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Giới thiệu về Su-27SKM và Su-30MK2 (PART-2)

Chủ đề trong 'Kỹ thuật quân sự nước ngoài' bởi gulfoil, 23/07/2007.

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  1. gulfoil

    gulfoil Thành viên mới

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    AIM-120D
    Mỹ quãng cáo loại tên lửa tầm xa này đã lâu,nghe đâu đã đua vào thử nghiệm và dùng cho F-22 nhưng tầm bắn thì mới là cho rằng hơn 50% so với loại 120C át chót 120 km nên tầm của AIM-120D là 180 km.Nhưng lại có tài liệu cho rằng là chỉ là 120km vì là cải tiến của AIM-120B hay giống như vậy.Hay cùng xem lại AIM-120 của Mỹ vậy.
    F-22 CTF tests AIM-120D noise, vibration
    by Christopher Ball
    95th Air Base Wing Public Affairs
    4/19/2006 - EDWARDS AIR FORCE BASE, Calif. -- The F-22 Combined Test Force here achieved another first when a Raptor flew with an AIM-120D missile in its weapons bay to test the effect of noise and vibration on the missile April 14.
    What was unique about the flight was that the weapon on board, the latest version of the AIM-120 Advanced Medium Range Air-to-Air Missile, or AMRAAM, is still being developed at Eglin Air Force Base, Fla.
    "This is a first for the Raptor, as the weapon hasn''t been fielded yet," said Capt. Jason Armstrong, an armament engineer with the 411th Flight Test Squadron here. "In the past, we''ve integrated existing weapons systems such as the JDAM into the aircraft. We''re doing this flight testing to help Eglin develop the weapon."
    Micah Besson and Adam Yingling, structural engineers with the 411th FLTS, explained the need for noise and vibration testing.
    "In previous tests with the C-7 (the AIM-120C), measurements determined that vibration levels in certain frequencies were harmful to the missile''s electronics, Mr. Besson said.
    The difference between the AIM-120D and the earlier C-model is in the navigation system, Mr. Yingling said.
    "The cards inside are arranged differently, and we''re not sure how vibro-acoustics will transmit," he said. "We needed to test the missile to validate Raytheon''s modeling and assumptions."
    Raytheon is the contractor responsible for designing and building the AIM-120 series missile.
    The test plan includes putting the aircraft through a variety of maneuvers throughout the flight regime of the aircraft, including working with the weapons bay doors open and closed, Mr. Yingling said.
    "We''re trying to give the missile the worst ride and expose it to the worst possible environment," Mr. Yingling added.
    He said the tests will allow Raytheon to gather data, which will be used in future qualification tests.
    AIM-120D AMRAAM
    Fabricante: Raytheon Systems
    Função principal: Missil ar-ar de longo alcance
    Alcance: 120 Km. Velocidade: 4500Km/h
    Tipo de ogiva : Alto Explosivo Peso da ogiva : 21Kg.
    Peso total: 157Kg Comprimento: 3.66 M.
    Diâmetro: 158mm Sistema orientação: GPS + Datalink
    O AIM-120D é um equipamento ainda em fase experimental
    O AIM-120D, anteriormente conhecido apenas como míssil experimental AIM-120C-8, é diferente do modelo C, principalmente pela inclusão de capacidade para utilização do sistema GPS. De resto, o AIM-120D parece ser relativamente idêntico ao AIM-120C-5.
    Ele terá um alcance aproximado de 120Km, (o dobro do alcance do AIM-120B) e uma capacidade idêntica no que respeita às dimensões da ogiva.
    O AIM-120D, é o míssil de longo alcance que equipará o caça americano F-22 Raptor. As suas novas capacidades, especialmente a sua utilização do GPS e a possibilidade de comunicar com o avião lançador, dão-lhe várias vantagens tacticas.
    Um dos problemas dos aviões «***os» invisíveis, é o de tornarem a sua presença conhecida logo que lançam os seus mísseis. Com o AIM-120D, será possível a um F-22 Raptor lançar o míssil a uma altitude mínima, sendo que este. Se dirige ao alvo, rasando o solo, e aproveitando a sua capacidade de reconhecer o terreno em que se encontra.
    O míssil só se dirige directamente contra o alvo, quando está já muito próximo, não permitindo assim a detecção do F-22, baseada na análise do seu trajecto.
    Informação genérica:
    O míssil AIM-120 AMRAAM (Advanced Medium-Range Air-to-Air Missile), ou míssil ar-ar de médio alcance avançado (o que implica que é disparado desde um avião, com o objectivo de destruir outro avião) é um míssil de longo alcance de última geração, de interceptação aérea. É guiado por radar activo, tem velocidade supersónica e possui a capacidade de operar com qualquer tempo, tanto de dia como de noite.
    O seu projecto iniciou-se em 1975 com o objectivo da substituição do míssil AIM-7 Sparrow, que já apresentava grandes falhas. Ao longo do projecto e programa, houve vários problemas técnicos, políticos e custos, que juntamente com os atrasos levaram quase ao seu cancelamento, mas em 1991 US Navy recebe o seu míssil AIM-120A AMRAAM, sendo a produção normal iniciada em Abril 1992. Ao longo dos tempos foram sendo desenvolvidas versões mais modernas do míssil tais como AIM-120 B/C
    O AIM-120 pode ser disparado de vários modos, tais como: ?o Dispara-e-esqueça ?; ?o LRI ?" Long Range Interceptation ?; ?o LOBL ?" Lock-on Before Launch ?..
    No modo ?odispara-e-esqueça? o míssil domina o alvo através do radar do avião que o dispara e no momento do lançamento, passa a ser controlado pelas ordens enviadas a partir do avião. Durante a fase intermédia do voo o míssil passa para um sistema de navegação por inércia, ou seja, o seu computador de bordo calcula o ponto de intercepção com base na rota e velocidade do alvo e como se trata de um sistema passivo o míssil fica imune as contra medidas do alvo. Quando o míssil atinge o ponto previsto para a intercepção, o seu radar é accionado e dirige o mesmo para o alvo, podendo o radar variar o seu comprimento de onda e a frequência dos impulsos para enganar as interferências dos aviões inimigos. Com a aproximação ao alvo uma espoleta de laser-radar explode a ogiva, que espalha um círculo de fragmentos.
    No modo LRI Long Range Interception o míssil actualiza os dados do ponto futuro onde deve ligar o radar, usando para esse efeito um datalink, estando a antena montada na traseira.
    No modo LOBL Lock-on Before Launch o míssil adquire o alvo antes do disparo
    O míssil tem também a capacidade Look-down e Shoot-down, podendo ser disparado contra alvos múltiplos.
    Este míssil revolucionou o combate ar-ar, pois conjuga as melhores características para o combate: velocidade, maneabilidade, alcance e precisão. Para poder conjugar estas características, o míssil tem um sistema triplo de orientação. Assim sendo, este míssil é suficientemente ágil para o combate a curta distância, mas também preciso para lá do campo visual, o AMRAAM é o mais mortífero míssil em serviço no ocidente sendo utilizado por vários países do Mundo.
    Este míssil também é utilizado em sistemas superfície-ar (SAM) tais como: NASAMS de origem Norueguesa, CLAWS e JLENS ambos de origem Americana.
    Autoria: Humberto Cardoso

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  2. Anonymous_boy

    Anonymous_boy Thành viên mới

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    Đúng như kế hoạch, đầu năm 2008 Su-35BM đã được bay thử chuyến đầu tiên.
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    Được Anonymous_boy sửa chữa / chuyển vào 19:25 ngày 22/02/2008
  3. huyphuc1981_nb

    huyphuc1981_nb Thành viên mới Đang bị khóa

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    Su ban đầu được thiết kế như là máy bay đa năng. Về không chiến, nó không đẩy cao yêu cầu đánh chặn nhữg mục tiêu mạnh nhất trên thế giới. Yêu cầu trong không chiến của Su là hiệu quả cao khi ra trận với những mục tiêu thông thường, ngang nó và thấp hơn. Nó chú trọng nhiều phòng thủ, giảm thương vong, kiểm soát bốn phía, tấn công và phát hiện, theo dõi nhiều mục tiêu cùng lúc.
    MiG-31 là máy bay không chiến chuyên nghiệp dùng để đánh những mục tiêu mạnh nhất như đạn đạo, vệ tinh hay những máy bay chiến đấu mạnh của đối phương. MiG-31 có antena không chiến lớn nhất, tốc độ lớn nhất trong số các máy bay chiến đấu thực tế trên thế giới.
    Các Su có tốc độ cao nhất từ M2 đến M2,5.
    MiG-31 có tốc độ cao nhất M2,8-khi này tầm bay 1200km. Tầm bay ở tốc độ 2500km/h là 3000km. MiG-31BM sử dụng radar đa tần, có tần số rất thấp 400MHz.
    Các máy bay Su thường phân ra các dòng đối đất Như Su-32, Su-34 hay Su-30 hai chỗ ngồi. Ngoài ra có các dòng chiến đấu trên không chuyên nghiệp như một số SU-27, SU-30 và các máy bay SU-33, SU-35, SU-37.
    Su-35 nối tiếp các dòng SU không chiến. Nó có radar kích thước lớn và động cơ mạnh. Khi mang nhẹ, tốc độ lên thẳng đứng là M1 (18 ngàn mét phút). Đánh gần thì Su hơn MiG. Hệ thống động cực của Su có bào khí, lái lực đẩy, diện tích lớn (hight aspect ratio)... để nhào lộn. Su lại có radar hậu, Irst hậu... để phòng thủ tốt. Nhìn chung, với tình hình các đạn đối không tầm xa phương Tây như AIM-120 thì Su trang bị đủ coi muỗi. Su đánh một lúc hàng chục con trực thăng, A-10... an toàn. Chứ MiG-31 đánh bọn ấy có khi bị bọn nó cắn trộm.
    Nhưng đánh xa thì radar của MiG mạnh hơn, tốc độ cao hơn, gia tốc mạnh hơn...
  4. OldBuff

    OldBuff Thành viên tích cực

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    Chán Phú-cầy!
    Trẻ nó hỏi Mig35 lại cứ trả lời Su35, so SuMk lại cứ lôi 35 vào. Cứ cái trò hỏi trâu nói ngựa này mà cãi nhau nổ phải biết. Ẩm khẩn trương hoạt huyết dưỡng não đê!
  5. gulfoil

    gulfoil Thành viên mới

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    --------------------------------------------------------------------------------------------------
    cảm ơn vì ảnh đẹp quá-Nga đã thu Su-35 trên mặt đất và trên không ,bay 55 phút ở độ cao 5000 m để thử động cơ 117S.Tất cả đều tốt đẹp, Nga sẽ trang bị cho quân đội Nga Su-35 vào 2-3 năm nữa và sẽ chào xuất khẩu cho tất cả các nước.TT Putin cũng vừ xem Su-35 và ký sắc lệnh xây dựng Maks thành trung tâm hàng không của Nga
    http://rapidshare.com/files/94122874/MAKS.flv.html
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    Được gulfoil sửa chữa / chuyển vào 09:41 ngày 23/02/2008
  6. huyphuc1981_nb

    huyphuc1981_nb Thành viên mới Đang bị khóa

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    À, thế à. Đang nói chuyện Su-35 với MiG-31. Hồi này mắt mũi kèm nhèm quá.
    MiG-35 là MiG-29 hiện đại hoá. MiG-29 là máy bay tiền tuyến đa năng rất giống cấu hình phương Tây, chứ không phải là máy bay chiến đấu trên không mạnh. Cấu hình MiG-29 có đường bay ổn định, linh hoạt, đa năng, nhỏ gọn tiết kiệm. Vì ảnh hưởng của Liên Xô đổ, mà phiên bản tiếp theo của MiG-29, ban đầu dự định là MiG-35 đã không được đưa vào thực tế.
    Do đó, MiG-29 có cấu hình khá cổ. Ví như, hệ thống radar của nó nhỏ, trong khi radar của Su hay MiG-31 rất lớn và toàn diện.
    MiG-35 hiện nay được trang bị radar AESA, tăng đường kính antena từ cỡ 600-700mm lên 1 mét. Nó tăng cường khả năng quét bản đồ, phát hiện mục tiêu trên đất và đối không đa năng.
  7. gulfoil

    gulfoil Thành viên mới

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    SU-35 ( SU-35BM)​
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    SU-35
    The Sukhoi company pins its near future at the global fighter market on the
    advent of the Su-35 super-manoeuvrable multirole fighter ?" a heavily upgraded
    Flanker-family member intended to fill the gap between various today?Ts versions of
    the Su-30MK fighter and a fifth-generation fighter whose deliveries might kick off in
    the later 2010s. ?oThe Su-35 is a Generation 4++ aircraft embodying numerous Gen.
    5 technologies. They ensure the Su-35?Ts superiority over all other Gen. 4 fighters
    under development throughout the world. During 2009?"2015, the cutting-edge
    technologies will make the Su-35 superior to all future multifunction fighters on
    the global market?, Sukhoi officials say. The plant in Komsomolsk-on-Amur is now
    building three Su-35 prototypes the first of which is due to kick off its flight trials
    as early as this summer. What kind of aircraft is the latest fighter and how does it
    differ from the Su-27 and Su-30 that are all the rage nowadays?
    The designation Su-35 has long been known in the world of aviation. Upgraded Su-27M fighters developed on order by the Russian Air Force have been displayed at international air shows repeatedly since 1992 under that name. On the verge of the new millennium, Su-35 competed in the tenders issued by the South Korean and Brazilian air forces, with aircraft made as far back as the early ?~90s acting as technology demonstrators.
    With the passage of time, it became clear that the aircraft needed a drastic upgrade of both its avionics and weapons to its airframe and powerplant for the aircraft to penetrate the global market and put up competition to the up-to-date and future foreign fighters.
    The latter was to be ensured by a considerable increase in the fighter?Ts service life. As a result, a concept of a comprehensively upgraded fighter of the Su-27 family, retaining
    the Su-35 designation, had matured by the middle of the first decade of the new century.
    So, what is new in the Su-35?Ts design? Firstly, the fighter shall be given an improved
    airframe featuring more titanium alloys, which is to result in a sizeable extension of
    the planê?Ts service life up to 6,000 hours or 30 years of operation, with the time before the first recon***ioning and between overhauls growing to 1,500 hours or 10 years of operation. The Su-35?Ts aerodynamic configuration is the same as that of the Su-27. Unlike the Su-30MKI, it will not have the canards but will feature the pitch, yaw and roll fly-by-wire control system without any mechanical control linkage. The fighter?Ts flight performance and manoeuvrability is to hike owing to the advanced KSU-35 fly-by-wire system under development by the MNPK Avionika company and handling the job used to be done by several individual systems on board the Su-27 ?" fly-by-wire system, automatic control system, stall warning and barrier, air data, landing gear wheel braking and nosewheel control systems. At the same time, the KSU-35 will handle proactive safety functions. Of the Su-35?Ts design features, mention also should be made of the lack of the Su-27?Ts typical upper air brake, due to its functions taken over by the differentially deflected rudders. Owing to an increase in the Su-35?Ts takeoff weight, its landing gear has been beefed up, with the nosegear made twin-wheel. The airframe embodies the radar abruption technologies slashing the fighter?Ts X-band radar cross-section within the ±60° sector.The redesigned airframe internal volumes allowed an increase in the Su-35?Ts fuel capacity by more than 20 per cent to 11,500 kg over 9,400 kg of the production Su-27. In ad***ion, the aircraft can carry two drop tanks 1,800 litres each on under-wing stores. With the drop tanks, the total fuel capacity measures 14,300 kg. The aircraft is also fitted with the drogue-and-hose mid-air refuelling system with the retractable refuelling probe on the port side of the nose section. The fuel transfer ratio is 1,100 litre/min.
    Fighter''s "heart"
    Another key feature distinguishing the Su-35 from its Su-27-family predecessors is its powerplant comprising deeply upgraded enhanced-thrust engine developed by NPO
    Saturn and dubbed ?~Product 117S?T. As far as the enginê?Ts design is concerned, it is a derivative of the production AL-31F, using the fifth-generation technology. It mounts the fan with a 3 % larger diameter (932 mm over 905 mm), advanced high- and low-pressure turbines and all-new digital control system. A provision has been made for using the thrust vector control nozzle similar to that of the AL-31FP. The upgrade has resulted in thrust hiking by 16 % to 14,500 kgf in afterburner mode and totaling 8,800 kg in the maximal non-afterburning mode. Compared to the current AL-31F, the new enginê?Ts service life is *****rge by 2?"2.7 times, with the time between overhauls increasing from 500 hours to 1,000 hours, time before first overhaul standing at 1,500 hours and assigned life spiking from 1,500 hours to 4,000 hours. Five prototype engines have been made
    under the Product 117S test and debugging programme. The first of them entered rig tests in 2003, with two more having been used in flight trials as part of the powerplant of the
    Su-27M No. 710 flying testbed. The test flight began in March 2004. About 30 test missions were flown at their first stage, including five on two engines. Then, the fourth example of Product 117 replaced the first prototype on the test bench while the fifth prototype was used as a backup during the flight tests.The rig tests have proven that the measures taken resulted in a much higher performance of the 117S engine compared with its prototype, with the thrust and specific fuel consumption requirements having been met
    in spades. Saturn?Ts division at the Lytkarino Machinebuilding Plant in the Moscow region launched the endurance bench tests of the 117S engine in support of the maiden flight of the Su-35, and one more engine of the type will undergo a set of special tests there. The production of the 117S is to be run by the Ufa Engine Production Association
    (UMPO) in the city of Ufa and NPO Saturn in the city of Rybinsk. The partners decided
    that all work on the 117S engine would be shared by Saturn and UMPO on parity basis. The Sukhoi design bureau, Saturn and UMPO has funded the programme out of their own pocket (40, 30 and 30 % respectively). Saturn built the first two production 117S
    engines and shipped them to KnAAPO for flight tests on board of the first Su-35 flying
    prototype earlier this year.
    Advanced avionics suite
    It looks like the key feature of the Su-35 is going to be its cutting-edge avionics suite
    wrapped around the information and control system designed for the functional, logical,
    informational and software integration of the avionics systems into a single suite and ensuring an interface between the crew and the equipment. The information and control system comprises two central digital computers, switching and data-processing gear and ?~glass ****pit?T display system.
    The Su-35?Ts ****pit management system comprises two huge MFI-35 full-colour
    multifunction liquid crystal displays (LCD), multifunction control panel with an in-built
    display processor, IKSh-1M wide-angle collimator HUD and control display unit.
    The MFI-35 multifunction displays with integral display processors measure 9x12'''' (15''''diagonally) and have the 1,400x1,050-pixel resolution. They are designed to receive,
    process and display in numerous windows graphic, numerical/letter and symbolic information, television imagery fed by onboard TV sensors and overlayed with numerical/letter and symbolic synthesised data as well as generate and feed digital video signals to the video recorder system. The multifunction display with the integral display processor is intended to show relevant information and issue commands by pushing buttons around it throughout the flight. The IKSh-1M collimator HUD with the integral processor is designed for the crew to watch the collimated display of sighting data in the form of marks, digits and other symbols. The HUD?Ts field of vision is 20°x30°.
    Control of the Su-35?Ts avionics, systems and weapons in its new ****pit is exercised by buttons and switches on the control stick and throttles and around the multifunction
    panels and displays. Thus, the fighters features the HOTAS concept. The Ramenskoye
    Design Company and other members of the Technocomplex corporation handle the
    development of the displays and some other of the Su-35?Ts avionics.
    ........................
  8. gulfoil

    gulfoil Thành viên mới

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    .......................
    ?oEyes? and ?oears?
    The fighter?Ts fire control system is based on the advanced Irbis-E phased-array radar
    system boasting the unique target acquisition range. The Irbis-E was developed by
    the Tikhmirov NIIP institute as a derivative of the Bars radar that fits the Su-30MKI,
    Su-30MKM and Su-30MKA fighters. The Irbis-E is an X-band multifunction radar with
    a 900 mm passive phased array mounted on a hydraulic actuator operating in azimuth
    and banking the promising computing system based on the Solo-35 digital computer. The
    passed array electronically scans 60° sectors in azimuth and elevation, while the hydraulic actuator ad***ionally steers the array mechanically to 60° in azimuth and to 120° in banking. With electronic control and mechanical steering of the array, the maximum beam angle increases to 120° in azimuth.The Irbis features a simultaneous 30-target acquisition and tracking capability in the track-while-scan mode. It engages two
    targets simultaneously with two semi-active radar homing missiles and up to eight targets with eight active radar homing missiles, including four of the targets out at 300 km
    or more. In the ground-attack mode, the radar handles terrain mapping (both ground
    and water) and ground target acquisition in the low-resolution ?~real-beam?T, medium-resolution Doppler beam sharpening (DBS) and high/extra-highresolution adaptive synthetic aperture focusing modes. Operating against aerial and ground threats at the same time, the Irbis-E maps the ground while keeping an eye on airspace or tracking an aerial threat with precision sufficient for attacking it with active radar homing missiles.
    The system features a head-on acquisition range of at least 350?"400 km for aerial targets
    with the 3 sq.m radar cross-section (RCS) and a pursuit acquisition range of at least
    150 km with a target traveling at 10,000 m or higher. The Irbis-E spots ?~super-low-observablê?T threats with the 0.01 sq.m RCS out at 90 km.
    As a derivative of the Bars radar, the Irbis features far superior characteristics than its
    predecessor, namely an operating frequency band that has been expanded more than twofold, the aerial target acquisition and azimuth tracking zone that grew from 70° to 120°, a far greater range, enhanced ECM immunity, etc.
    In these terms, the Irbis is on a par with the latest foreign designs, surpassing most of US and west European passive and active phased-array radars. The Irbis PAR has been under development by NIIP since 2004. To date, its prototypes have passed their rig tests, and the first of them has been fitted to the Su-30MK2 No 503 flying testbed for flight trials. The first flight of the flying testbed, which included the activation of the Irbis, took place at the Gromov LII flight research institute earlier this year, with the radar performing well in the air-to-surface mode. In April, the flying testbed was ferried to Akhtubinsk for com-prehensive flight trials. The basic objective of the first stage of testing the Irbis on board the aircraft are to test the new software and hardware, evaluate new operating modes and prove the design acquisition range characteristics. This phase of the trials is to be completed before year-end. Meanwhile, Tikhomirov NIIP and the GRPZ State Ryazan Instrument Plant are preparing the first Irbis sets for installation on Su-35 prototypes. Two radars are being prepared for fitting the second and fourth examples of the advanced fighter. The first of the two is slated for installation as early as August, with the radar to fit the other fighter to be ready before the end of the year. Another advanced subsystem of the Su-35?Ts fire control system is the OLS-35 infrared search-and-track (IRST) system combining a heat-seeker, a laser rangefinder/designator and a TV camera. The up-to-date electronic componentry, advanced algorithms and latest software predetermined the superiority of the OLS-35 over the IRSTs of other Su-27 and Su-30 families?T aircraft in terms of range, precision and reliability. The target search, acquisition and automatic tracking zone measures ±90° in azimuth and +60/-15° in elevation.
    The aerial target acquisition range (in nonafterburner mode) in the front hemisphere is
    at least 50 km and that in the rear hemisphere is at least 90 km. The laser rangefinder ranges aerial targets out at 20 km and ground targets out at 30 km with a precision of 5 m.
    In ad***ion, to ensure effective ground attack, the aircraft can carry an electro-optical
    pod ?" a laser/TV sighting system capable of acquisition, tracking, ranging and laser
    illumination of ground threats. The podded optronic system can be used, in particular, to
    cue laser-guided bombs to the target. Other advanced avionics of the Su-35 include new navigation system, communication systems ensuring operations as a package of fighters, and a very effective electronic countermeasures (ECM) system, which composition and specific elements are subject to the customer?Ts requirements.
    Weapons
    In ad***ion to eight R-27ER1, four R-27ET1 or R-27EP1 and twelve RVV-AE medium-range AAMs as well as six R-73E dogfight missiles, the Su-35?Ts weapons suite
    will comprise five advanced long-range airto- air missiles ( AAM ). The air-to-surface warload includes six Kh-29TE or Kh-29L tactical missiles, six Kh-31A antiship and Kh-31P antiradiation missiles, five advanced Kh-59MK long-range antiship missiles as
    well as five Kh-58UShE extended-range antiradiation missiles, three Club-family
    long-range antiship missiles (3M-14AE/3M-54AE1) and a Yakhont heavy long-range
    antiship missile. The guided bombs include up to eight TV-guided KAB-500Kr (OD),
    latest satellite-guided KAB-500S-E and laser-guided LGB-250 weapons as well as
    up to three KAB-1500Kr or KAB-1500LG TV or laser-guided bombs. The Su-35?Ts
    choice of bombs and rockets is the same as the one of the Su-30MK, but in the future it
    can employ improved or brand-new 500 kg and 250 kg bombs 80, 122 and 266/420 mm
    rockets, including those with laser guidance.The Su-35?Ts maximum payload on 12external hardpoints stands at 8,000 kg.
    Su-35 main data
    Length, m .............................................................21.9
    Wing span, m .......................................................15.3
    Height, m ...............................................................5.9
    Take-off weight, kg:
    - normal ...........................................................25,300
    - max ...............................................................34,500
    Combat load, kg .................................................8,000
    Fuel, kg:
    - internal tanks .................................................11,500
    - with two drop tanks .......................................14,300
    Max speed, km/h:
    - at sea level ......................................................1,400
    - at high altitude .................................................2,400
    Max Mach number ...............................................2.25
    Service ceiling, m ............................................18,000
    G-load .......................................................................9
    Range, km:
    - at sea level ......................................................1,580
    - at high altitude .................................................3,600
    - ferry range with two drop tanks .......................4,500
    Powerplant type ...................................... Saturn 117S
    Take-off thrust, kgf .......................................2Đ.14,500
    State of the programme
    The first Su-35 flying prototype has been completed and is in the final stages of its ground tests in the run-up of its flight trials. Its maiden flight is scheduled for this summer, and the aircraft is to be unveiled at the MAKS 2007 air show in late August. Two more Su-35 prototypes have followed the first example at the assembly line. They are to join the test programme in the later
    2007 or earlier 2008. At the same time, several flying testbeds derived from various Su-27 versions are used in the trials. The Su-35?Ts full-rate production and delivery are expected to commence as early as 2009 to continue until a fifth-generation fighter hits the market.
    [​IMG]
  9. gulfoil

    gulfoil Thành viên mới

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    Được gulfoil sửa chữa / chuyển vào 14:20 ngày 23/02/2008
  10. OldBuff

    OldBuff Thành viên tích cực

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