Showing posts with label Fighter Aircraft. Show all posts
Showing posts with label Fighter Aircraft. Show all posts

Wednesday, August 31, 2011

Mitsubishi ATD-X

Mitsubishi ATD-X
The Mitsubishi ATD-X Shinshin is a prototype fifth-generation jet fighter that uses advanced stealth technology. Being developed by the Japanese Ministry of Defense Technical Research and Development Institute (TRDI) for research purposes. The main contractor of the project is Mitsubishi Heavy Industries. Many consider this aircraft to be Japan's first domestically made stealth fighter. ATD-X is an acronym meaning "Advanced Technology Demonstrator – X". The aircraft's Japanese name is 心神 (shin-shin) which means one's mind. The aircraft's first flight is scheduled for 2014.

Mitsubishi ATD-X Development

At the beginning of the twenty-first century, Japan sought to replace its aging fleet of fighter aircraft, began making overtures to the United States on the topic of purchasing several Lockheed Martin F-22 Raptor fighters for their own forces. However the U.S. Congress had banned the exporting of the aircraft in order to safeguard secrets of the aircraft's technology such as its extensive use of stealth; this rejection necessitated Japan to develop its own modern fighter, to be equipped with stealth features and other advanced systems.

A mock-up of the ATD-X was constructed and used to study the radar cross section in France in 2005. A radio-controlled 1/5 scale model made its first flight in 2006 to gain data on performance at high angles of attack and to test new sensory equipment and self-repairing flight control systems.

Following these preliminary steps, the decision was taken in 2007 to push ahead with the multi billion-yen project. At the time of this decision, production was forecast to start roughly 10 years later, around 2017. As of 2007, the ATD-X is expected to conduct its maiden flight in 2014.

Mitsubishi ATD-X Design

The ATD-X will be used as a technology demonstrator and research prototype to determine whether domestic advanced technologies for a fifth generation fighter aircraft are viable, and is a 1/3 size model of a possible full-production aircraft. The aircraft also features 3D thrust vectoring capability. Thrust is controlled in the ATD-X by the use of 3 paddles on each engine nozzle similar to the system used on the Rockwell X-31, while an axis-symmetric thrust vectoring engine is also being developed for the full scale production model. The nozzles on the prototype appear to be uncovered and might have a slight adverse effect on the aircraft's stealth characteristics.

Among the features the ATD-X is to have is a fly-by-optics flight control system, which by substituting optical fibers for wires, allows data to be transferred faster and with immunity to electromagnetic disturbance.

Its radar will be an active electronically scanned array (AESA) radar called the 'Multifunction RF Sensor', which is intended to have broad spectrum agility, capabilities for electronic countermeasures (ECM), electronic support measures (ESM), communications functions, and possibly even microwave weapon functions.

A further feature will be a so-called 'Self Repairing Flight Control Capability', which will allow the aircraft to automatically detect failures or damage in its flight control surfaces, and using the remaining control surfaces, calibrate accordingly to retain controlled flight.

The JASDF is reported to have issued a request for information for engines in the 10 to 20 thousand pound thrust range to power the prototypes while Ishikawajima-Harima Heavy Industries is to provide the engines for the completed fighter.

Specifications (ATD-X)

General characteristics

  • Crew: 1
  • Length: 14.174 meters (46.50 feet)
  • Wingspan: 9.099 meters (29.85 feet)
  • Height: 4.514 meters (14.80 feet)
  • Max takeoff weight: 8 tonnes max takeoff weight alt = 17,636 pounds ()
  • Powerplant: 2 × IHI XF5-1.
    • Dry thrust: 10 tonnes (22,046 pounds) each
    • Thrust with afterburner: 15 tonnes (33,069 pounds) each


Sukhoi PAK FA

Sukhoi PAK FA

The Sukhoi PAK FA is a twin-engine jet fighter being developed by Sukhoi OKB for the Russian Air Force.

The current prototype is Sukhoi's T-50. The PAK FA, when fully developed, is intended to be the successor to the MiG-29 and Su-27 in the Russian inventory and serve as the basis of the Sukhoi/HAL FGFA being developed with India. A fifth generation jet fighter, the T-50 performed its first flight 29 January 2010. Its second flight was on 6 February and its third on 12 February 2010. As of 31 August 2010, it had made 17 flights and by mid-November, 40 in total. The second prototype was to start its flight test by the end of 2010, but this was delayed until March 2011.

Sukhoi director Mikhail Pogosyan has projected a market for 1,000 aircraft over the next four decades, which will be produced in a joint venture with India, 200 each for Russia and India and 600 for other countries. He has also said that the Indian contribution would be in the form of joint work under the current agreement rather than as a joint venture. The Indian Air Force will "acquire 50 single-seater fighters of the Russian version" before the two seat FGFA is developed. The Russian Defense Ministry will purchase the first 10 aircraft after 2012 and then 60 after 2016. The first batch of fighters will be delivered with current technology engines. Ruslan Pukhov, director of the Centre for Analysis of Strategies and Technologies, has projected that Vietnam will be the second export customer for the fighter. The PAK-FA is expected to have a service life of about 30–35 years.

Sukhoi PAK FA Development

In the late 1980s, the Soviet Union outlined a need for a next-generation aircraft to replace its MiG-29 and Su-27 in frontline service. Two projects were proposed to meet this need, the Sukhoi Su-47 and the Mikoyan Project 1.44. In 2002, Sukhoi was chosen to lead the design for the new combat aircraft.

The Tekhnokompleks Scientific and Production Center, Ramenskoye Instrument Building Design Bureau, the Tikhomirov Scientific Research Institute of Instrument Design, the Ural Optical and Mechanical Plant (Yekaterinburg), the Polet firm (Nizhniy Novgorod) and the Central Scientific Research Radio Engineering Institute (Moscow) were pronounced winners in the competition held in the beginning of 2003 for the development of the avionics suite for the fifth-generation airplane. NPO Saturn has been determined the lead executor for work on the engines for this airplane.

The Novosibirsk Chkalov Aviation Production Association (NAPO Chkalov) has begun construction of the fifth-generation multirole fighter. This work is being performed at Komsomol'sk-on-Amur together with Komsomolsk-on-Amur Aircraft Production Association; the enterprise's general director, Fedor Zhdanov reported during a visit to NAPO by Novosibirsk Oblast's governor Viktor Tolokonskiy on 6 March 2007. "Final assembly will take place at Komsomol'sk-on-Amur, and we will be carrying out assembly of the fore body of this airplane", Zhdanov specified.

On 8 August 2007, Russian Air Force Commander Alexander Zelin was quoted by Russian news agencies that the development stage of the PAK FA program is now complete and construction of the first aircraft for flight testing will now begin. Alexander Zelin also said that by 2009 there will be three fifth-generation aircraft ready. "All of them are currently undergoing tests and are more or less ready", he said. In the summer of 2009 the design was approved.

On 11 September 2010, it was reported that Indian and Russian negotiators had agreed on a preliminary design contract that would then be subject to Cabinet approval. The joint development deal would have each country invest $6 billion and take 8 to 10 years to develop the FGFA fighter. The agreement on the pre-design of the fighter was to be signed in December 2010. The preliminary design will cost $295 million and will be complete within 18 months.

On 17 August 2011, it was reported by Russian state-run media that the Sukhoi T-50 aircraft cost Russia and India $6 billion to develop, with India shouldering about 35% of the cost.

On 17 August 2011, Russian Air Force chief says the Sukhoi T-50 will enter service in 2014-2015. "We will receive a T-50 prototype in 2013," Russian Air Force commander-in-chief General Alexander Zelin told reporters. "Mass produced aircraft will not arrive until 2014-2015."

Flight testing

On 28 February 2009, Mikhail Pogosyan announced that the airframe for the aircraft was almost finished and that the first prototype should be ready by August 2009. On 20 August 2009, Sukhoi General Director Mikhail Pogosyan said that the first flight would be by year end. Konstantin Makiyenko, deputy head of the Moscow-based Centre for Analysis of Strategies and Technologies said that "even with delays", the aircraft would likely make its first flight by January or February, adding that it would take 5 to 10 years for commercial production.

The maiden flight had been repeatedly postponed since early 2007 as the T-50 encountered unspecified technical problems. Air Force chief Alexander Zelin admitted as recently as August 2009 that problems with the engine and in technical research remained unsolved.

On 8 December 2009, Deputy Prime Minister Sergei Ivanov announced that the first trials with the fifth-generation aircraft would begin in 2010. The testing, however, has commenced earlier than stated, with the first successful taxiing test taking place on 24 December 2009.

The aircraft's maiden flight took place on 29 January 2010 at KnAAPO's Komsomolsk-on-Amur Dzemgi Airport; the aircraft was piloted by Sergey Bogdan (Сергей Богдан) and the flight lasted for 47 minutes.

A second airframe was first planned to join the flight testing in the fourth quarter of 2010 but was postponed. On 3 March 2011 a second prototype was reported to have made a successful 44 minute test flight. These first two aircraft will lack radar and weapon control systems, while the third and fourth aircraft, to be added in 2011, will be fully functional test aircraft.

On 14 March 2011, the aircraft achieved supersonic flight at a test range near Komsomolsk-on-Amur in Siberia.

The T-50 was displayed publicly for the first time at the 2011 MAKS Airshow. Russian Prime Minister Vladimir Putin was in attendance.

In June 2011, an unauthorized video was made of the Sukhoi PAK FA in flight displaying a variety of acrobatic moves.

On August 21, 2011 during a take-off run at the MAKS Airshow, a brief flame appeared out of the right-hand engine before liftoff. The takeoff was aborted, braking parachutes were deployed and the aircraft returned to its park position under its own power.

Naval version

Navalized Sukhoi T-50 PAK FAs will be deployed on the Russian aircraft carrier Admiral Kuznetsov and future Russian aircraft carriers. There will be a competition between the Sukhoi, Mikoyan and Yakovlev design bureaus to choose the new naval aircraft.

Light fighter

Alexei Fedorov has said that any decision on applying fifth generation technologies to produce a smaller fighter (in the F-35 range) must wait until after the heavy fighter, based on the T-50, is completed.

Sukhoi PAK FA Design

Although most of information about the PAK FA is classified, it is believed from interviews with people in the Russian Air Force and Defense Ministry that it will be stealthy, have the ability to supercruise, be outfitted with the next generation of air-to-air, air-to-surface, and air-to-ship missiles, incorporate a fix-mounted AESA radar with a 1,500-element array and have an "artificial intellect".

According to Sukhoi, the new radar will reduce pilot load and the aircraft will have a new data link to share information between aircraft.

Composites are used extensively on the T-50 and comprise 25% of its weight and almost 70% of the outer surface. It is estimated that titanium alloy content of the fuselage is 75%. Sukhoi's concern for minimizing radar cross-section (RCS) and drag is also shown by the provision of two tandem main weapons bays in the centre fuselage, between the engine nacelles. Each is estimated to be between 4.9-5.1 m long. The main bays are augmented by bulged, triangular-section bays at the wing root.

The Moskovsky Komsomolets reported that the T-50 has been designed to be more maneuverable than the F-22 Raptor at the cost of making it less stealthy than the F-22. One of the design elements that have such an effect is the Leading Edge Vortex Controller (LEVCON).

Avionics

The PAK FA SH121 radar complex includes three X-Band AESA radars located on the front and sides of the aircraft. These will be accompanied by L-Band radars on the wing leading edges. L-Band radars are proven to have increased effectiveness against very low observable (VLO) targets which are optimized only against X-Band frequencies, but their longer wavelengths reduce their resolution. However the initial prototypes will use legacy passive electronically scanned array radar.

The PAK FA will feature an IRST optical/IR search and tracking system, based on the OLS-35M which is currently in service with the Su-35S.

Hindustan Aeronautics Limited will reportedly provide the navigation system and the mission computer.

Engines

PAK FA was expected to use a pair of Saturn 117S engines on its first flights. The 117S (AL-41F1A) is a major upgrade of the AL-31F based on the AL-41F intended to power the Su-35BM, producing 142 kN (32,000 lb) of thrust in afterburner and 86.3 kN (19,400 lb) dry. In fact, PAK FA already used a completely new engine 117 (AL-41F1) in its first flight, as stated by NPO Saturn. The engine is not based on the Saturn 117S

The 117 (AL-41F1) is a new 5th generation engine custom built for Russia’s fifth-generation stealth fighter jet PAK-FA according to Sukhoi General Director Mikhail Pogosyan.Mikhail Pogosyan has clarified that claims that fifth-generation fighter allegedly has an old engine are wrong. Such claims are made by people with limited knowledge,he said.Though most parameters of the new 5th Gen Engine remains classified General Director Mikhail Pogosyan provided some information on the new engine, The engine thrust was enlarged by 2.5 tonnes when compared with the AL-31 engine, while the engine weight was cut by 150 kilograms. That allowed the new jet to supercruise i.e. move at a supersonic cruise speed without the use of after burner.

The Saturn Research and Production center made digitally-controlled system (FADEC) of Project 117 Engine.The new engine produces 33,000 lbs (147 kN) of thrust in afterburner has a Dry weight of 1420 kilogram and T:W ratio of 10.5:1

Mikhail Pogosyan further mentioned that this engine (117) meets the client’s (Russian AirForce) requirements. This is not an intermediate product made particularly for test flights. The engine will be installed in production PAK-FA fighter which will be supplied to the Russian Air Force and prospective foreign clients he said. The engine generates a larger thrust and has a complex automation system, to facilitate flight modes such as maneuverability. It is expected that each engine will be able to independently vector its thrust upwards, downward or side to side. Vectoring one engine up with the other one down can produce a twisting force. Therefore the PAK FA would be the first fifth generation fighter with full 3-D thrust vectoring along all three aircraft axes: pitch, yaw and roll. These engines will incorporate infrared and RCS reduction measures.

Armament

The PAK FA has a reported maximum weapons load of 7,500 kg. It has an apparent provision for a cannon (most likely GSh-301). It could possibly carry as many as two 30 mm cannons. It has two internal bays estimated at 4.6-4.7 metres by 1-1.1 metres. Some sources suggest two auxiliary internal bays for short range AAMS and six external hardpoints.

Two Izdeliye 810 Extended beyond visual range missiles per weapons bay. Multiple Izdeliye 180 / K77M beyond visual range missiles. K74 and K30 within visual range missiles can also be carried. Two KH38M or KH58 USHK air-to-ground missiles per weapons bay. Multiple 250–500 kg precision guided bombs per weapons bay, with a maximum of 10 bombs in internal bays. Other possible loads include one 1,500 kg bomb per weapons bay or two 400 km+ range anti-AWACS weapons on external hardpoints.

Operational history

Testing

The first flight video shows that PAK FA has no conventional rudders, its vertical tails are fully movable. This special tail fin design is mechanically similar to V-tails used by the Northrop YF-23 in 1990s, but is supplemented by dedicated horizontal stabilators (as on the F-22). The T-50 has wing leading-edge devices above the jet engine intakes that have been called a challenge for signature control.

Exports

Russia has offered the PAK-FA for South Korea's next generation jet fighter. South Korea's defence procurement agency has confirmed that the Sukhoi PAK-FA is a candidate for the Republic of Korea Air Force's next-generation fighter (F-X Phase 3) aircraft.

Sukhoi PAK FA Specifications

Because the aircraft is in development, these specifications are preliminary and are taken as estimates from the available images.

General characteristics

  • Crew: 1
  • Length: 19.8 m (65.9 ft)
  • Wingspan: 14 m (46.6 ft)
  • Height: 6.05 m (19.8 ft)
  • Wing area: 78.8 m2 (848.1 ft2)
  • Empty weight: 18,500 kg (40,785 lb)
  • Loaded weight: 26,000 kg (57,320 lb)
  • Useful load: 7,500 kg (combat load) (16,534 lb)
  • Max takeoff weight: 37,000 kg (81,570 lb)
  • Powerplant: 2 × New unnamed engine by NPO Saturn and FNPTS MMPP Salyut of 175 kN each. Prototype with AL-41F1 of 147 kN each, definitive version with new engine >157 kN
  • Fuel capability: 10,300 kg (22,711 lb)

Performance

  • Maximum speed: 2,100 - 2,500 km/h (Mach 2+) (1,300 - 1,560 mph) ; at 17,000 m (45,000 ft) altitude
  • Cruise speed: 1,850 - 2,100 km/h (1,150 - 1,300 mph)
  • Ferry range: 5,500 km (3417 miles)
  • Service ceiling: 20,000 m (65,616 ft)
  • Rate of climb: 350 m/s (68,900 ft/min)
  • Wing loading: 330(normal) - 470(maximum) kg/m2 (67(normal) - 96(maximum) lb/ft2)
  • Thrust/weight: 1.19
  • Maximum g-load: 9+ g

Armament

  • Guns: None on prototype. Apparent provision for a cannon (most likely GSh-301). Possible two 30 mm cannons.
  • Hardpoints: Two internal bays Other sources suggest two auxiliary internal bays for short range AAMS and six external hardpoints

Avionics

N050 BRLS AFAR/AESA built by Tikhomirov NIIP and based on Tikhomirov NIIP N035 Irbis-E. It will be the second aircraft based AESA Radar to be built by Russia, the first being the Phazotron NIIR ZHUK-A Radar in the MiG-35.

Sukhoi/HAL FGFA - Fifth Generation Fighter Aircraft

Sukhoi/HAL FGFA  - Fifth Generation Fighter Aircraft

The Sukhoi/HAL Fifth Generation Fighter Aircraft (FGFA) is a fifth-generation fighter being developed by Russia and India. It is a derivative project from the PAK FA (T-50 is the prototype) being developed for the Indian Air Force (FGFA is the official designation for the Indian version).

Two separate prototypes will be developed, one by Russia and a separate one by India. According to HAL chairman A.K. Baweja shortly after the India-Russia Inter-Governmental Committee meeting on 18 September 2008, the Russian version of the aircraft will be a single-seater, the Indian version will be a twin seater, analogous to the Su-30MKI which is a twin seat variant of the baseline Su-27.

A contract between Bangalore-based Hindustan Aeronautics Ltd (HAL) and Russia’s United Aircraft Corporation (UAC), will commit to building 250 fighters for the IAF and an equal number for Russia. The option for further orders will be kept open. HAL and UAC will be equal partners in a joint venture company, much like the Brahmos JV, that will develop and manufacture the FGFA. Further it was reported that the Bangalore-based HAL has negotiated firmly to get a 25 per cent share of design and development work in the FGFA programme. HAL’s work share will include critical software, including the mission computer; navigation systems; most of the cockpit displays; the counter measure dispensing (CMD) systems; and modifying Sukhoi’s single-seat prototype into the twin-seat fighter that the Indian Air Force (IAF) wants. Further Russia’s expertise in titanium structures will be complemented by India’s experience in composites like in the fuselage. A total of 500 aircraft are planned with option for further aircraft. Russian Air Force will have 200 single seated and 50 twin-seated PAK FAs while Indian Air Force will get 200 twin-seated and 50 single seated FGFAs.

Sukhoi director Mikhail Pogosyan has projected a market for 1000 aircraft over the next four decades, two hundred each for Russia and India and six hundred for other countries. Russian Trade Minister Viktor Khristenko said that the aircraft are to be jointly developed and produced with India and both countries will "share benefits from selling the plane not only on their domestic markets, but also on the markets of third countries."

The Indian media also use the term FGFA generically to refer to any fifth generation fighter aircraft.

Sukhoi/HAL FGFA Development

India will eventually spend over $25 billion to induct 200 FGFA and 50 PAK FA advanced stealth fighter aircraft. This will be in addition to the huge investments to be made in co-developing FGFA, as with the infrastructure required to base, operate and maintain such jets in India. Air Chief Marshal Naik said the 30-tonne FGFA will be a "swing-role fighter, with advanced avionics, super cruise, stealth (Very Low RCS) to increase survivability, enhanced lethality, 360 degree situational awareness, smart weapons, data-links, high-end mission computers and the like. Along with 126 medium multi-role combat aircraft, which India plans to acquire, 270 Sukhoi-30MKIs contracted from Russia, and 220 indigenous Tejas Light Combat Aircraft, the FGFA will be the mainstay of India's air combat fleet for the foreseeable future. This, in addition to the remaining 50 odd Mirage 2000 fighters, 61 MIG-29 SMT, and the 125 MIG-21 Bison operational till 2017.This will help IAF to reach the sanctioned healthy strength of 44 squadrons with more than 792 aircraft.

The joint-venture borrows heavily from the success of the Brahmos project. Russia and India had agreed in early 2007 to jointly study and develop a Fifth Generation Fighter Aircraft Programme (FGFA). On October 27, 2007, Asia Times quoted Sukhoi's director, Mikhail Pogosyan, "We will share the funding, engineering and intellectual property in a 50-50 proportion." The Indian version, according to the deal, will be different from the Russian version and specific to Indian requirements. While the Russian version will be a single-pilot fighter, the Indian variant will have a twin-seat configuration based on its operational doctrine which calls for greater radius of combat operations. The wings and control surfaces need to be reworked for the FGFA. Although, development work has yet to begin, the Russian side has expressed optimism that a test article will be ready for its maiden flight by 2009, one year after PAK FA scheduled maiden flight and induction into service by 2015.

According to HAL chairman A.K. Baweja on 16 September 2008, HAL will be contributing largely to composites, cockpits and avionics. HAL is working to enter into a joint development mechanism with Russia for the evolution of the FGFA engine as an upward derivative of the AL-37. By February 2009 as per Sukhoi general director Mikhail Pogosyan India will initially get the same PAK FA fighter of Russia and the only difference will be the software.

Difference between PAK FA and FGFA

The difference between PAK FA and the FGFA will be similar to that between Su-30M and Su-30MKI. Su-30M is a standard Russian version of a plane, whereas the Su-30MKI (MKI stands for "Modernizirovannyi Kommercheskiy Indiski" meaning "Modernized Commercial India") was jointly-developed with India's Hindustan Aeronautics Limited for the Indian Air Force. The Su-30MKI includes 2.5D Thrust Vectoring Control (TVC) and canards. It is equipped with a multi-national avionics complex sourced from India, Israel, Russia and France. Further the FGFA will be predominantly using weapons of Indian origin such as Astra, a BVR Beyond Visual Range missile being developed by India, although in keeping with the Russian BVR doctrine of using a vast variety of different missiles for versatility and unpredictability to countermeasures, it can be expected to have compatibility with many different missile types. Ashok Baweja stated that "The Indian FGFA is significantly different from the Russian PAK FA because a second pilot means the addition of another dimension, development of wings and control surfaces."

The FGFA may also include systems developed by third parties.

Sukhoi/HAL FGFA Design

Although there is no reliable information about the PAK FA and FGFA specifications yet, it is known from interviews with people in the Russian Air Force that it will be stealthy, have the ability to supercruise, be outfitted with the next generation of air-to-air, air-to-surface, and air-to-ship missiles, and incorporate an AESA radar. The FGFA will use on its first flights 2 Saturn 117S engines (about 14.5 ton thrust each). The 117S is an advanced version of the AL-31F, but built with the experience gained in the AL-41F program. The AL-41F powered the Mikoyan MFI fighter (Mikoyan Project 1.44). Later versions of the PAK FA will use a completely new engine (17.5 ton thrust each), developed by NPO Saturn or FGUP MMPP Salyut.

Three Russian companies will compete to provide the engines with the final version to be delivered in 2015-2016.

Speaking to Flight magazine, United Aircraft chief Mikhail Pogosyan denied India is simply providing funding for Russian designers to produce a modified aircraft for the Indian air force's requirements. He said India is giving engineering inputs covering latest airframe design, Hi-Tech software development and other systems.

Specifications (PAK FA and FGFA - projected)

Most of these figures are for the single seat Sukhoi T-50 and not the finished PAK FA or two seat HAL FGFA.

General characteristics

  • Crew: 2 (pilot)
  • Length: 22.0 m (72 ft 2 in)
  • Wingspan: 14.2 m (46 ft 7 in)
  • Height: 6.05 m (19 ft 10 in)
  • Wing area: 78.8 m² (848 ft²)
  • Empty weight: 18,500 kg (40,786 lb)
  • Loaded weight: 26,000 kg (57,320 lb)
  • Useful load: 7,500 kg (16,535 lb)
  • Max takeoff weight: 37,000 kg (81,571 lb)
  • Powerplant: 2 × Saturn-Lyulka AL-41F turbofan
    • Dry thrust: 96.1 kN (9,800 kgf, 21,605 lbf) each
    • Thrust with afterburner: 152 kN (15,500 kgf, 34,172 lbf) each

Performance

  • Maximum speed: 2,100 km/h (Mach 2) (1,305 mph)
  • g-limits: (10-11 g)
  • Cruise speed: 1,300 km/h (800 mph)
  • Combat radius: 1,500 km

  • Ferry range: 5,500 km (3,400 mi)
  • Service ceiling: 20,000 m (65,617 ft)
  • Rate of climb: 350 m/s (68,898 ft/min)
  • Wing loading: 330(normal) - 470(maximum) kg/m2 (67(normal) - 96(maximum) lb/ft2)
  • Thrust/weight: 1.19
  • Runway: 350 m (1,148 ft)
  • Endurance: 3.3 hrs (198 mins)

Armament

  • Guns: 2× 30 mm internal cannon
  • Hardpoints: 16 total, 8 internal, 8 on wings.

Avionics

  • Radar: N050(?)BRLS AESA/PESA Radar (Enhancement of IRBIS-E) on SU-35
    • Frequency: X (8 - 12 GHz)
    • Diameter: 0.7 m (2 ft 4 in)
    • Targets: 32 tracked, 8 engaged
    • Range: > 400 km (248 mi)
      • EPR: 3 m² (32.3 ft²) at 400 km (248 mi)
      • RCS: 3 m ² to 400 km, 1 m ² to 300 km, 0.5 m ² to 240 km, 0.1m ² to 165 km, 0.01M ² to 90 km.
      • Azimuth: 240 ° (± 120 °)
    • Power: 5,000 W
    • Weight: 65 to 80 kg (143 to 176 lb)


Chengdu J-20 Stealth Air Superiority Fighter

Chengdu J-20
The Chengdu J-20 is a purported fifth generation, stealth, twin-engine fighter aircraft prototype developed by Chengdu Aircraft Industry Group for the Chinese People's Liberation Army Air Force (PLAAF). In late 2010, the J-20 underwent high speed taxiing tests. The J-20 made its first flight on 11 January 2011. General He Weirong, Deputy Commander of the People's Liberation Army Air Force said in November 2009 that he expected the J-20 to be operational in 2017–2019.

Chengdu J-20 Development

The J-20 was one of the stealth fighter programs under the codename J-XX that was launched in the late 1990s. It was designated “Project 718”, and won the PLAAF endorsement in a 2008 competition against a Shenyang proposal that was reportedly even larger than J-20. Two prototypes (#2001-01 & #2001–02) have been built as of the end of 2010.

On 22 December 2010, the J-20 was under-going high speed taxiing tests outside the Chengdu Aircraft Design Institute with no confirmed flight tests. The J-20 made its first flight, which lasted about 20 minutes, on 11 January 2011.

Director of National Intelligence James R. Clapper has testified that the United States has known about the program for a "long time" and that the test flight was not a surprise.

Flight testing

The J-20 made its first flight, lasting about 15 minutes, on 11 January 2011. A Chengdu J-10S served as the chase aircraft. After the successful first flight, a ceremony was held. The test pilot of the J-20, Li Gang, Chief designer Yang Wei and General Li Andong (Deputy-Director of General Armaments Department, and Director of Science and Technology Commission of General Armaments Department of the PLA since 2000) attended the ceremony.

China thus became the third nation in the world to "develop and test-fly a full-size stealth combat aircraft demonstrator", after the United States and Russia. The Guardian reported that experts, on the one hand, expressed "surprise" at the speed with which the aircraft was developed, but on the other hand "said the country's military prowess was still relatively backward and way behind that of the US" and that its military interests were limited to its region.

The first test flight coincided with a visit of United States Secretary of Defense Robert Gates to China, and was initially interpreted by Pentagon officials and media pundits as a possible signal to the visiting delegation from the U.S. However, after meeting with senior Chinese officials including Chinese President Hu Jintao, Secretary Gates remarked, "The civilian leadership seemed surprised by the test and assured me it had nothing to do with my visit." Jin Canrong, a professor at Renmin University in Beijing who specializes in China-U.S. relations, suggested that President Hu's ignorance of the test raises questions about the nature of civilian control of the Chinese military.] However, as Michael Swaine, an expert on the PLA and United States – China military relations, explained, although it's possible and even likely that "senior officials in the Chinese leadership did not know that this flight test would occur on this precise day," this is not necessarily evidence of a military-backed effort to insult Secretary Gates' delegation or embarrass President Hu. Rather, decisions regarding the production, development and testing of such military aircraft are routinely managed by engineers and low-level officials more than by senior civilian or military leadership. Coupled with the fact that there was relatively limited coverage of the event in Chinese media initially, it is likely that the test may not have been considered a significant enough event to warrant notification to President Hu.

A second test flight of an hour and twenty minutes took place on 17 April 2011. On 5 May 2011, a 55 minute test flight included retraction of the landing gear.

The full initial test program of 10 to 20 test flights is expected to take years to complete.

Technology transfer

China probably declined to participate in joint development and production of new fifth generation fighter with Russia given the belief that Russia stood to gain more from Chinese participation. Chinese leaders may have determined that their design was superior to the Russian PAK FA. United States House Committee on Armed Services chairman Howard McKeon said on the J-20 "my understanding is that they built it on information that they received from Russia, from a Russian plane, that they were able to copy". MiG spokeswoman Yelena Fyodorova has denied that any of the project 1.44 materials had been provided to China.

Balkan military officials told the Associated Press that China and Russia may have adopted some stealth technology from a Lockheed F-117 Nighthawk, which was shot down by the Serbian military in 1999 during the Kosovo war. If Chinese experts used the F-117 stealth coatings, the result would be decades behind current American state-of-the-art. However, Chinese test pilot Xu Yongling said that the J-20 was a "masterpiece" of home-grown innovation, he also said the F-117 technology was already "outdated" even at the time it was shot down, and could not be applied to a next-generation stealth jet. Janes editor James Hardy agrees that it was unlikely China would have learned much from the wreckage.

Retired USAF General Thomas G. McInerney has suggested that the J-20 design may have been based on cyber-espionage of the Lockheed Martin FB-22 project.

A federal prosecutor has suggested that China may have used technology from the Northrop Grumman B-2 Spirit for their stealth aircraft which was supplied by Noshir Gowadia.

Chief of the Air Staff of the Indian Air Force Pradeep Vasant Naik has suggested that the J-20 is entirely reverse engineered with no Chinese R&D involved, and questioned if the practice was ethical. The Deccan Chronicle has called Naik's comment an "unusual outburst of helplessness" as China surpasses Indian airpower.

Russian military commentator Ilya Kramnik conjectures that China is still 10 to 15 years behind the United States and Russia in fighter technology and may not be able to manufacture all the advanced composite materials, avionics and sensor packages needed for such aircraft, and could instead turn to foreign suppliers. However, he speculates that China may be able to produce the J-20 at a cost 50% to 80% lower than US and Russian fifth-generation jet fighters, and that potential customers may include Pakistan, the Middle East, Latin America, Southeast Asia and the richest countries in Africa. Konstantin Sivkov of the Academy for Geopolitical Issues argued that the US is correct to be alarmed at the progress of Chinese military technology. Mikhail Pogosyan, head of the United Aircraft Corporation, has claimed that the Chinese program is more a demonstration and that they lack the scale and experience to complete the project.

Bill Sweetman speculates that China will have problems meeting its production requirements, as it has several other jet fighter projects in production. Aviation Week raised the question of whether the aircraft is a prototype, like the Sukhoi T-50, or a technology demonstrator similar to the Lockheed YF-22.

Chengdu J-20 Design

Characteristics

The J-20 is a single-seat, twin-engine aircraft which appears to be somewhat larger and heavier than the comparable Sukhoi T-50 and Lockheed Martin F-22 Raptor. Bill Sweetman estimates that it is approximately 75 feet (23 m) in length, has a wingspan of 45 feet (14 m) or more, and is expected to have a takeoff weight of 75,000 to 80,000 pounds (34,000 to 36,000 kg) with internal stores only. The prototype could be powered by twin 32,000 pounds (15,000 kg) thrust Saturn 117S engines provided by Russia, a sign of problems in the development of the aircraft, according to Pentagon spokesman Col. David Lapan. Chinese sources have claimed that production aircraft will be powered by two 13,200 kilograms (29,000 lb)/WS-10 class high thrust turbofan engines fitted with Thrust Vector Controlled (TVC) nozzles, both made in China. However Richard Aboulafia has said that the WS-10 engine has suffered catastrophic failures in flight. The best estimates are that China will take five to ten years to perfect the fifth generation jet engines needed for the J-20.

The J-20 may have lower supercruise speed (yet greater range) and less agility than a Lockheed Martin F-22 Raptor or PAK FA, but might also have larger weapons bays and carry more fuel. The J-20 has a long and wide fuselage and low jet engine intakes with a forward chine, a main delta wing, forward canards, a bubble canopy, conventional round engine exhausts and canted all-moving fins. The front section of the J-20 is similarly chiseled as the F-22 Raptor and the body and tail resemble those of the Sukhoi T-50 prototype. As early photographs of the prototype surfaced, Bill Sweetman commented that the design may suggest a large, long range ground attack aircraft, not unlike a "stealth version" of the General Dynamics F-111 Aardvark. Douglas Barrie has noted that the canard-delta configuration with canted vertical fins appears to resemble the MiG 1.42. Yet, Barrie notes that key differences include greater forward fuselage shaping as the basis for low observable characteristics, along with the different engine intake configuration. It is suspected that cyberespionage may have assisted the development of the J-20, with information used by subcontractors of Lockheed Martin for the F-35 project in particular having been significantly compromised during development of the J-20.

The J-20 has a pair of all-moving tailfins that are swept back in the F-35 style instead of being trapezoid like the F-22 and PAK-FA tails and ventral stabilizing fins. It also has an F-22 style nose section, but with F-35 style dropped nose, forward swept intake cowls with diverterless supersonic inlet (DSI) bumps and a one-piece canopy. It was reported in November 2006 that a T/W=10 17,000 kilograms (37,000 lb) class turbofan (WS-15/"large thrust") was being developed for the J-20. One (#2001-01) prototype is fitted with AL-31F, the other (#2001–02) is fitted with the improved WS-10G with a new "stealth" nozzle possibly to reduce RCS and IR emission.

The J-20 may become the first operational combat aircraft that carries sufficient fuel to supercruise throughout its missions, doubling its sortie rate.

Pentagon spokesman Geoff Morrell has said that it was premature to call the J-20 a stealth fighter or to judge if it had any other fifth generation characteristics.

Avionics

The production J-20 may incorporate an advanced fly-by-wire (FBW) system fully integrated with the fire-control and the engine systems. Its fire-control radar is expected to be Active Electronically Scanned Array (AESA) (Type 1475/KLJ5).

According to recent pictures from the internet, two small dark diamond shaped windows can be seen on both sides of the nose, which could house certain EO sensors, such as MAWS and/or IRST. Two additional windows are seen underneath the rear fuselage, plus two more on top of the forward fuselage above the canard wings, suggesting a distributed situational awareness system similar to the EODAS onboard American F-35 was installed providing a full 360° coverage.

Cockpit

The aircraft features a "pure" glass cockpit (two large color liquid crystal display (LCD) and several smaller ones and a wide-angle holographic head-up display (HUD)). Many of these subsystems have been tested onboard J-10Bs to speed up the development.

Armament

The J-20 has a large belly weapon bay for short/long-range air-to-air missiles (AAM) (PL-10, PL-12C/D & PL-21) and two smaller lateral weapon bays behind the air inlets for short-range AAMs (PL-10).

One photo depicts the same air to air loadout as the F-22, that is six medium range and two short range air to air missiles.

Stealth

Carlo Kopp has suggested that the J-20's overall stealth shaping is "without doubt considerably better" than the F-35 and PAK FA, but he agrees with others, such as Shih Hiao-wei of Defense International monthly and Bill Sweetman of Aviation Week, that some parts on the J-20 will challenge its ability to remain stealthy from all directions: "The aft fuselage, tailbooms, fins/strakes and axi-symmetric nozzles are not compatible with high stealth performance, but may only be stop-gap measures to expedite flight testing of a prototype." As of January 2011 the engine nozzles were clearly non-stealthy; this may be due to the fact that the final "fifth generation" engines had not been completed yet. However, one of the prototypes uses WS-10G engines with stealthy jagged-edge nozzles and tiles.

Robert Gates has also questioned how stealthy the J-20 might be although he did say the development of the J-20 had the potential to "put some of our capabilities at risk, and we have to pay attention to them, we have to respond appropriately with our own programs.” Kopp and Goon have further speculated that the J-20 is designed to operate as a heavy interceptor, destroying opposing AWACS and tanker aircraft. If true, this would make it more similar to a MiG-25 with stealth capability. Sweetman agrees that this is the most likely role for such a large aircraft with low thrust to weight ratio and limited agility that is optimized for range and speed. Lewis Page has said that it is unlikely that the Chinese will soon have an American style Low Probability of Intercept Radar and so the J-20 would be limited to attacking ground targets like previous generations of American stealth aircraft such as the Lockheed F-117 Nighthawk. In that case the J-20 would carry a radar, but using it would instantly give away its location. However, the J-20 is expected to use a AESA radar, which should have Low Probability of Intercept modes. Given that the F-35 can already track and jam even the F-22's radar, this might not be sufficient.

Loren B. Thompson has said that this combination of forward sector only stealth and long range will allow the J-20 to make attacks on surface targets while the United States lacks sufficient bases for F-22s in the area to counter these attacks and American allies have no comparable aircraft. Thompson has also said that a long-range maritime strike aircraft may cause the United States more trouble than a shorter range air-superiority fighter like the F-22. The Pentagon's 2011 report on the Chinese military agrees that the J-20 is "a platform capable of long range, penetrating strikes into complex air defense environments."

A canard delta offers greater efficiency in both subsonic and supersonic flight (which may help supercruise range), but it is unknown if the Chinese have the same software used on the Eurofighter Typhoon to control the otherwise non-stealthy canards. Teal Group analyst Richard Aboulafia has also raised doubts about the use of canards on a design that is intended to be low-observable: “There’s no better way of guaranteeing a radar reflection and compromise of stealth”. Aboulafia has also called the J-20 a kludge made of mismatched parts and questioned if the Chinese have the skills or technology to produce a true fifth generation fighter. Nevertheless, canards greatly boost the aircraft's maneuverability over that of a pure delta wing without canards. Sweetman notes that the canard delta works with the Whitcomb area rule for a large-volume mid-body section supersonic aircraft. Also, while the DSI intakes are easier to maintain than more complex stealth-compatible intakes, such as on the F-22, their fixed form limits the aircraft to around Mach 2.0. J.D. McFarlan of Lockheed Martin has said that the J-20 DSI inlets resemble those of the F-35, but it is unclear if the Chinese have perfected their own design.

Kanwa Andrew Chan, editor-in-chief of Hong Kong Military News Agency, questioned the J-20's stealth among other parameters saying that it cannot yet match its competitors—the Russian T-50 and U.S. F-22—due to lack of engine power, the inability to fly at supersonic speeds, and shortcomings in its radar system and stealth, calling it a 4+ generation fighter in its current state.

Chengdu J-20 Specifications

Because the aircraft is in development, these specifications are preliminary and are taken as estimates from the available images.

General characteristics

  • Crew: 1
  • Length: 70 ft (21.26 m)
  • Wingspan: 42 ft (12.88 m)
  • Height: 4.45m (14.6 ft)
  • Wing area: 630 ft^2 ()
  • Max takeoff weight: 66,000–80,000 lb (34,000 - 37,000 kg)
  • Powerplant: 2 × 117S and WS-10G turbofans (prototypes); WS-15 (production) turbofans
    • Dry thrust: Unknown () each
    • Thrust with afterburner: 31,900 lb (117S); 32,845 (WS-10G); 40,500 (WS-15) (142 kN for 117S; 155 kN for WS-10G; 180 kN for WS-15) each

Performance

Armament

  • Guns: None on prototype.

    Expected to have internal and external hardpoints for missiles, bombs and fuel tanks.


KAI KF-X Multirole Fighter Aircraft

KAI KF-X Multirole Fighter Aircraft

The Korea Aerospace Industries KF-X is a South Korean program to develop an advanced multirole fighter for the Republic of Korea Air Force (ROKAF) and Indonesian Air Force (TNI-AU), spearheaded by South Korea with Indonesia as the primary partner. It is South Korea's second fighter development program following the FA-50.

The project was first announced by South Korean President Kim Dae-Jung at the graduation ceremony of the Air Force Academy in March 2001. South Korea and Indonesia had agreed to cooperate in the production of KF-X warplanes in Seoul on July 15, 2010. The initial operational requirements for the KF-X program as stated by the ADD (Agency for Defence Development) were to develop a single-seat, twin-engine jet with stealth capabilities beyond either the Dassault Rafale or Eurofighter Typhoon, but still less than the Lockheed Martin F-35 Lightning II. The overall focus of the program is producing a fighter with higher capabilities than a KF-16 class fighter by 2020.

KAI KF-X Design and development

KAI KF-X DesignAccording to the Weapon Systems Concept Development and Application Research Center of Konkuk University, the KF-X is intended to be a superior than KF-16 which would replace South Korea's aging F-4D/E Phantom II and F-5E/F Tiger II aircraft, with production numbers estimated to be over 250 aircraft. Compared to KF-16, the KF-X will have a 50% greater combat radius, 34% longer airframe lifespan, better avionics including a domestically produced AESA radar, and better electronic warfare, IRST, and datalink capabilities. Operational requirements also specify approx 50,000 pounds of thrust provided by one or preferably two engines, high-speed interception and supercruise capabilities, basic stealth technology, and multirole capabilities. There are currently two competing designs for the KFX, the KFX-201 which has a tri-plane layout with canards and a more conventional, Single Engine F-35 style KFX-101 design.

South Korea will fund 60% of the aircraft's development, and expects foreign partners to provide the remaining 40% of the development funding. South Korea possesses 63% of the necessary technology to produce the KF-X, and is therefore seeking cooperation from Indonesian Aerospace, Turkish Aerospace Industries, Saab, Boeing, and Lockheed Martin to develop the KF-X. About 120 KF-Xs would be built initially and more than 130 aircraft would be produced additionally after the first-phase models reach operational capability. The cost of each KF-X aircraft is estimated to be roughly $50 million +.

In October 2009 a retired general in the South Korean Air Force was arrested for leaking classified documents to Swedish aviation and defence corporation Saab. The general was to have been given a bribe of several hundred thousand dollars for copies of a number of secret documents that he had photographed in the South Korean Defence University. Saab officials denied any involvement.

On 15 July 2010, the Indonesia government agreed to fund 20% of KF-X project cost in return of around 50 planes built for Indonesian Air Force after project completion. In September 2010, Indonesia sent a team of legal and aviation experts to South Korea to discuss copyright issues of the aircraft.

On 7 September 2010, Maj. Gen. Choi Cha-kyu, director general of the aircraft program bureau at the Korean Defense Acquisition Program Administration (DAPA) said that Turkey was interested in joining the program.

On 15 December 2010, a senior Turkish procurement official said that "What we need is a true and equal partnership for the development of a fighter. The problem is that South Korea is not likely to agree to an equal partnership".

In December 2010 the program shifted from a F-16 class fighter to a stealth aircraft in order to respond to North Korean pressure.

On 2 August 2011, a joint research center was opened in Daejeon.

Advanced Medium Combat Aircraft

Advanced Medium Combat Aircraft
The Advanced Medium Combat Aircraft (AMCA), formerly known as the Medium Combat Aircraft (MCA), is a single-seat, twin-engine fifth-generation stealth multirole fighter being developed by India. It will complement the HAL Tejas, the Sukhoi/HAL FGFA, the Sukhoi Su-30MKI and the as yet undecided MRCA in the Indian Air Force. The main purpose of this aircraft is to replace the aging SEPECAT Jaguar and MiG-27. Unofficial design work on the MCA has been started. A naval version is confirmed as Indian Navy also contributed to the funding.

AMCA Development

In August 2006, India's then defence minister Mr. Pranab Mukherjee announced in Parliament that the government is evaluating experiences gained from the Tejas programme for the MCA.

In October 2008, the Indian Air Force asked the Aeronautical Development Agency (ADA) to prepare a detailed project report on the development of a Medium Combat Aircraft (MCA) incorporating stealth features.

In February 2009, ADA director P.S Subramanyam said at a Aero-India 2009 seminar, that they are working closely with Indian Air Force to develop a Medium Combat Aircraft. He added that according to the specification provided by the Indian Air Force, it would likely be a twenty ton aircraft powered by two GTX Kaveri engines.

In April 2010, the Indian Air Force issued the Air Staff requirements (ASR) for the AMCA which placed the aircraft in the twenty five ton category.

AMCA Design

The AMCA will be designed with a very small radar cross-section and will also feature serpentine shaped air-intakes, internal weapons and the use of composites and other materials.

It will be a twin-engined design using the GTX Kaveri engine with thrust vectoring with the possibility of giving the aircraft supercruise capabilities. A wind-tunnel testing model of the MCA airframe was seen at Aero-India 2009.

As well as advanced sensors the aircraft will be equipped with missiles like DRDO Astra and other advanced missiles, stand-off weapons and precision weapons. The aircraft will have the capability to deploy JDAM's. The aircraft will feature Extended detection range and targeting range with the ability to release weapons at supersonic speeds. The aircraft's avionics suite will include AESA radar IRST and appropriate Electronic warfare systems and all aspect missile warning suite.

As of August 2011, the aircraft is in its preliminary design phase. The final design is expected to be shown to the air force by 2012, after which full scale development on the aircraft may start.



Tuesday, August 30, 2011

Next Generation Air Dominance

Next Generation Air Dominance

Next Generation Air Dominance is a development and acquisition program for a future sixth generation air superiority fighter to replace the US Navy’s F/A-18E/F Super Hornet beginning in 2025. It is planned to incorporate sixth generation stealth capability. The aircraft is to be operated with or without a pilot, depending on the role. The new fighter is to perform strike, air superiority, ground support, precision bombing and reconnaissance roles. Only Boeing is known to have interest in the program though Northrop Grumman is known to be developing a carrier-based aircraft known as the X-47B. A 1/16 scale model shown at the Navy League Sea Air Space Exposition 2010 shows a 'Flying wing' design with no vertical tails and twin engines.

In late 2011, the Navy plans to analyze alternatives for the NGAD program with a technology demonstration phase beginning in 2013. One of the alternatives being considered is the Lockheed Martin F-35 Lightning II, which would double the Navy's purchase of that aircraft.

Sunday, July 12, 2009

F-117 Nighthawk US Military (US Air Force) Ground Attack Aircraft





F-117 NighthawkThe Lockheed F-117 Nighthawk is a stealth ground attack aircraft formerly operated by the United States Air Force. The F-117A's first flight was in 1981, and it achieved Initial Operational Capability status in October 1983. The F-117A was "acknowledged" and revealed to the world in November 1988.

A product of the Skunk Works and a development of the Have Blue prototype, it became the first operational aircraft initially designed around stealth technology. The F-117A was widely publicized during the Gulf War of 1991.

The Air Force retired the F-117 on 22 April 2008, primarily due to the acquisition and eventual deployment of the more effective F-22 Raptor and F-35 Lightning II.

F-117 Nighthawk Specifications

General characteristics
  • Crew: 1
  • Length: 69 ft 9 in (20.08 m)
  • Wingspan: 43 ft 4 in (13.20 m)
  • Height: 12 ft 9.5 in (3.78 m)
  • Wing area: 780 ft² (73 m²)
  • Empty weight: 29,500 lb (13,380 kg)
  • Loaded weight: 52,500 lb (23,800 kg)
  • Powerplant: 2× General Electric F404-F1D2 turbofans, 10,600 lbf (48.0 kN) each

Performance

  • Maximum speed: Mach 0.92 (617 mph, 993 km/h)
  • Cruise speed: Mach 0.92
  • Range: 930 NM (1720 km)
  • Service ceiling: 69,000 ft (20,000 m)
  • Wing loading: 65 lb/ft² (330 kg/m²)
  • Thrust/weight: 0.40

Armament

  • 2 × internal weapons bays with one hardpoint each (total of two weapons) equipped to carry:
  • Bombs:
    • BLU-109 hardened penetrator
    • GBU-10 Paveway II laser-guided bomb
    • GBU-12 Paveway II laser-guided bomb
    • GBU-27 Paveway III laser-guided bomb
    • JDAM INS/GPS guided munition
F-117 Nighthawk Design

About the size of an F-15C Eagle, the single-seat F-117A is powered by two non-afterburning General Electric F404 turbofan engines, and has quadruple-redundant fly-by-wire flight controls. It is air refuelable. To lower development costs, the avionics, fly-by-wire systems, and other parts are derived from the F-16 Fighting Falcon, F/A-18 Hornet and F-15E Strike Eagle.

Among the penalties for stealth are lower engine power thrust, due to losses in the inlet and outlet, a very low wing aspect ratio, and a high sweep angle (50°) needed to deflect incoming radar waves to the sides. With these design considerations and no afterburner, the F-117 is limited to subsonic speeds.

The F-117A is equipped with sophisticated navigation and attack systems integrated into a digital avionics suite. It carries no radar, which lowers emissions and cross-section. It navigates primarily by GPS and high-accuracy inertial navigation. Missions are coordinated by an automated planning system that can automatically perform all aspects of a strike mission, including weapons release. Targets are acquired by a thermal imaging infrared system, slaved to a laser that finds the range and designates targets for laser-guided bombs.

The F-117A's split internal bay can carry 5,000 lb (2,300 kg) of ordnance. Typical weapons are a pair of GBU-10, GBU-12, or GBU-27 laser-guided bombs, two BLU-109 penetration bombs, or two Joint Direct Attack Munitions (JDAMs), a GPS/INS guided stand-off bomb.





Sukhoi Su-30MKI Review and Videos



Sukhoi Su-30MKIThe Sukhoi Su-30 MKI is a variant of the Sukhoi Su-30 jointly-developed by Russia's Sukhoi Corporation and India's Hindustan Aeronautics Limited (HAL) for the Indian Air Force (IAF). It is an air superiority fighter which can also act as a multirole, strike fighter jet.

The development of the variant started after India signed a deal with Russia in 2000 to manufacture 140 Su-30 fighter jets. The first Russian-made Su-30MKI variant was integrated into the IAF in 2002, while the first indigenous Su-30MKI entered service with the IAF in 2004. In 2007, the IAF ordered 40 additional MKIs. As of July 2009, the IAF has 98 MKIs under active service and it plans to have an operational fleet of 250 MKIs by 2015.

Capable of carrying nuclear weapons and tailor-made for Indian specifications, the fighter jet integrates Indian systems and avionics. It also contains French and Israeli subsystems. The MKI variant features several improvements over the basic K and MK variants and is classified as a 4.5 generation fighter aircraft. Due to similar features and components, the MKI variant is often considered to be a customized Indian variant of the Sukhoi Su-35.



Sukhoi Su-30MKI General characteristics

  • Crew: 2
  • Length: 21.935 m (72.97 ft)
  • Wingspan: 14.7 m (48.2 ft)
  • Height: 6.36 m (20.85 ft)
  • Wing area: 62.0 m² (667 ft²)
  • Empty weight: 17,700 kg (39,300 lb)
  • Loaded weight: 24,900 kg (54,895 lb)
  • Max takeoff weight: 38,800 kg (85,600 lb)
  • Powerplant: 2× Lyulka AL-31FP turbofans with thrust vectoring, 131 kN (29,449 lbf) each

Sukhoi Su-30MKI Performance

  • Maximum speed: Mach 2.35 (2,500 km/h) at 11,000 m (36,000 ft)
  • Range: 5,000 km (2,700 nmi) at altitude; (1,270 km, 690 nmi near ground level)(With Internal Fuel Tank)
  • Service ceiling: 17,300 m (56,800 ft)
  • Rate of climb: >304 m/s (70,000 ft/min)
  • Wing loading: 401 kg/m² (98 lb/ft²)
  • Thrust/weight: 1.07 (at loaded weight & 1.15 with 50% fuel)

Armament: Air to Air Missiles:

  • 6 × R-27R/AA-10A/Astra semi-active radar homing medium range AAM of range 80 km.
  • 6 × R-27T (AA-10B) infrared homing seeker, medium range AAM, 70 km
  • 2 × R-27P (AA-10C) passive radar seeker, long range AAM
  • 10 × R-77 (AA-12) active radar homing medium range AAM, 100 km
  • 6 × R-73 (AA-11) short range AAM, 30 km

Air to Surface Missiles:

  • 2 × Kh-59ME TV guided standoff Missile, 115 km
  • 2 × Kh-59MK Laser guided standoff Missile, 130 km
  • 4 × Kh-35 Anti-Ship Missile, 130 km
  • 3 × PJ-10 Brahmos Supersonic Cruise Missile,300 km
  • 6 × Kh-31P/A anti-radar missile, 70 km
  • 6 × Kh-29T/L laser guided missile, 30 km
  • 4 × S-8 rocket pods (80 unguided rockets)
  • 4 × S-13 rocket pods (20 unguided rockets)

Bombs:

  • 6 × KAB-500L laser guided bombs
  • 3 × KAB-1500L laser guided bombs
  • 8 × FAB-500T dumb bombs
  • 28 × OFAB-250-270 dumb bombs
  • 32 × OFAB-100-120 dumb bombs
  • 8 × RBK-500 cluster bombs
Su-30MKI
Role Multirole fighter, air superiority fighter
National origin Russia / India
Manufacturer Hindustan Aeronautics Limited under licence from Sukhoi)
Designed by Sukhoi Design Bureau
First flight IAF Su-30: 1 July 1997

Su-30MKI: 2000
Introduced 27 September 2002
Status Active
Primary user Indian Air Force
Produced 2000–present
Number built ~100 as of August 2011
Unit cost INR1.61 billion (US$35.9 million)
Developed from Sukhoi Su-30
Variants Sukhoi Su-30MKK

Sukhoi Su-30MKM


Airframe

The Sukhoi Su-30 MKI is a highly integrated twin-finned aircraft. The airframe is constructed of titanium and high-strength aluminium alloys. The engine nacelles are fitted with trouser fairings to provide a continuous streamlined profile between the nacelles and the tail beams. The fins and horizontal tail consoles are attached to tail beams. The central beam section between the engine nacelles consists of the equipment compartment, fuel tank and the brake parachute container. The fuselage head is of semi-monocoque construction and includes the cockpit, radar compartments and the avionics bay.

Cockpit and ergonomics

The Sukhoi Su-30 MKI cockpit instrumentation The displays include a highly customised version of the Elbit Su 967 head-up display consisting of bicubic phase conjugated holographic displays and seven liquid crystal multifunction displays, six 127 mm x 127 mm and one 152 mm x 152 mm. The HUD was widely misreported to be the VEH 3000 from Thales. Variants of the same HUD have also been chosen for the IAF's MiG-27 and SEPECAT Jaguar upgrades, on grounds of standardisation. Flight information is displayed on four LCD displays which include one for piloting and navigation, a tactical situation indicator, and two for display systems information including operating modes and overall operation status. The rear cockpit is fitted with a larger monochromatic screen display for the air-to-surface missile guidance.

Flight control

The Sukhoi Su-30 MKI aircraft has a fly by wire (FBW) with quadruple redundancy. Depending on the flight conditions, signals from the control stick position transmitter or the FCS will be coupled to the remote control amplifiers. These signals are combined with feedback signals fed by acceleration sensors and rate gyros. The resultant control signals are coupled to the high-speed electro-hydraulic actuators of the elevators, rudders and the canard. The output signals are compared and, if the difference is significant, the faulty channel is disconnected. FBW is based on a stall warning and barrier mechanism which prevents development of aircraft stalls through a dramatic increase in the control stick pressure. This allows a pilot to effectively control the aircraft without running the risk of reaching the limit values of angle of attack and acceleration. Although the maximum angle of attack is limited by the canards the FBW acts as an additional safety mechanism.

General features

The Sukhoi Su-30 MKI displays include a highly customized version of the Elbit Su 967 head-up display consisting of bi-cubic phase conjugated holographic displays and seven liquid crystal multifunction displays, six 127 mm x 127 mm and one 152 mm x 152 mm. The HUD was widely misreported to be the VEH 3000 from Thales. Variants of the same HUD have also been chosen for the IAF's MiG-27 and SEPECAT Jaguar upgrades, on grounds of standardization. Flight information is displayed on four LCD displays which include one for piloting and navigation, a tactical situation indicator, and two for display systems information including operating modes and overall operation status. The rear cockpit is fitted with a larger monochromatic screen display for the air-to-surface missile guidance. The Sukhoi Su-30 MKI on-board health and usage monitoring system (HUMS) monitors almost every aircraft system and sub-system including the avionics sub-systems. It can also act as an engineering data recorder

Navigation

The Sukhoi Su-30 MKI aircraft is fitted with a satellite navigation system (A-737 GPS compatible), which permits it to make flights in all weather, day and night. The navigation complex comprises high accuracy SAGEM integrated global positioning system and ring laser gyroscope inertial navigation system.

Pilot ejection

The Sukhoi Su-30 MKI crew are provided with zero-zero KD-36DM ejection seats. The rear seat is raised for better visibility. The cockpit is provided with containers to store food and water reserves, a waste disposal system and extra oxygen bottles. The KD-36DM ejection seat is inclined at 30º, to help the pilot resist aircraft accelerations in air combat.

Aerodynamics

The Sukhoi Su-30 MKI aerodynamic configuration is an unstable longitudinal triplane. The canard increases the aircraft lifting ability and deflects automatically to allow high angle-of-attack (AoA) flights allowing it to perform Pugachev's Cobra . The integral aerodynamic configuration combined with thrust vectoring results in extremely capable maneuverability, taking off and landing characteristics. This high agility allows rapid deployment of weapons in any direction as desired by the crew. The canard notably assists in controlling the aircraft at large angles-of-attack and bringing it to a level flight condition. The wing will have high-lift devices featured as deflecting leading edges, and flaperons acting as flaps and ailerons.

Radar

The forward facing NIIP N011M Bars (Panther) is a powerful integrated passive electronically scanned array radar. The N011M is a digital multi-mode dual frequency band radar. The N011M can function in air-to-air and air-to-land/sea mode simultaneously while being tied into a high-precision laser-inertial or GPS navigation system. It is equipped with a modern digital weapons control system as well as anti-jamming features. N011M has a 350 km search range and a maximum 200 km tracking range, and 60 km in the rear hemisphere. The radar can track 15 air targets and engage the 4 most dangerous simultaneously. These targets can even include cruise missiles and motionless helicopters. The Su-30MKI can function as a mini-AWACS as a director or command post for other aircraft. The target co-ordinates can be transferred automatically to at least 4 other aircraft. The radar can detect ground targets such as tanks at 40–50 km.

A modified Sukhoi Su-30 MKI is being developed to carry BrahMos cruise missiles, with induction planned for 2012. The program is experiencing difficulties due to the enormous weight of the missile.

Avionics

Laser-optical locator system

OLS-30 laser-optical locator system to include a day and night FLIR capability and is used in conjunction with the helmet mounted sighting system. The OLS-30 is a combined IRST/LR device using a cooled, broader waveband, sensor. Detection range is up to 90 Km, whilst the laser ranger is effective to 3.5 Km. Targets are displayed on the same LCD display as the radar.

LITENING targeting pod

Israeli LITENING targeting pod is used to target the laser guided munitions. Litening incorporates in a single pod all the targeting features required by a modern strike fighter. The original Litening pod includes a long range FLIR, a TV camera, a flash-lamp powered laser designator, laser spot tracker for tracking target designated by other aircraft or from the ground, and an electro-optical point and inertial tracker, which enabled continuous engagement of the target even when the target is partly obscured by clouds or countermeasures. The pod integrates the necessary laser rangefinder and designator, required for the delivery of Laser Guided Bombs, cluster and general purpose bomb.

Electronic countermeasures

The Sukhoi Su-30 MKI has electronic counter-measure systems. The RWR system is an indigenously developed system by DRDO, called Tarang, (Wave in Sanskrit). It has direction finding capability and is known to have a programmable threat library. The RWR is derived from work done on an earlier system for India's MiG-23BNs known as the Tranquil, which is now superseded by the more advanced Tarang series. Elta EL/M-8222 a self-protection jammer developed by Israel Aircraft Industries is the MKI's standard EW pod, which the Israeli Air Force uses on its F-15s. The ELTA El/M-8222 Self Protection Pod is a power-managed jammer, air-cooled system with an ESM receiver integrated into the pod. The pod contains an antenna on the forward and aft ends, which receive the hostile RF signal and after processing deliver the appropriate response.

Propulsion

The Sukhoi Su-30 MKI is powered by the two Al-31FP turbofans. Each Al-31FP is rated at 12,500 kgf (27,550 lbf) of full afterburning thrust. Two AL-31FP by-pass thrust-vectoring turbojet reheated engines (25,000 kgf full afterburning thrust) ensure a 2M horizontal flight speed (a 1350 km/h ground-level speed) and a rate of climb of 230 m/s. The mean time between overhaul for the AL-31FP is given at 1,000 hours with a full-life span of 3,000 hours. The titanium nozzle has a mean time between overhaul of 500 hours. Al-31FP builds on the Al-37FU with the capability to vector in 2 planes. The TVC nozzles of the MKI are mounted 32 degrees outward to longitudinal engine axis (i.e. in the horizontal plane) and can be deflected ±15 degrees in the vertical plane. This produces a cork-screw effect and thus enhancing the turning capability of the aircraft. There is no strain-gauge engine control stick to change the engine thrust in the cockpit, rather just a conventional engine throttle control lever. The pilot controls the aircraft with help of a standard control stick. On the pilot's right there is a switch which is turned on for performing difficult maneuvers. After the switch-over, the computer determines the level of use of aerodynamic surfaces and swiveling nozzles and their required deflection angles.

Fuel system

The Sukhoi Su-30 MKI has a range of 5,000 km with internal fuel which ensures a 4.5 hour combat mission. Also, it has an in-flight refueling (IFR) probe that retracts beside the cockpit during normal operation. The air refueling system increases the flight duration up to 10 hours with a range of 8,000 km at a cruise height of 11 to 13 km. Su-30 MKIs can also use the Cobham 754 buddy refueling pods.

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