY); SYARPNIYARBN NRYARPEKYU OYURPNMNB sb-26 DK GYUYHRSH NR PUYER I REOOKNBSHL MYUBEDEMHEL.

pYYYAYALYURPHBYU PUGKKHVMSHE YAKHYARELSH YAOYUYAEMKH SHCHYHOYUFYU, LHKEBZHSH ONMYUVYUKS NRYUGYUKHYAE NR YURYUOSKERKHPNBYUMH I NRYARPEKNL KNOYUYAREI MEYASYETSN BKHMRYU, MN MU lH- 28m BYAE-RUYKH SYARYUMNBHKH OHPNANKRSH YPEOKEMKH KNOYUYAREI. YAHYARELYU YAOYUYAEMH PUANRYUER ON NDMNLS HG ​​DBSU YUKTSNPHRLNB, YNRNPSHE MU DUMMSHY LNLEMR NRPYUANRYUMSH X BYAYARNPNMME HYAOSHRYUMSH:

1. oPH BNGMKHYMNBEMKHH MEURYURMNI YAHRSYUZHHH XKH YURYUYARPNTHVEYAYNTSN PYUGPSIEMKH YNMYARPSYZHKH MU BSHIANRE ANKEE100 L YAMYUVYUKYU NRYARPEKHBUCHRYA KNOYUYARKH BKHMRYU, YNMYANK X YPSHKYU X DBEPKH NAEKHU YUAKHM, GUREL YAOEZHYUKEMSHLH PEGYUYULH OEPEPEGYUCHRYA PELMH OPHMSDHREKEMNTSN OPHRITSIU, MYUDSBYUCHRYA YAOEZHHYUKEMSHE "RPYuOSH" - AYUKKNMERSH, Y NRNPSHE ME DUCHR SHYHOYUFS OPH ONYKHDYUMHH GYUDERE YUYAYAH XKH ONBEPMSRSCH OSYS, KH SHCHYKHOYUF ONYKHDUER LYUHMS I ONLNYECH OYUPYUCHRNB.
2. OPH RUYNI FE YAHRSYUZHHH, MN MU BSHIANRE LEMEE 100 L YAPYUAYURSHBUER YAHYARELYU OPHMSDHREKEMNTSN OPHRQTSYU PELMEI, MYUDEFMN THYAHPSCHYYU SHCHYHOYUF B SCHMEPTSNONTSKNYYUCHYU YPEYAK YU "oYULHP-y" PYUGPYUANRYKH ya "gBEGDU". YAMYUVYUKYU SHMEPTsKHCH SDYUPYU TSYUYAR NYAMNBMSHE YARNIYH YUYAYAKH, YNRNPSHE, DETNPLKHPSYAE, ONTSKNYYUCHR ITS. DYUKEE B PUANRS BYARSOYUCHR YPEYAKYU, YNRNPSHE YAONYANAMSH ONTSYUYAHRE BEPRKHYUKEMSCH OEPETSPSGYS 50-60 g DN 15-17 g, NAEYAOEVHBYU RPYUBLNAEGNOYUMNYARE OHKNRS X LRSPLUMS-NOEP YURNPS.

yuYAYAKH BEPRNKERNB YAELEIYARBU lH-28 BSHONKMEMN MESAKHPYUCHLYA, VRN NASYAKNBKEMN LYUKSHL GUOYUYANL BPELEMH OPH YUBYUPKHIMNI ONYAUDYE. b SCHRNI YAHRSYUZHKH SAKHPYUCHYEYUYAYAH, YU REL ANKEE YUYAYAKH, YNRNPNE GUYPSHBUERYA YARBNPYULH, LNFER ME SYAOERE BSHIRKH HG MHH, OEPEDYUB REL YYULSHL BYCH SHCHMEPTSKHCH MU TCHGEKЪF , VRN MEHGAEFMN OPHBEDER Y YURYUYARPNTHVEYAYHL PYUGPSEMHEL. th RNLS FE MESAKHPYUELNE YUYAYAH ONGBNKHKN BEPRNKERS "YAPNYAHRE BEYA" GYU YAVER NRYASRYARBKH LEUUMKHGLNB YAYKYUDSHBYUMKH KH SANPYKH YUYAYAH. Nyamnbmsha Yarniykhiyui Mu-28M Bshonkmemsh Shmeptsnelehlh, NMH Yaojkhukamshl Napyugnl Dettlhpsrya Tspsani Tsyuyudye, Zyu Gmyuvkhrekemsch owayarem Smemepskhh Sducyu.

хЯОШРУМХЪ lH-28m ASDSR YANBLEYEMSH B NDHM SHRYUO KERMN-YNMYARPSYRNPYAYKHU KH TSNYASDYUPYARBEMMSHU HYAOSHRYUMKHI. NYNMVYUMKHE KHU OKYUMHPSERYA GUYNMVHRE B 1998 TsNDS. dKH SYAYNPEMKH GUYKYUDSHBUCHRYA MNBSHE YAPEDYARBU ANPRNBSHU HGLEPEMKHI, YNRNPSHE ONGBNKR LTSMNBEMMN NAPUAYURSHBURE PEGSKERYURSH HYAOSHRYUMKHI H, YANNRBERYARBEMMN, DNAF MS SYAYNPHRE ONKSVEMKHE MENAUNDHLSHU GUYKCHVEMKHI. ONYAKE SCHRNTSN LYUKHMYU ASDER TsNRNBYU ONYARSOKHRE MU ANEBNE YAMYUAFEMKHE. eYARE EY NDMN MUOPYUBKEMKHE DERREKEMNYARKH nya KHLEMKH lHK: SKSVIEMKHE ANEBSHU UYUPYUREPHYARKHY lH-24, YNRNPSHY YAYEIVYUYA MUUNDHRYA MU BNNPSFEMHKH, GYU YAVER SYARYUMNBYKH MU METSN MNBKHMNY, OPHLEMYELSHU ​​MU lH-28m, BYKCHVYU MEYASYSCH YAKHYARELS KH PSKEBNI BKHMR. with lH-28m EYARE YNMYSPEMRSH: OYUPYUKKEKEMN DEKUERYA LYUHMY MU THPLE "YULNB", YANGDUCHRYA YUMYUKNTSKHVMSHE BEPRNKERSH H S YULEPHYUMZHEB, H S TPYUMZHSGNB. ndMUYN lH-28m NOEPEFUER GYUOJDMSCHE PYGPUANRICH. OPEDYARYUBK MNBSHI BEPRNKER, TSENPTSKHI YAHMEKEYKHINB I NYANANI REOKNRNI TsNBNPKHK N GMYUVHREKEMNL BYKYUDE B PYUGPYUANRYS SHRNI LYUKHMSH RYUKYUMRKHBNTSN YNMYARPSYRNPYU LYUPYU bK YUDHLHPNBKHVYU bYuIMAEPTSYU, MEDUBMN SEDJETSN HG FHGMH.

b MUYARNYE BPEL lbg YAVKHRYUER OPNTsPYULLS lH-28 X ETSN LNDHTHYUZHHI OPHNPHRERMNI, NRDYUBYU OPEDONVREMHE lH-28m, ME FUKE MU METSN YABNHU YAYSDMSHU YAPEDYARB. th YANFYUKEMHCH TSNYASDYUPYARBEMMNTSN THMYUMYAHPPNBYUMKH OPNTSPYULLYU ME ONKSVIUER. UND OPNTsPYULLSH KERMSHU HYAOSHRYUMKHI LNFMN YAPYUBMKHRE I DBHFEMHEL YUBRNLNAKHK I ONYARNMMN TSKNUMSYHL NR MEUBYURYKH AEMGHMYU DBKHTSUREKEL: yNMYPERMSHU GYUYUGNB NR YUPLXX MER . RUL DEMETS ME UBURUER DUFE MU ONKMNZHEMMSHE GYYSOYKH ONAEDKHBIETSN B YNMYSPYAE yu-50, VRN FE TsNBNPKHRE N OPNHTSPUYUBKHU: TsPSYARMN SCHRN BYAE: TsPSYARMN, VRN YARPYUME ME MSFMYR YYYU OEPYAOEYRKHBMYU X DNATSNYAPNVMYU PYUGPYUANRYU. lbg OPKHUNDHRYA NPKHEMRKHPNBUREYA MU BMEMKHI PSHMNY. mN ANKEHMYARBS TSNYASDYUPYARB, GYUHMREPEYANBUMMSHU B ONYSOYE lH-28yu X -28m MSFEM ONKMNYARECH HYAOSHRYUMMSHI (FEKUREKEMN “B DEKE”), DNPUANRYUMMSHI, MYUDEFMSHI X “DNBEDEMMSHI DN SLU" BEPRNKER. eYAKKH B AKKHFUIEEE BPEL ME ASDER OPEDOPKHMRN YAN YARNPNMSH TSNYASDYUPYARBU MKHYUYKHU LEP ON OPNDBHFEMKHCH OPNTsPYULLSH lH-28m, RN YARPYUMYU KKHHRYA ONVRKH TSNRNBNTSN BYAEONTs NDMNTsN YPSTSKNYASRNVMNTsN BEPRNKERYU, YNRNPSHI LNTs ASH I SIAOEUNL NAEYAOEVHRE OYUPHRER YAN YARPYUMYULH gyuoyudyu H yayu. yPNLE RNCN, BEPRNKER YAONYANAY OPHMNYAKHRE OPKHASHKE TSNYASDYUPYARBS X lbg GYU YAVER SHYYAONPRMSHU ONYARYUBNY (YUY ONYUGSHBUCHR HYAYAKEDNBYUMKH, YAOPNYA MU ANEBSHE BEPRNKERSH PUYARER). ONYU NYARYUERYA MYUDEREYA MU SHYYAONPRMSHI ONREMZHYUK BEPRNKERYU, YNRNPSHI NYUGYUKYA MELYUKSHL OPH OPNBEDEMHH B BBEZHHH YAPYUBMHREKEMSHU HYAOSHRYUMKHI lH-28yu X AH-64A « Apache."

HRYUY, KH BYAETSN BSHYE MYOOKHYUMMNTSN BHDMN, VRN lH-28m OPYURKHVEYAYKH BN BYAEL OPEBNYAUNDHR AH-64D. schRN YYUAYUERYAKH KERMSHU DUMMSHU, X YUYUPYUREPKYARKHY NPSFKH, X ANEBNI FHBSVEYARKH, X SDNAYARBU SHYAOXYURYUZHH. MN GDEYAE MENAUNDHLN NRLERHRE DBY TYURYU: BN-OEPBSHU AH-64D “Longbow” OPNKHGBNDHRYA YEPKHIMN. ShRN DUER ELS YNKNYAYUKEMNE OPEHLSYYARBN. BEDE KHLEMMN B OPNZHEYAYAYE JEPKHIMNTSN, YU ME URSVMNTSN OPNKHGBNDYARBU, X ONYAKEDSCHYEI SHYAOXYURYUZHKH B YARPNEBSHU VYUYARYU BSHYALYURPHBYUCHRYA X SYARPUUMCHRYA MEDNYARYURYKH, YNRNPSHE LNTSKKH ASHRE MEGULEVEMSH BN BPEL KERMSHU HYAOSHRYUMKHI. bN-BRNPSHU, lH-28m OPNEIRKHPPNBUKYA ME I MSK, YUY “Apache”, YU I NTSCIDYNI MU ONYAKEDMKHI. schRN DUBUKNE MEYNRNPNE OPEHLSYYARBN OPNTsPYULLE PNYYAKHIYYYNTSN BEPRNKERYU. ъ ME UNVS VEPMKHRE MYUKHU YNMYARPSYRNPNNB KH NABKHMЪRE KH B OKYUTSKHURE, MN OEPED MHLH YARNKYU MEYAYNKEIN ANKEE OPNYARYU I REUMKHVEYAYNI RNVYKH GPEMHЪ GYUDYUVYU. I DPSTSNI YARNPNMSH, EYAKH BYAONLMKHRE PUGLEPSH THMYUMYANBSHU BKHBYUMKHI B PNYYAKHIYAYKHI H YULEPKHYUMYAYKHI OPNEIRSH, RN LNFMN OPEDONKNFHRE, VRN lH-28m LNTs ASH MYUYURE OPNKHGBNDHR EYAYEPHIMN NYNKN DEYARKH KER MYUGYUD.

eYE LNFMN NRLERHRE, VRN MH NDHM HG BEPRNKERNB YAELEYARBYU lH-28 ME SVIYARBNBUK B ANEBSHU DEYARBKHU.
“Apache” FE YURKHBMN OPHLEMKHYAE X OPHLEMCHRYA BN LMNTSKHU KNYYUKEMSHU YNMTKHYRYUU, X BSHUBKEMMSHE MEDNYARYURYKH ASHKKH SVREMSH X SYARPYUMEMSH MY BEPRNKERYUU ONYAKEDSCHIKHU I EPHI. ONYU FE LNFMN YAYUGYURE, VRN lH-28m OPEBNYAUNDHR “Apache Longbow” KHIE MU ASLYUTSE. x DUY ANTS, VRNASH SHHRKH DBYU "GYUNVMSHU OPNRKHBMKHYU" MKHYNTSDU ME BYARPERHKHKHYAE B PEYUKEMNL ANCH, YUY BYAETSDU, ON TSKSONYARKH ONKHRKHYNB. lNDHTHYUZHHH :

lH-28m "mNVMNI NUNRMHY"	mNVMNI MU AYUGE lH-28yu. I TSKYUBMSHL PEDSYRNPNL bp-29 BLEYARN bp-28.
lH-28ml	lNDEPMHGYUZHXX lH-28m. YURMYU SYARYUMNBYU MYUDBRSKNVMNI pkya RHOYU m025, DSAKHPNBYUMMYU YAKHYARELYU SOPYUBKEMKH, DNONKMEMYU BNGLNFMNYARECH SOPYUBKEMKH aokyu. 29 KhChK 2016 TsNDYu lH-28ml YANBEPHK OEPBSHI ONK╦R.
lH-28msch	shYYAONPRMYU LNDKHTHYUZHKH BEPRNA╦RYU lH-28m.
lH-28sa	lH-28m I DBNIMSHL SOYUBKEMHEL. YaOZHHYUKEMSHI BEPRNA╦R I DBNIMSHL YNLOKEIRNL SOPYUBKEMKH, YNRNPSHI LNFER OPHLEMREYA DK NASVEMKH OKHKNRKHPNBYUMHCH lH-28m, OPH ShchRNL YANUPYUMER BYACH TSMYZH NMYUKEMNYARE SDYUPMNTSN BEPRNA╦RYU.

cru:

lNDHTHYUZHH	lH-28m
dHYULERP TSKYUBMNTSN BKHMRYU, L	17.20
dHYULERP UBNYARNBNTSN BKHMRYU, L	3.84
dKHMYu,L	17.01
bSHYANRYU,L	3.82
I love it, JC
OSYARNCN	7890
MNPLYUKEMYU BGKERMYU	10500
LYUYAHLYUKEMYU BGKERMYU	11700
bMSRPEMMHE RNOKHBN, K	1500
ora	4 U 500
RHO DBKHTSUREK	2 tsrd yKHLNB rb3-117blue
lnymnyare, YbR	2 U 1660
LYUYAKHLYUKEMYU YAYNPNYARE, YL/V	324
yPEIYEPYAYU YAYNPNYARE, YL/V	265
oEPETSNMNVMYU DUKEMNYARE, YL	1105
oPUYRHVEYAYU DUKEMNYARE, YL	500
YAYNPNONDZELMNYARE, L/LHM	816
oPUYIRKHVEYAYKHI ONRNNKNY, L	5700
YaRYURKHVEYAYKHI ONRNNKNY, L	3700
ShYKHOYUF, VEK	2
ONKEGMYU MYUTSPSGYU:	DN 2 OYYAYUFHPNB
bNNPSPHEMHE:	NDMYU 30-LL OSYU 2yu42 I 300 OYURPNMYULH ANEBYU MYUTSPSGYU - 1605 YTS MU 4 SGKYU ONDBEYAYKH: 4U4 ORSP URSP KKH yuRYUYU-b X 2 os sb-20-57 20U55-LL KHKH sb-2 0-80 20U80-LL msp HKH 2 os I 130-LL msp BNGLNFMYU SYARYUMNBYU 2U2 sp BNGDSU-BNGDSU p-60, YNMREIMEPSH I 23-LL OSYYULH KKH 30-LL TSPUMYURNLERYULH KKH 12.7-LL XKH 7.62-LL OSKELERYULH, KKH 500-YTS ANLASH, KKH ONYARYUMNBIKHYKH LHM OND YPSHKELKH - 16 orsp bHUPE

bottom. KhMTNPLYUZHKH:

VEPREF "lHKE lH-28" VEPREF "lHKE lH-28m" tNRNTsPYUTKHH:	oEPBSHI NOSHRMSHI lH-28m
oEPBSHI NOSHRMSHI lH-28m
oEPBSHI NOSHRMSHI lH-28m
oEPBSHI NOSHRMSHI lH-28m
bRNPNNI NOSHRMSHI lH-28m
bRNPNI NOSHRMSHI lH-28m (c) yuMYURNKHI asPZHEB
oPEDAEPHIMSHI lH-28m
lH-28m
lH-28m
lH-28m
lH-28m
lH-28m (c) TsPTsNPKHI b.
lH-28m (c) hKEЪ anKDSHPEB
lH-28m (c) yuPR╦L YARUPYNB
nAGNPMN-OPKHZHEKEMSHI YNLOKEYA lH-28m (c) hTSNPE yNKNYNKNB
ONDBHFMYU SYARYUMNBYU moos-28 I OSYNI 2yu42 MU lH-28m (c) hTSNPE yNKNYNKNB
yYUAHMYU lH-28m (c) yUKEYYYUMDP kSHYAYEMYN

IWELSH:

lH-28m

YNLONMNBNVMYU YAUELYU

YNLONMNBNVMYU YAUELYU

yaUUELYU ONDBEYAYKH BNNPSFEMHЪ

bYUPHYUMRSH NYPYYAYH:

oEPBSHI NOSHRMSHI lH-28m

oPEDAEPKHIMSHI lH-28m (c) south. hPCEMYANM

YaOHYANY HYARNVMKHYNB:

yuBHYuyNKKEIZHH 2008-06. M.B. ъYSANBHV. aNEBNI BEPRNKER lH-28 oNKHTSNM. b.p. lHUEEEB. lNYAINBAYKHI BEPRNKERMSHI GYUBND KHLEMKH l.k. lХКЪ ъСГУ. mKHYNKYUYYSANBHV. BYAE ANEBSHE BEPRNKERSH YAYAYAP X PNYAYAHH YUSCHPNYNYALHVEYAYNE NANGPEMHE 2019-03. lHUYUHK mHYNKEYAYKHI. lH-28 bGKER 2011-01-02. YuMDPEI TNLHM. lH-28: ONYARYUBYKH PUYARSR bGKER 2014-06. YuMDPEI TNLHM. “mNVMNI NUNRMKHY”: dK PNYAHIYAYKHU bbya X GYUPSAEFMSHU GYUYUGVKHYNB yPSHKE pNDHMSH 1997-07-08. kEB aEPME. "mNVMNI OKHPYUR" LNYAYNBAYKHI BEPRNKERMSHI GYUBND HL. l.k.lHKЪ. lH-28m LYYYAHL YARYUPNYARKHM. bYAE BEPRNKERSH lHPYU. lHKE lH-28m BEYARMKHY BNGDSMNTSN TKNRYU. b. YANNKEMHYNB b. aNEBSHE BEPRNA╦РШ yu-50 Х lХ-28 BEYARMHY yuBХУжХХ Х йНЯЛНМУБРХХ. m. BYUKSEB. lH-28m - MNVMNI NUNRMHY reUMHYU H BNNPSPHEMHE. lHUYUHK mHYNKEYAYKHI. gYUNVMSHI ANI: lH-28 Vs yum-64 bHYRNP kHRNBYHM. "pYUGPSHREKE" BGKERUER ONYAKE ONPUFEMHЪ Air International 2013-02. Alexander Mladenov. Russian's Night Hunter Aero Magazin Lotniczy 2007-12. Piotr Butowski. Mi-28N konczy proby L+K 1999-12-13. Petr Kolmann. Mil Mi-28 L+K 2004-07. Miroslav Gyurosi. Nocny dravec Mi-28N Russianplanes.net. lH-28m

sTSNKNY MEAYU. 2020

Vitality

The cabin design uses highly resistant armor, fully armored plane-parallel glazing can withstand direct hits from armor-piercing bullets of 12.7 mm caliber, high-explosive fragmentation shells of 20 mm caliber, the blades remain operational when hit by 30 mm shells.

The armored crew cabin, the so-called “bath,” is made of 10-mm aluminum sheets, onto which 16-mm ceramic armor elements are glued. The cabin doors are made of fiberglass with an aluminum plate and ceramic armor. The cabin windshields are made of transparent silicate blocks 42 mm thick, and the side windows and door windows are made of the same blocks, but 22 mm thick. The pilot's cabin is separated from the operator's cabin by a 10-mm aluminum armor plate, which minimizes damage to both crew members when a small-caliber high-explosive incendiary (HEF) shell explodes in one of the cabins. The fuel tanks are filled with polyurethane foam and equipped with a latex self-tightening protector.

The Mi-28 is capable of flying at extremely low altitudes (up to 5 m) while skirting the terrain. The maneuverability of the helicopter has been increased, which can now move backwards and to the sides at a speed of 100 km/h. During hovering, the total angular speed of turn can reach 90 degrees per second, and taking into account the angular speed of yaw of just over 117 degrees/sec, the maximum angular speed of roll is more than 100 degrees/sec.

Compared to the Mi-24, the Mi-28 has 1.5 - 2 times reduced visibility in the infrared range (with the same engines) due to the installation of screen-exhaust devices (ESD).

Protection from guided missiles on the Mi-28N is provided by equipment for jamming radar stations and IR homing heads. In the future, it is planned to use the full set of the Vitebsk L370 (export name - President-S (SOEP)) - currently this complex (in export version) is installed on the Mi-28NE prototype (b/n 38), created for the Indian tender for the supply of attack helicopters (Mi-28NE lost this tender). The helicopter can conduct combat operations autonomously, outside the airfield, for 15 days. The complexity of maintenance compared to the Mi-24 is reduced by 3 times. Dust-proof devices are installed at the engine inlet, ensuring surge-free operation of the engines when starting the NAR. An AI-9V APU is installed, which provides air conditioning, heating of the cabin and power supply to the electrical systems.

For the first time in the domestic practice of helicopter construction, spherical elastomeric hinges that do not require lubrication are used in the design of the main rotor hub, instead of horizontal, axial and vertical hinges. In other articulated joints of the bushing, self-lubricating metal fluoroplastic and fabric bearings are used, which made it possible to reduce lubrication points from 20 to 1, compared to the Mi-24.

The most important helicopter components and wiring are duplicated and located on different sides, important ones are covered by less important ones.

Interesting facts about the Mi 28N helicopter

the Mi-28 in the Russian helicopter industry, none of the helicopters performed such aerobatics as the barrel roll and Nesterov loop. And the Mi-28 not only made these figures, but also flew sideways and backwards at a speed of at least 100 km/h.

Performing flights in difficult weather conditions and at night, the Mi-28N flies at an altitude of 5 meters, skirting the terrain, searching for and destroying the enemy and guiding other helicopters to targets.

Mi-28N helicopter detects the enemy even at night at a distance of 35 km.

Test pilots called the Mi-28 a “fighter helicopter”, and popularly called it a “flying tank”.

Performance characteristics

Specifications

• Crew: 2 people
• Fuselage length: 17.05 m
• Height: 3,82
• Width with wing consoles 5.88 m
• Main rotor diameter: 17.2 m
• Tail rotor diameter: 3.85 m
• Weight: empty: 8095 kg
• normal take-off weight: 10900 kg

• maximum take-off weight: 12100 kg
• Weight of combat load: 2300 kg
• Fuel weight: 1500 kg

Power point:

Engine type: turboshaft

Model: VK-2500-02

Power: in emergency mode: 2700 l. With.

at takeoff mode: 2200 l. With.

at cruising mode: 1500 l. With.

Flight characteristics

• Maximum speed: 300 km/h
• cruising: 265 km/h
• Flight range: maximum 450 km
• with PTB: 1087 km

Static ceiling: 3600 m

Dynamic ceiling: 5600 m

Rate of climb: 13.6 m/s

Armament

• Built-in rifle and cannon: 1 × 30 mm 2A42 cannon, 250 rounds of ammunition.
• Suspension points: 4
• Unguided rocket: NAR S-8 - 4 x 20 pcs; NAR S-13
• Guided missile: ATGM "Ataka-V" (9M120, 9M120F, 9A-2200) 16 pcs
• "Air-to-air": Strelets with Igla-V missile - 4 x 4 pcs.

• 30-mm NPPU-28 cannon with 250 rounds of ammunition, two-way selective supply of shells, a choice of shells: armor-piercing or OFZ. Designed to destroy lightly armored vehicles at a range of 1500 m, manpower up to 4000 m and low-speed air targets up to 2500 m. To increase shooting accuracy, the barrel is shock-absorbed. The ammunition consists of armor-piercing and high-explosive fragmentation shells. Gun deflection range: azimuth ±110°; elevation angle +13…-40°. The gun is synchronized with the sight. The pilot can also fire using the HUD or helmet-mounted sight. Experience in using guns on various variants of the Mi-24 has shown that a movable gun is much more convenient to use: turning a quad machine gun on a Mi-24D turret took 3-4 times less time than turning the entire Mi-24P helicopter with a fixed gun. A helicopter with a movable cannon does not need to turn around, reducing speed up to 100 km/h, which makes the helicopter more vulnerable to the enemy.

• UR Attack-V (beam holder DB-3UV) is designed to destroy armored vehicles, manpower, helicopters, bunkers, bunkers. The missile is controlled through an anti-jamming millimeter-wave radio channel (narrow directional pattern), the transmitter is located in the bow of the helicopter, the receiver is located in the rear of the missile. It is possible to use missiles simultaneously from 10 carriers. In combination with an automatic target tracking system, the helicopter can maneuver with a yaw angle of ±110° and a roll angle of ±30°. Unlike laser beam guidance systems, it has the advantage of unlimited missile control time with a high rate of fire; laser systems are less reliable in smoke conditions (dust and fog).
• The Igla-V TGSN missile is designed to destroy small-sized UAVs, helicopters, airplanes, and cruise missiles. The Igla missile is equipped with cooling for the missile's homing head, which makes it possible to hit targets not only by the heat from hot engine exhaust gases, but also any heat-contrasting targets; the missile seeker ensures selection of thermal interference.
• KMGU-2 Container for small-sized cargo, for laying minefields.
• NAR Unguided missiles are designed to destroy manpower, light armored vehicles and infrastructure. The main advantage is low cost.

Description of the Mi-28NE helicopter

The Mi-28NE was developed taking into account the experience in the creation and combat use of Mi-35 helicopters and their foreign analogues. The fuselage of the Mi-28NE consists of the nose and central parts, as well as the tail and keel beams. In the bow there is a crew cabin consisting of two armored compartments. The crew cabin is tandem, hermetic, ventilated with an air conditioning system, and has armor protection. The helicopter crew consists of a pilot and a pilot-operator. The Mi-28NE is resistant to difficult operating conditions, and also has the ability to adapt to the latest equipment and weapons systems. The Mi-28NE has high maneuverability, which allows it to perform complex aerobatic maneuvers, for example: figure eights, snakes, spirals, combat turns and slides. It has high combat survivability, operational and technical characteristics and modern means of protection. The Mi-28N has the lowest possible acoustic signature for enemy air defenses, which allows it to effectively carry out combat missions. The helicopter is built according to the classic single-rotor design with a tail rotor and is equipped with two VK-2500-02 turboshaft engines. Currently, the Mi-28NE helicopter is produced with dual controls and can be used to train cadets of military schools and military pilots in piloting, while it retains all the functionality of an attack helicopter. The presence of a dual mechanical control system is the main difference from the previous version of the helicopter. This allows you to control the helicopter both from the pilot’s cockpit and from the cockpit of the pilot-operator serving as an instructor. The crew cabin has been enlarged, the upper part of the canopy has been expanded, and upgraded energy-absorbing seats with a new parachute system have been installed.

Contracts for supplies to other countries

Contract for the supply of Mi-28L to Iraq (1990)

The contract was concluded in 1990 for supply and licensed assembly, but was not implemented due to the Iraqi occupation of Kuwait.

Mi-28A at tender in Sweden

Comparative tests were carried out with combat launches of NARs, ATGMs and cannon weapons. The launch of the 9M114 "Sturm" ATGM was carried out while hovering, at a target at a range of 900 meters, the launch of the 9M120 "Attack" - from horizontal flight at a speed of 200 km/h and a range of 4700 meters. Both missiles passed at a distance of about one meter from the aiming point, although one of them did not hit the tank. The NAR S-8KOM was fired from two B8V20A units from horizontal flight (speed 160 km/h) to a range of 2000 meters and from pitching up (angle 16-18°, speed 220 km/h) to a range of 4000 meters. The main part of the missiles covered an area 400-600 meters long and 100-200 meters wide. While firing the NAR, one of the helicopter's engines experienced a surge. The 2A42 gun did not hit a single target due to poor-quality cold zeroing. There have been no purchases of Mi-28A helicopters from Sweden.

Tender in India for the supply of 22 attack helicopters

Based on the test results, the Indian military decided to purchase American AH-64D Apache helicopters rather than Russian Mi-28N Night Hunter attack helicopters. According to the Indian military, the Mi-28N does not meet the tender requirements on 20 points. A spokesman for the Western Air Command in New Delhi said that “both machines performed excellently, but the American one showed superiority in such key characteristics as increased capabilities and all-weather use.” The American helicopter was chosen based on the results of a lengthy tender, in which it won over the Russian Mi-28N attack helicopter. The cost of the contract, which will be implemented through the American foreign military assistance program FMS (Foreign Military Sales), will be $1.2 billion. The contract provides for the supply of 22 rotorcraft, from 4 to 6 spare engines and 12 AN/APG-78 Longbow fire control radars. The list of aviation weapons ordered by the Indian side includes 812 AGM-114L-3 Longbow Hellfire air-to-surface guided missiles, 542 AGM-114R-3 Hellfire II air-to-surface guided missiles and 245 Stinger missiles. block I-92H" air-to-air class.

Algeria

Russia has offered Algeria a number of Mi-28NE attack helicopters. Rosvertol hopes to sign a contract under which delivery of the Mi-28NE will begin between 2012 and 2022.

Contract with Iraq (2012)

In 2012, a contract was signed between the Russian Federation and Iraq for the supply of more than 10 Mi-28NEs as part of a larger package agreement totaling $4.3 billion. The contract also includes training of pilots and technical personnel, and the supply of weapons for the helicopter.

Comparison with analogues

Comparative performance characteristics of modern attack helicopters

Comparative performance characteristics of modern attack helicopters
Mi-28N	Ka-52	AH-64D Apache Longbow (Block III)	Bell AH-1Z Viper
Appearance
Year of adoption	2009	2011	2011	2011
Empty weight, kg	8095	7800	5165	5580
Fuel weight, kg	1500	1500	1100	n/a
Weight of combat load, kg	2300	2800	n/a	n/a
Built-in cannon	1 x 30 mm 2A42	1 x 30 mm 2A42	1 x 30mm M230	3 x 20mm M197
Suspension points	4	6	4	6
Maximum take-off weight, kg	12 000	10 800	10 400	8390
Power point	2 × “Motor Sich” VK-2500-02	2 × Motor Sich VK-2500	2 × General Electric T700-GE-701D	2 × General Electric T700-GE-401C
Engine power, l. With.	2 x 2200	2 x 2400	2 x 2000	2 x 1800
Maximum speed, km/h	300	310	265	300
Practical range (without PTB), km	450	520	480	680
Practical ceiling, m	5000	5500	5900	6100
Rate of climb, m/s	13,6	10,0	12,3	14,2
Cost, million USD	~8,0	~27,0	52,0-61,0	27,0-31,0
Augusta Westland T129	Eurocopter Tiger	Denel AH-2 Rooivalk	Kawasaki OH-1 Ninja
Appearance
Year of adoption	2012	2003	1999	2000
Empty weight, kg	2530	3060	5730	2450
Fuel weight, kg	n/a	1100	1470	n/a
Weight of combat load, kg	1200	n/a	1560	n/a
Built-in cannon	3 x 20mm 197B	1 x 30mm GIAT 30	1 × 20 mm F2	—
Suspension points	4	4	6	4
Maximum take-off weight, kg	5000	6600	8750	4000
Power point	2 × LHTEC CTS800-4A	2 × Rolls-Royce MTR390-E	2 × Turbomeca Makila 1K2	2 × Mitsubishi TS1-10QT
Engine power, l. With.	2 x 1360	2 x 1464	2 x 1500	2 x 890
Maximum speed, km/h	280	290	280	280
Practical range (without PTB), km	550	740	700	550
Practical ceiling, m	6000	4000	6100	n/a
Rate of climb, m/s	11,3	14,0	13,3	n/a
Cost, million USD	43,0-53,0	39,0	~40,0	n/a
Harbin Z-19	CAIC WZ-10	HAL LCH	HESA Shahed 285
Appearance
Year of adoption	—	2011	2013 (plan)	n/a
Empty weight, kg	2350	5400	3000	820
Fuel weight, kg	n/a	n/a	n/a	n/a
Weight of combat load, kg	n/a	1500	n/a	n/a
Built-in cannon	1 × 23 mm	1 × 23 mm	1 × 20 mm	1 × 7.62 mm
Suspension points	4	4	4	2
Maximum take-off weight, kg	4500	7500	5500	1450
Power point	2 × WZ-8A	2 × Pratt & Whitney Canada PT6C-67C	2 × HAL/Turbomeca Shakti	1 × Allison 250-C20J
Engine power, l. With.	2 x 850	2 x 1530	2 x 1200	1 x 420
Maximum speed, km/h	245	n/a	275	225
Practical range (without PTB), km	700	n/a	700	800
Practical ceiling, m	4900	n/a	6000	4150
Rate of climb, m/s	9,0	n/a	12,0	7,0
Cost, million USD	n/a	n/a	~22,0	n/a