Tiềm Lực Tên Lửa của Nga

Có lẽ bàn về S-300 thì còn nhiều, nhưng mình muốn xem lại vấn đề đã từ lâu Nga muốn đưa S-300 lên Airborne,nhưng có lẽ vì bận về S-400 và do còn dánh để cho các máy bay thế hệ mới như Su-35 , Mig-35? nên còn rất ít thông tin.Vấn đề đa dạng hóa các loại tên lửa là Nga học ở Mỹ gần đây các loại tên lửa như Moskit, Yakhont, Brahmos, Uran, Club.. đều hạm đối hạm, bờ đối hạm, không đối hạm và ngầm đối hạm. Ngay cả tên lửa không đối không của Nga như RVV-AE ( R-77 ) cũng đã trình làng loại đất đối không tầm thấp ( 12 Km ).Tại triển lãm Le Bourget 2007 gần đây Nga đã đưa ra mô hình loại máy bay mới là Su-35 và Mig-35 với rõ ràng cùng các mô hình các loại tên lửa tầm xa mới như không đối không và không đối hạm/ đất. ( Các ban xem ảnh sau đây ).Riêng về S-300 thì Nga có hai loại tên lửa mới 9M96E và 9M96E2 , so với các loại cũ thì compact và gọn hơn-loại đầu có tầm bắn 40 km loại thứ hai có tầm bắn 120 km.Nếu đưa lên máy bay thì tầm bắn tăng được vài lần-đó là ý đồ đưa S-300 lên máy bay,Hiện tại Nga mới trình làng loại KS-172 mới được gọi là RVV-L có tầm bắn 400km ,nhiều nhười cho rằng nó được chế tạo trên cơ sở tên lửa của hệ thống S-300/S-400..Có lẽ tại MAKS-2007 sắp tới sẽ rõ vấn đề này hơn.
Su-35



Mig-35


MiG-29K


Tên lửa mới 9M96E và 9M96E2


KS-172 hay RVV-L

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In Russia, multipurpose ADM systems have, for years, been developed by an association of manufacturers, research institutes, and design bureaus. In recents years, their cooperative effort has led *****ch operational ADM systems as the S-300PMU, -1, -2, and their shipborne versions, designated Rif and Rif-M. These systems integrate, to a maximum possible degree, the abilities that make them effective against ballistic and aerodynamic targets. In the near future, the latest versions of the ADM systems, ground-based and shipborne, will receive the new 9M96E and 9M96E2 missiles developed by the Fakel Engineering Design Bureau and incorporated in the Oboronitelnye Systemy (Defense Systems) Ffinancial and Industrial Group.
These missiles are a new step in the creation of ADM systems. Obviously, the development of a new missile is a fairly long process and, therefore, it is very important for its designers to make a correct assessment of current trends in the evolution of air attack and air defense weapons.
Today, new generation of surface-to-air missiles (SAMs) have come to replace their predecessors. This tendency manifests itself most vividly in the replacement of medium-range SAMs which constitute the backbone of air defense systems in the majority of the world=s most developed nations. While basic components of the ADM systems such as radars, communications systems, and command posts are being improved gradually, surface-to-air missiles have made a dramatic qualitative leap forward in their development. This is primarily attributed to the revolutionary advances that have been made in the missile flight control methods and in the on-board equipment itself.
New generations of SAMs feature a combination of active homing heads with devices ensuring their high agility. This innovation has brought about a dPACtic increase in the missile target accuracy and has made it, basically, a sort of a kinetic weapon, i. e. a weapon that kills its target with a direct hit. Another feature of these new missiles is the significant reduction in their launching weight: from 1 - 1.8 t (U.S.-made Patriot PAC-1 and PAC-2, and=Russian-made S-300PMU SAM systems) to 300 - 500 kg (U.S.-made Patriot PAC-3, Franco-Italian Aster-15, and Aster-30, as well as Russian-made 9M96E and 9M96E2).
In October 1998, Russian missiles were displayed for the first time in October 1998 at the Defendory =98 exhibition in Athens. With such advanced foreign counterparts as the PAC-3 and Aster, the Russian missiles stood out from the rest in terms of their performance characteristics. The 9M96E and 9M96E2 missiles carry similar onboard equipment, payload and are identical in construction. The only difference between the two missiles is that the 9M96E2 model is equipped with a more powerful propulsion motor featuring a greater power-to-weight ratio. With little difference in size and weight, the 9M96E and 9M96E2 missiles may engage targets at a range of 1 to 40 km (9M96E) and 120 km (9M96E2) and at an altitude of 5 m to 20 km (9M96E) and 30 km (9M96E2), outperforming their foreign counterparts.
To develop new missiles, engineers and designers had to revise tra***ional approaches, devise fundamentally new engineering solutions, review previous experience and investigate current trends. The experience gained by Fakel in developing reliable high-rate-of-fire missiles was also taken into account. The new missile concept and architecture have been chosen in close cooperation with the country=s leading research and design organizations. Owing to this coordinated effort, the new developments incorporate the latest engineering advances and have been devised with a view to virtually all major SAM development trends. Confident of the precision and soundness of the assessments made, Fakel developed the required technical documentation for the missiles, using the most advanced CAD methods. The flight tests performed in the late 1980s demonstrated the basic advantages of these new missiles.
As the work on the 9M96E and 9M96E2 missiles was going on, all efforts were focused on creating highly effective surface-to-air missiles capable of destroying all currently operational and future missiles and aircraft.
The primary aim of an air defense missile is to destroy the incoming missile=s payload in the interception phase, lest it should fall in the area of a protected installation (e.g. near an electric power station or ship). The attacking missile=s payload can be destroyed either by a direct hit on the payload section or, in the event of an insignificant miss, by the SAM=s warhead splinters
To understand how this mission can be accomplished by new missiles, consider the principle of their operation in the target interception phase. Unlike foreign counterparts, the 9M96E (9M96E2) missile uses the so-called =cold= vertical lift-off: before its sustainer motor is started the missile is expelled from its container to a height of over 30 m. While the missile is ascending, its gas-dynamic system causes the weapon to tilt towards the target. Once the sustainer motor is started the missile assumes inertial control via radio link at the initial and mid-course legs of the flight path (to assure maximum noise protection). In the target interception phase, the missile switches over to the radar homing mode. Whenever the missile has to perform a maneuver to get to its rendezvouz point it can activate a =superagility= mode, for which purpose the gas-dynamic control system is enabled. The system increases the missile=s aerodynamic overload capacity by about 20 units within 0.025 seconds.
It should be pointed out here that the =superagility= feature of the 9M96E and 9M96E2 missiles, augmented by their enhanced guidance accuracy, provides a guided path most suitable for target engagement by the missile, as well as the lethality of the missile=s payload.
The introduction of a considerable number of new components in the new missiles called for a profound optimization of their design features, component units and assemblies on the ground in the most realistic operational and flying con***ions. A multitude of laboratory and rig tests (fire, heat resistance, environmental, weather, special electronic, etc.) were carried out.
While development work on the 9M96E and 9M96E2 missiles was in progress, extensive use was made of advanced computer-aided modeling methods which allowed the designers to use the results of the ground and flight-rig tests of individual components as the input data. The results of the tests indicated the ability of the new missiles to destroy the payload of the Scud ballistic missile (or its updated version) and the Harpoon antiship missile with a probability of 70 percent. The 9M96E and 9M96E2 missiles carry a 24-kg warhead which produces a controlled killing zone. The use of such a warhead makes these missiles highly effective against all aircraft types.
The provision of the 9M96E and 9M96E2 missiles with the data-ware-controlled payload is another way to enhance the effectiveness of modern air attack means. This kind of payload is designed to =stop= a piloted target, i.e. cause its structural disintegration upon interception, and to destroy (disable) the payload carried by remote-piloted vehicles (RPVs).
The payload is activated via radio fuze which uses all the data available on board the missile for its adaptation to the con***ions of the target-missile rendezvous. The radio fuze sets the time the payload should be detonated. To destroy the vulnerable portion of the target, the set time must agree with the velocities of fragments and fragmentation spray direction.
The directed spray is achieved with the aid of a controllable blast-fragmentation warhead using a multipoint initiation system. Once the radio fuze generates a command for the initiation of the warhead in the controlled mode in the presence of the =miss= information, the system activates initiation of the explosive charge at peripheral points facing the required direction (towards the target). As a result, the energy of the explosion is concentrated in this direction and the bulk of the fragmentation field is flung towards the target at an increased velocity. If there is no =miss= information in the system, the warhead=s explosive charge is initiated at the center and fragments scatter symmetrically in all directions.
The 9M96E and 9M96E2 missiles are fully adapted for use in air defense systems of the Air Force and Navy. A considerable reduction in their size and weight has made it possible to accommodate four missiles into one container, which has the same dimensions as the one used by the S-300PMU, Rif-5V55R, 48N6E and 48N6E2 ADM systems. The greater number of missiles at hand makes the system more flexible in action, and allows it to remain operational for a longer time before running out of missiles as a result of heavy attacks conducted by the enemy using precision-guided munitions or RPVs.
Fakel=s designers and engineers have developed missiles which outperform their foreign counterparts, including American and French ones, and incorporate the latest technological advances in the field made by the military-industrial complexes of the USA and Western Europe.
These new missiles fully meet the requirements of the 21st century. They incorporate the advances of Russia=s missile-building industry, science and technology made over the past decade, and demonstrate that Russia, despite the economic and financial crisis, is still one of the world=s leading missile-producing nations.

Basic characteristics of the 9M96E and 9M96E2 missiles
9M96E 9M96E2
Target engagement envelope, km:
Range:
minimum 1 1
maximum 40 120
Altitude:
minimum 0.005 0.005
maximum 20 30
Weight, kg:
missile 333 420
warhead 24 24
container with four missiles 2,300 2,700
Average velocity, m/s 750 1,000
First shot hit probability:
piloted target 0.9 0.9
unpiloted target 0.8 0.8
target=s payload 0.7 0.7

Quả này bản xuất khẩu có tầm bắn 300km, nếu NC có độ chục quả mang táng AWAC của anh béo cũng được, có điều máy bay cua NC hình như không mang được. Bác guifoil dạo này quảng cáo tên lửa Nga nhiều nhỉ ... .

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À vì có dịp Mỹ Nga triển khai NMD của mình lại anh Nga đưa ra mấy loại tên lửa mới cũng hay lắm nên xem lại cùng các bạn S-300.Mình muốn bàn thêm về S-400 và đưa vài ảnh S-300 của TQ, ảmh thật trực chiến của S-300V, nhưng thấy dài quá.Bạn thấy thế nào ?
Buồng điều khiển của S-300PMU2

Để nghỉ chút xíu trước khi bàn tiếp về S-300/S-400 và các tên lửa tấn công của Nga,mình muốn nói về việc đa dạng hoá đa chức năng của một loại tên lửa bây giờ trrên thí dụ về tên lửa Brahmos là loại tên lửa liên doanh giữa Nga và Ấn Độ.
Brahmos

Bờ đối hạm

Không đối hạm
Il-38SD ( Máy bay chông tầu )

Su-30MKI



Ngầm đối hạm

Hạm đối hạm

nhà mình cần những con này là chủ yếu,thay mấy em SS-N-3 Shaddock ,ngắn trên mấy em Su-30 MK2V và thay mấy quả SS-N-2 termit trên mấy em tarantul,thế là cũng đủ để thèng tung của biết điều hơn roài
Được terminaterx300 sửa chữa / chuyển vào 12:01 ngày 22/07/2007

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At the beginning of 2007, Russia maintained approximately
5,600 operational nuclear warheads for delivery by ballistic
missiles, aircraft, cruise missiles and torpedoes, according
to the latest Nuclear Notebook published in the Bulletin of
the Atomic Scientists. The Russian Notebook, which is
written by Hans M. Kristensen of FAS and Robert S. Norris
of NRDC, breaks down the Russian arsenal into roughly
3,300 warheads for delivery by strategic weapon systems
and 2,300 warheads for delivery by tactical systems.
BRAHMOS đây

Tác chiến đây

Tham Khảo nha...
In ad***ion to 5600 operational warheads, the
Notebook estimates that Russia has a stock of roughly
9,400 warheads intended as a reserve or
awaiting dismantlement, for a total stockpile of approximately
15,000 warheads.
May 9, 2007.
........
Russia and the United States apparently have decided not
to extend the START agreement when it expires in 2009.
The demise of the treaty will effect the number of warheads
deployed on Russia''s ICBMs. Russia has already
announced its intention to change the warhead loading on
its Topol-M ICBMs.