::EK:: Air Club.... Only 4 Aviation Lovers

Hashan dis

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    Background

    Does the United States Air Force or one of America's intelligence agencies have a secret hypersonic aircraft capable of a Mach 6 performance? Continually growing evidence suggests that the answer to this question is yes. Perhaps the most well-known event which provides evidence of such a craft's existence is the sighting of a triangular plane over the North Sea in August 1989 by oil-exploration engineer Chris Gibson. As well as the famous "skyquakes" heard over Los Angeles since the early 1990s, found to be heading for the secret Groom Lake installation in the Nevada desert, numerous other facts provide an understanding of how the aircraft's technology works. Rumoured to exist but routinely denied by U.S. officials, the name of this aircraft is Aurora. People are also referring to it as the SR-75 Penetrator.
    The outside world uses the name Aurora because a censor's slip let it appear below the SR-71 Blackbird and U-2 in the 1985 Pentagon budget request. Even if this was the actual name of the project, it would have by now been changed after being compromised in such a manner. The plane's real name has been kept a secret along with its existence. This is not unfamiliar though, the F-117a stealth fighter was kept a secret for over ten years after its first pre-production test flight. The project is what is technically known as a Special Access Program (SAP). More often, such projects are referred to as "black programs".
    So what was the first sign of the existence of such an aircraft? On 6 March 1990, one of the United States Air Force's Lockheed SR-71 Blackbird spyplanes shattered the official air speed record from Los Angeles to Washington's Dulles Airport. There, a brief ceremony marked the end of the SR-71's operational career. Officially, the SR-71 was being retired to save the $200-$300 million a year it cost to operate the fleet. Some reporters were told the plane had been made redundant by sophisticated spy satellites.
    But there was one problem, the USAF made no opposition towards the plane's retirement, and congressional attempts to revive the program were discouraged. Never in the history of the USAF had a program been closed without opposition. Aurora is the missing factor to the silent closure of the SR-71 program. Testing such a new radical aircraft brings immense costs and inconvenience, not just in the design and development of a prototype aircraft, but also in providing a secret testing place for aircraft that are obviously different from those the public are aware of.
    Groom Dry Lake, in the Nevada desert, is home to one of America's elite secret proving grounds. Here is Aurora's most likely test location. Comparing today's Groom Lake with images of the base in the 1970s, it is apparent that many of the larger buildings and hangars were added during the following decade. Also, the Groom Lake test facility has a lake-bed runway that is six miles long, twice as long as the longest normal runways in the United States. The reason for such a long runway is simple: the length of a runway is determined either by the distance an aircraft requires to accelerate to flying speed, or the distance that the aircraft needs to decelerate after landing. That distance is proportional to the speed at which lift-off takes place. Usually, very long runways are designed for aircraft with very high minimum flying speeds, and, as is the case at Edwards AFB, these are aircraft that are optimised for very high maximum speeds. Almost 19,000 feet of the runway at Groom Lake is paved for normal operations.
    Lockheed's Skunk Works, now the Lockheed Advanced Development Company, is the most likely prime contractor for the Aurora aircraft. Throughout the 1980s, financial analysts concluded that Lockheed had been engaged in several large classified projects. However, they weren't able to identify enough of them to account for the company's income. Technically, the Skunk Works has a unique record of managing large, high-risk programs under an incredible unparalleled secrecy. Even with high-risk projects the company has undertaken, Lockheed has a record of providing what it promises to deliver.

    Aurora Specifications

    Speed:
    Speeds are reported to be in the range of Mach 5-8.

    Length:
    110 feet (33.5 meters)

    Wingspan:
    60 feet (18.2 meters)

    Ceiling:
    150,000 feet (28.4 miles)
    aurora.jpg
     

    Hashan dis

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    JF-17 Thunder, FC-1 Fierce Dragon

    The Joint Fighter-17 (JF-17) Thunder, also known as the Fighter China-1 (FC-1) Fierce Dragon (Xiaolong) in China (initially known as Super-7), is a single-seat multirole fighter aircraft co-developed by China and Pakistan. Currently four prototypes are flying. A joint venture between CAC and Pakistani Aeronautical Complex (PAC) will begin initial production of 16 aircraft in 2006. The designation of the aircraft in the Pakistani Air Force (PAF) is Joint Fighter-17 (JF-17) Thunder. It is still not clear whether the Pakistan Air Force (PLA) Air Force will eventually acquire any of this aircraft. If they do introduction can be as soon as 2007. Overview

    The JF-17 is designed to meet the tactical and strategic needs of the Pakistani Air Force with a minimal reliance on imports from other countries. In addition, the requirement was for the aircraft to have sufficient space for future upgrades and/or equipment specified by export buyers. The JF-17 is considered to be in the "mid-high-tech class" of fighter aircraft. Project

    The JF-17 is being built by Chengdu Aircraft Industry Corporation (CAC), and the Pakistan Aeronautical Complex (PAIC) is expected to license produce it at a later stage. Initial reports claimed that the aircraft was based on the design of the MiG-33, a proposed single-engined version of the MiG-29, which was rejected by the Soviet Air Force. However, the FC-1/JF-17 is instead derived from the "Super Seven" project, not the Project 33 (not to be confused with the MiG-33) or the failed Chengdu J-9. Indications are that MiG assisted the program by contributing their light fighter design as well as providing additional design & development assistance.

    The project is expected to cost about $500 million (USD), divided equally between China and Pakistan, while each individual aircraft is expected to have a fly-away cost of $15-20 million. Pakistan has announced that it will procure 150 planes by 2015, which will replace the MiG-21 derived Chengdu F-7. Other countries which have expressed interest in purchasing the JF-17 are Egypt, Bangladesh, Nigeria, Burma, Zimbabwe, Morocco and Algeria. History

    In 1986, China signed an agreement with Grumman to develop an upgrade/replacement for the J-7 known as the "Super 7". The program was cancelled in 1990, primarily due to worsening relations with the US following the Tiananmen Square protests of 1989. However, CAC kept the program alive by providing low-level funding from its own resources. After US sanctions were imposed on Pakistan in 1990, Pakistan also became interested in the project. In June 1999, Pakistan and China made an agreement to restart the program with Pakistan paying about 50% of the development costs. The project became known as JF-17 in Pakistan and FC-1 in China.

    The first prototype was rolled out on 31 May 2003, conducted its first taxi trials on 1 July, and made its first flight on 24 August of the same year. The prototype 03 made its first flight in April 2004. On April 28 2006, the prototype 04 made its first flight with fully operational avionics. Serial production was expected to begin in June 2006 and the first 16 aircraft would be rolled out in early 2007. Serial production from 2007-2008 will be at an annual 10-15 planes per year while in 2008+ it will be at 25-30 planes per year.

    President Of Pakistan Pervez Musharraf has declared in the Independence day speech on 14th August 2006 that the aircraft will be flying in the Pakistani sky on the 23rd March 2007.


    SPECIFICATIONS JF-17 / FC-1 Role Multi-role fighter Crew 1 First Flight September 3, 2003 Enter Service 2006-2007 Manufacturer (CAC) China & Pakistan Aeronautical Complex Engine 1 x RD-93 turbofan (Russian-made), rated 49.4kN dry / 81.4kN with afterburning. Length 14.00 m Wingspan 9.00 m Height 5.10 m Empty Weight 6,321 kg Normal take-off weight 9,100 kg Max take-off 12,700 kg; Maximum Weapon Load 3,600 kg Maximum Speed Mach 1.6 (ProtoType-1,2 and 3) Ferry range 3,000 km Operational Radius 1352 km Service Ceiling 16500 m Maximum Climb Rate N/A G-Limits +8.5 Weapons

    Weapons

    The aircraft has 7 stores stations, including one under the fuselage, 4 under the wings, and 2 wingtip mounted, with up to 3,800kg weapon payload. The aircraft can carry a special pod allowing day/night delivery of laser-guided weapons. In addition, it can also carry unguided weapons such as iron bomb and unguided rocket launchers.

    The JF-17 / FC-1 has beyond-vision-range (BVR) attack capability with the SD-10 medium-range air-to-air missile (MRAAM) developed by China Leihua Electronic Technology Research Institute (LETRI, also known as 607 Institute). The aircraft also carries two short-range AAMs on its wingtip-mounted launch rails. The options include U.S. AIM-9P and Chinese PL-6, PL-8, and PL-9.

    jf17.jpg

    3,800 kg payload
     

    Hashan dis

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    Tejas / Light Combat Aircraft (LCA)



    The Tejas (formerly known as LCA; Light Combat Aircraft) is India's second indigenous jet fighter design, after the HF-24 Marut of the 1950s. It's the world's smallest, light weight, multi-role combat aircraft designed to meet the requirements of the Indian Air Force as its frontline multi-mission single seater tactical aircraft during the period 2000 - 2020. Development began in 1983; the basic design was finalised in 1990; the first prototype rolled out on 17 November 1995. On 04 January 2001 at 10.18 a.m. the first LCA Prototype TD-1 (Technology Demonstrator-1), finally took off on its first flight from Yelahanka AFS.

    The configuration is a delta wing, with no tailplanes or foreplanes, and a single vertical fin. The LCA is constructed of aluminium-lithium alloys, carbon-fibre composites, and titanium. The design incorporates "control-configured vehicle" concepts to enhance manoeuvrability, and quadruplex fly-by-wire controls. Both prototypes are powered by General Electric F404-GE-F2J3 engines, but an indigenous engine, the GTX-35VS Kaveri, is being developed for the production Tejas.
    The Tejas (LCA) is a small, lightweight, supersonic, multi-role, single-seat fighter designed primarily to replace the MiG-21 series of aircraft of Indian Air Force as its front-line multi-mission single-seat tactical aircraft. The LCA integrates modern design concepts like static instability, digital fly-by-wire flight control system, integrated avionics, glass cockpit, primary composite structure, multi-mode radar, microprocessor based utility and brake management systems.

    Short takeoff and landing, high maneuverability with excellent maintainability and a wide range of weapon fit are some of Tejas' features. Two aircraft technology demonstrators are powered by single GE F404/F2J3 augmented turbofan engines. For maintenance the aircraft has more than five hundred Line Replaceable Units (LRSs), each tested for performance and capability to meet the severe operational conditions to be encountered. Major subsystems like fly-by-wire digital flight control system, integrated avionics, hydraulic and electricalsystems, environmental control system, fuel system etc., are being tested to ensure performance and safety. Following satisfactory subsystem test results the flight test program of the Tejan began in 2001. Production will start in 2007

    The Tejas has been designed and developed by a consortium of five aircraft research, design, production and product support organizations pooled by the Bangalore-based Aeronautical Development Agency (ADA), under Department of Defense Research and Development Organization (DRDO). Hindustan Aeronautics Limited (HAL) is the Principal Partner in the design and fabrication of the LCA and its integration leading to flight testing. Several academic institutions from over the country have participated in the development of design and manufacturing software for LCA. National teams formed by pooling the talents and expertise in the country are entrusted with the responsibility of the development of major tasks such as development of carbon composite wing, design, design of control law and flight testing. Several private and public sector organizations have also supported design and manufacture of various subsystems.

    Various international aircraft and system manufacturers are also participating in the program with supply of specific equipment, design consultancy and support. For example, GE Aircraft Engines provides the propulsion and Lockheed Martin the flight control system.

    Tejas or Light Combat Aircraft (LCA)

    The Indian Tejas is the world's smallest, light weight, multi-role combat aircraft designed to meet the requirements of Indian Air Force as its frontline multi-mission single-seat tactical aircraft to replace the MiG-21 series of aircraft. The delta wing configuration , with no tailplanes or foreplanes, features a single vertical fin. The Tejas is constructed of aluminium-lithium alloys, carbon-fibre composites, and titanium. Tejas integrates modern design concepts and the state-of-art technologies such as relaxed static stability, flyby-wire Flight Control System, Advanced Digital Cockpit, Multi-Mode Radar, Integrated Digital Avionics System, Advanced Composite Material Structures and a Flat Rated Engine.

    The Tejas design has been configured to match the demands of modern combat scenario such as speed, acceleration, maneuverability and agility. Short takeoff and landing, excellent flight performance, safety, reliability and maintainability, are salient features of Tejas design. The Tejas integrates modern design concepts like static instability, digital fly-by-wire flight control system, integrated avionics, glass cockpit, primary composite structure, multi-mode radar, microprocessor based utility and brake management systems.

    The avionics system enhances the role of Light Combat Aircraft as an effective weapon platform. The glass cockpit and hands on throttle and stick (HOTAS) controls reduce pilot workload. Accurate navigation and weapon aiming information on the head up display helps the pilot achieve his mission effectively. The multifunction displays provide information on engine, hydraulics, electrical, flight control and environmental control system on a need-to-know basis along with basic flight and tactical information. Dual redundant display processors (DP) generate computer-generated imagery on these displays. The pilot interacts with the complex avionics systems through a simple multifunction keyboard, and function and sensor selection panels. A state-of-the-art multi-mode radar (MMR), laser designator pod (LDP), forward looking infra-red (FLIR) and other opto-electronic sensors provide accurate target information to enhance kill probabilities. A ring laser gyro (RLG)-based inertial navigation system (INS), provides accurate navigation guidance to the pilot. An advanced electronic warfare (EW) suite enhances the aircraft survivability during deep penetration and combat. Secure and jam-resistant communication systems, such as IFF, VHF/UHF and air-to-air/air-to-ground data link are provided as a part of the avionics suite. All these systems are integrated on three 1553B buses by a centralised 32-bit mission computer (MC) with high throughput which performs weapon computations and flight management, and reconfiguration/redundancy management. Reversionary mission functions are provided by a control and coding unit (CCU). Most of these subsystems have been developed indigenously.

    The digital FBW system of the Tejas is built around a quadruplex redundant architecture to give it a fail op-fail op-fail safe capability. It employs a powerful digital flight control computer (DFCC) comprising four computing channels, each powered by an independent power supply and all housed in a single line replaceable unit (LRU). The system is designed to meet a probability of loss of control of better than 1x10-7 per flight hour. The DFCC channels are built around 32-bit microprocessors and use a safe subset of Ada language for the implementation of software. The DFCC receives signals from quad rate, acceleration sensors, pilot control stick, rudder pedal, triplex air data system, dual air flow angle sensors, etc. The DFCC channels excite and control the elevon, rudder and leading edge slat hydraulic actuators. The computer interfaces with pilot display elements like multifunction displays through MIL-STD-1553B avionics bus and RS 422 serial link. The digital FBW system of the Tejas is built around a quadruplex redundant architecture to give it a fail op-fail op-fail safe capability. It employs a powerful digital flight control computer (DFCC) comprising four computing channels, each powered by an independent power supply and all housed in a single line replaceable unit (LRU). The system is designed to meet a probability of loss of control of better than 1x107 per flight hour. The DFCC channels are built around 32-bit microprocessors and use a safe subset of Ada language for the implementation of software. The DFCC receives signals from quad rate, acceleration sensors, pilot control stick, rudder pedal, triplex air data system, dual air flow angle sensors, etc. The DFCC channels excite and control the elevon, rudder and leading edge slat hydraulic actuators. The computer interfaces with pilot display elements like multifunction displays through MIL-STD-1553B avionics bus and RS 422 serial link.

    Multi-mode radar (MMR), the primary mission sensor of the Tejas in its air defence role, will be a key determinant of the operational effectiveness of the fighter. This is an X-band, pulse Doppler radar with air-to-air, air-to-ground and air-to-sea modes. Its track-while-scan capability caters to radar functions under multiple target environment. The antenna is a light weight (<5 kg), low profile slotted waveguide array with a multilayer feed network for broad band operation. The salient technical features are: two plane monopulse signals, low side lobe levels and integrated IFF, and GUARD and BITE channels. The heart of MMR is the signal processor, which is built around VLSI-ASICs and i960 processors to meet the functional needs of MMR in different modes of its operation. Its role is to process the radar receiver output, detect and locate targets, create ground map, and provide contour map when selected. Post-detection processor resolves range and Doppler ambiguities and forms plots for subsequent data processor. The special feature of signal processor is its real-time configurability to adapt to requirements depending on selected mode of operation.

    Seven weapon stations provided on Tejas offer flexibility in the choice of weapons Tejas can carry in various mission roles. Provision of drop tanks and inflight refueling probe ensure extended range and flight endurance of demanding missions. Provisions for the growth of hardware and software in the avionics and flight control system, available in Tejas, ensure to maintain its effectiveness and advantages as a frontline fighter throughout its service life. For maintenance the aircraft has more than five hundred Line Replaceable Units (LRSs), each tested for performance and capability to meet the severe operational conditions to be encountered.

    Hindustan Aeronautics Limited (HAL) is the Principal Partner in the design and fabrication of Tejas and its integration leading to flight testing. The Tejas has been designed and developed by a consortium of five aircraft research, design, production and product support organizations pooled by the Bangalore-based Aeronautical Development Agency (ADA), under Department of Defense Research and Development Organization (DRDO). Various international aircraft and system manufacturers are also participating in the program with supply of specific equipment, design consultancy and support. For example, GE Aircraft Engines provides the propulsion.

    The first prototype of Tejas rolled out on 17 November 1995. Two aircraft technology demonstrators are powered by single GE F404/F2J3 augmented turbofan engines. Regular flights with the state-of-the-art "Kaveri" engine, being developed by the Gas Turbine Research Establishment (GTRE) in Bangalore, are planned by 2002, although by mid-1999 the Kaveri engine had yet to achieve the required thrust-to-weight ratio.

    The Tejas is India's second attempt at an indigenous jet fighter design, following the somewhat unsatisfactory HF-24 Marut Ground Attack Fighter built in limited numbers by Hindustan Aeronautics Limited in the 1950s. Conceived in 1983, the Tejas will serve as the Indian air force's frontline tactical plane through the year 2020. The Tejas will go into service around 2007.

    Following India's nuclear weapons tests in early 1998, the United States placed an embargo on the sale of General Electric 404 jet engines which are to power the Tejas. The US also denied the fly-by-wire system for the aircraft sold by the US firm Lockheed-Martin. As of June 1998 the first flight of the Tejas had been delayed due to systems integration tests. The first flight awaits completion of the Digital Flight Control Systems, being developed by the Aeronautical Development Establishment (ADE).
    Type: Tejas / LCA
    Country: India
    Function: fighter
    Crew: 1
    Engines: 1 (83.4 kN GTRE GTX-35VS augmented turbofan)
    Wing Span: 8.20 m
    Length: 13.20 m
    Empty Weight: 5500 kg
    Ceiling: 16400 m
    Range: 850 km
    Armament: GSh-23 twin-barrel 23mm cannon (220 rounds);
    7 hardpoints, max external load over 4000 kg
    Unit cost: 21 million USD

    lca.jpg
     

    Hashan dis

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    gayan kalhara said:
    But indian means ether USA, RSS, China.... tech.. they don't have own.. only copies.. as i know..
    ya i saw india build satellite also

    its name is Chandrayaan-1
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    Last edited:

    gayan kalhara

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    Hashan dis said:
    ya i saw india build satellite also

    its name is Chandrayaan-1
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    it's also a combine of Russian sous and US design
     

    Hashan dis

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    The V-22 Osprey is destined to be the first operational tilt-rotor aircraft. It has the configuration of the smaller V-15, with rotating engine pods set at the wingtips. The fuselage is box-like. The wing is set above the fuselage, and can rotate to be parallel with the fuselage, for storage. The tiltrotor aircraft takes off and lands like a helicopter. Once airborne, its engine nacelles can be rotated to convert the aircraft to a turboprop airplane capable of high-speed, high-altitude flight. The USAF received the first CV-22 Osprey in November 2006.
    Type: Bell-Boeing V-22 Osprey
    Country: USA
    Function: multi-mission military aircraft
    Year: 2006
    Crew: 3; 2 pilots
    Engines: 2 * Rolls-Royce AE1107C-Liberty turboshafts, 6150 hp (4,586 kW) each.
    Total Wing Span: 25.55 m
    Length fuselage: 17.48 m
    Width Rotors turning: 25.55 m
    Rotor diameter: 11.58 m
    Height: 5.38 m (stabilizer), 6.63 m (Nacelles vertical)
    Empty Weight: 15032 kg
    Max.Weight Vert. T/O: 23495 kg
    Max.Weight: 27442 kg
    Max. Speed: 510 km/h
    Rate of climb: 11.8 m/s
    Ceiling: 7925 m
    Max. Range (ferry): 4239 km
    Armament: up to 8463 kg (20000 pounds) of internal or external cargo.

    V-22 Osprey Description & Purpose

    The V-22 Osprey is a joint service multi-role combat aircraft utilizing tiltrotor technology to combine the vertical performance of a helicopter with the speed and range of a fixed wing aircraft. With its engine nacelles and rotors in vertical position, it can take off, land and hover like a helicopter, but once airborne, its engine nacelles can be rotated to convert the aircraft to a turboprop airplane capable of high-speed, high-altitude flight. This combination allows the V-22 to fill an operational niche no other aircraft can approach.

    The Osprey can carry 24 combat troops, or up to 20,000 pounds of internal cargo or 15,000 pounds of external cargo, at twice the speed of a helicopter. It includes crosscoupled transmissions so either engine can power the rotors if one engine fails. The rotors can fold and the wing rotates so the aircraft can be stored on board an aircraft carrier or assault ship. V-22 Osprey Development

    The Osprey's development processes have been long and controversial. When the development budget, first set at $2.5 billion in 1986, had reached $30 billion in 1988, then-Defense Secretary Dick Cheney zeroed out the budget, but was overruled by Congress. The first flight occurred on March 19, 1989.

    The MV-22B is equipped with a glass cockpit, which incorporates four Multi-Function Displays (MFDs) and two Communications Display Units (CDUs), allowing the pilots to display a variety of layers, including: digimaps centered or decentered on current position, FLIR imagery, primary flight instruments, navigation (TACAN, VOR, ILS, GPS, INS) and system status. The flight director panel of the Cockpit Management System (CMS) allows for fully-coupled (aka: autopilot) functions which will take the aircraft from forward flight into a 50' hover with no pilot interaction other than programming the system.

    The aircraft was originally designed to be pressurized, but the rotating wing (for shipboard stowage) makes it difficult to properly seal the cabin. As a result, pilots and aircrew must wear oxygen masks while flying above 10,000 feet (3,000 m). The Osprey uses an on-board oxygen generating system (OBOGS) which enriches ambient air by filtering out the oxygen. The nitrogen remaining is then routed to the fuel cells to fill the ullage with inert gas as the JP-5 is consumed.

    The MV-22 is a fly-by-wire aircraft with triple redundant flight control systems. With the nacelles straight up in conversion mode (90 degrees), the flight computers command the aircraft to fly like a helicopter, with cyclic forces being applied to a conventional swashplate at the rotor hub. With the nacelles in airplane mode (0 degrees) the flaperons, rudder and elevator fly the aircraft like an airplane. This is a gradual transition which occurs over the entire 96 degree range of the nacelles. The lower the nacelles, the greater effect of the airplane-mode control surfaces.

    The Osprey was developed and is built jointly by Bell Helicopter Textron, who manufacture and integrate the wing, nacelles, rotors, drive system, tail surfaces, and aft ramp, as well as integrating the Rolls-Royce engines; and Boeing Helicopters, who manufacture and integrate the fuselage, cockpit, avionics, and flight controls. Portions are manufactured in Philadelphia, Pennsylvania, and Amarillo, Texas. Final assembly and delivery occurs in Amarillo. The joint development team is known as Bell-Boeing.

    v22.jpg
     

    Hashan dis

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    Su-37 Terminator, Sukhoi

    A derivative of the Su-27 'Flanker', the Su-37 is a super-maneuverable thrust vectoring fighter. Designed from an http://www.fighter-planes.com/info/su35.htm prototype, the Su-37 test aircraft (designated T10M-11) made its maiden flight in April 1996 from the Zhukovsky flight testing center near Moscow. The Su-37 powerplant features more standard thrust than all earlier 'Flanker' variants, including the Su-35. In addition, the hydraulically actuated nozzles of its Lyulka/Saturn AL-37FU (Forsazh Upravlaemoye meaning 'afterburning steerable') engines are steerable -15 to +15 degrees along the vertical plane. Thrust control is fully integrated into the flight control system, requiring no input from the pilot. An emergency system can automatically return the nozzles to level flight in the event of an onboard failure. The Su-37 has the newer, more powerful, NIIP NO-11M pulse-Doppler phased-array nose radar. A rearward-facing missile system and NIIP NO-12 rear-radar will give the pilot the ability to fire at enemy aircraft behind the Su-37, in addition to the front. While the Su-37 is the first Russian aircraft to feature thrust vector control comparable to that of the American F-22, it may not be the last. A new axisymmetrical (three-dimensional) nozzle is currently being developed by Lyulka for the future Sukhoi S-55 aircraft, a single-engined version of the Su-35. Nozzles are also being readied to make current Su-35s TVC capable.
    Prime contractor: Sukhoi Design Bureau
    Nation of origin: Russia
    Function: Multi-role fighter
    Crew: 1
    Year: 1996
    In-service year: ?
    Engine: Two Lyulka AL-37FU vectored-thrust afterburning turbofans, 30,855 lb thrust each
    Dimensions
    Wing span: 14.70 m
    Length: 22.10 m
    Height: 6.32 m
    Weight: 40,565 lb empty / 74,956 lb max. take off
    Ceiling: 59,055 ft
    Speed: 2,440 km/h
    Range: 3,500 km
    Armament: One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, ASMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points
    Multi-role combat version of the Su-27, developed from the Su-35. The Su-37 uses full digital FBW controls in combination with two- dimensional thrust vectoring nozzles. Like the Su-35, it has canards. The Su-37 is not yet in production.
    Type: Su-37
    Function: fighter
    Year: 1996
    Crew: 1
    Engines: 2 * 137kN Saturn AL-37FU
    Wing Span: 14.70 m
    Length: 22.10 m
    Height: 6.32 m
    Wing Area:
    Empty Weight: 18500 kg
    Max.Weight: 34000 kg
    Speed: 2400 km/h
    Ceiling: 17800 m
    Range:
    Armament: 1*g30mm 8000 kg







    su37.jpg


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