Mikoyan MiG-35 (Fulcrum-F)

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The Mikoyan MiG-35 is the latest incarnation of the successful light-weight MiG-29 Fulcrum series. With an increase to its MTOW as much as 30 percent, the MiG-35 is now considered in the medum weight class. The aircraft is codenamed "Fulcrum-F" by NATO and is considered a full-fledged multi-role platform utilizing the latest in targeting and tracking systems comparable to Western aircraft types. The aircraft is intended as an export product and is adaptable to various Western systems to open the product up more favorably to the market. The MIG-35 is a further development of the MiG-29M series and features advancements made through the MiG-29K model as well.

As of this writing, the MiG-35 exists in a handful of working flyable prototype forms with the aircraft's initial official appearance coming at Aero India 2007. It is currently being offered to India as the Mikoyan solution to Indian multi-role aircraft needs. Among the contenders are the venerable American Lockheed Martin F-16 Falcon and Boeing/McDonnell Douglas F/A-18 Super Hornet models, the French Dassault Rafale, the Swedish SAAB JAS 39 Gripen and the European consortium Eurofighter Typhoon. Some 125 aircraft are expected to be purchased from this preliminary single order by India.

In terms of finding equal footing with its Western counterparts, the MiG-35 does just that in sporting three large liquid-crystal multi-function displays as opposed to the old Soviet/Russian trademark design philosophy of incorporating analog electronic dials. In the two-seat version of the MiG-35, the rear cockpit features no fewer than an additional four multi-function displays of this type. Perhaps the most important upgrade to the life of the series is the inclusion of the powerful Phazotron Zhuk-AE active electronically-scanned array offering improved target tracking (improved array range for early detection, multiple target tracking, etc...) and enemy target avoidance. Targets can be designated through the helmet mounted system in both air-to-air and air-to-surface modes. Air-to-air detection can occur as far away as 45 kilometers while air-to-surface detection is within 20 kilometers. Beyond the advanced radar and targeting systems, the MiG-35 will feature a higher-rated engine capable of 19,840lbf and afterburn. The engines can also be adapted to fit vectored-thrusting nozzles for improved handling and dogfighting capabilities.

As an export product, the MiG-35 is intended to be as friendly as possible when it comes to adapting itself to foreign-designed weaponry and avionics suites. Base weaponry is a single 30mm GSh-1 series cannon while the 8 external hardpoints can mount a variety of air-to-air and air-to-surface weaponry, from missiles to bombs and rockets to fuel tanks. The improvements throughout the MiG-35 have now brought its general classification up to a medium-weight aircraft and an integrated in-flight refueling system has also been documented.

McDonnell Douglas EA-18G Growler

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The EA-18G is a derivative of the proven two-seat F/A-18F Super Hornet being developed by the Boeing corporation to meet the US Navy requirements for EA-6B Prowler replacement in the 2009 timeframe. The EA-18G program was valued at $8.66 billion including developmental costs (2005 estimate).

In December 2003, the US Navy awarded Boeing a $1 billion contract for EA-18G System Development and Demonstration (SDD) allowing for an initial operational capability (IOC) by 2009. Up to 90 aircraft will be procured by the US Navy to replace EA-6B Prowler fleet by 2012.

The EA-18G airborne electronic attack aircraft should be able to carry up to 5 ALQ-99, 2 AIM-120C AMRAAM air-to-air missiles, 2 AGM-88 HARM missiles, and the AN/ALQ-218(V)2 electronic warfare receiver suite.

On March 18, 2005, Northrop-Grumman announced that the first fuselage section was completed marking an important milestone for the EA-18G electronic attack aircraft program.

Sukhoi Su-35 (Flanker-E / Super Flanker)

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The Su-35 (and similar Su-37) is known as the "Super Flanker" (NATO reporting codename of "Flanker-E"). The Su-35 is based on the Su-27 Flanker air-superiority fighter developed in the 1980's with the Su-35 representing a "more-capable" Su-27 and able to take on sorties in the multi-role, long-range mold. The inherent qualities of the Su-27 system as an air superiority fighter have been melded together with strike fighter capabilities to produce the more lethal Su-35.

The Su-35 features a variety of upgrades and updates over the base Su-27 series and is the pinnacle of the Su-27M model development (first flight achieved in 1988). Among these features are an integrated in-flight refueling probe, provisions for ECM pods, upgraded and more powerful engines, larger wings and forward and rear-facing Phazotron radar systems capable of tracking 24 targets up to 62 miles (100km) away over uneven terrain. An additional auxiliary internal reserve fuel tank has been added to the tail fins as well. The cockpit features updated color CRT and HUD displays and digital fly-by-wire featuring a quadruple redundant system capable of finding four different ways for the computer to achieve the pilots requested control action. The new Su-35 designation came about in 1993 through the aircraft was showcased in the Farnborough Air Show a year prior.

Two Su-27 aircraft were utilized in another improvement program becoming the Su-37 "Flanker-F". Similar to the Su-35 model, these systems featured thrust vectoring nozzles for increased agility. Only two were ever produced before the experimental program was shelved - the test aircraft being converted into full Su-35 variants.

Ten total prototypes of the Su-35 were built, four being conversions from existing Su-27s while the rest were new-build aircraft. Official Russian evaluation occurred in 1996. As of this writing, the Su-35 is only in limited production numbers with Russian forces and it has not been placed into service with any other known operator. The Indian-exported Su-30MKI variant is said to retain some of the reported Su-35 systems and ability mentioned above.

Main specifications
Length: 21.9 meters
Height: 5.9 meters
Wingspan: 15.3 meters

Take-off weight, with two R-77 and two R-73: 25.3 tons
Take-off weight, with maximum payload: 34.5 tons
Total thrust available, two Saturn 177S powerplants: 29 tons
Thrust to weight ratio, under normal and maximum load: 1.14 / 0.84

Maximum fuel in integrated fueltanks: 11.5 tons
Maximum weapons load: 8 tons

Service ceiling: 18 kilometers
Range with maximum fuel, on sea-level and altitude: 1,580 km / 3,600 km
Ferry range, with two PTB-2000 external tanks: 4,500 km

Acceleration from 600kph to 1100kph, at 1000m alt and 50% fuel: 13.8 seconds
Acceleration from 1100kph to 1300kph, at 1000m alt and 50% fuel: 8.0 seconds
Maximum rate of climb, at 1000m alt: 280 meters / sec
Maximum airspeed, low-level and altitude (200m / 11000m): 1,400 kph / M2.25
Maximum G-load: 9 G’s

Take-off run, full afterburner, normal weight: 400-450 meters
Landing roll, brakes + parachute, standard landing weight: 650 meters


Weapons
Novator R-72 (KS-172S-1) or Vympel R-37M (”Arrow”): 400 km range, active and semi-active radar, passive radiation guidance
Maximum of five carried. AAM.
Vympel R-77 / RVV-AE (”Adder”): 100 km range, active radar guidance
Maximum of twelve carried. AAM.
Vympel R-27ET[1] (”Alamo”): 110-130 km range, thermal guidance
Maximum of four carried. AAM.
Vympel R-27EP[1] (”Alamo”): 110-130 km range, passive radiation guidance
Maximum of four carried. AAM.
Vympel R-27ER[1] (”Alamo”): 110-130 km range, semi-active radar guidance
Maximum of eight carried. AAM.
Vympel R-73E (”Archer”): 30 km range, thermal guidance
Maximum of six carried. AAM.

Non-specified ultralong range air to ground missile: Maximum of one carried. AGM.
Non-specified long range air to ground missile: Maximum of three carried. AGM.
Non-specified long range anti-radar missile: Maximum of five carried. AGM.
Non-specified long range air to ship missile: Maximum of five carried. ASM.

Raduga X-59M[K] Ovod (”Kazoo”): 140 km range, TV guidance
Maximum of 5 carried, AGM/ASM.
Zvezda X-31A/P (”Krypton”): 70 / 140 km range, active radar / passive radiation guidance
Maximum of 6 carried, AGM.
Molniya X-29TE[L] (”Kedge”): 10 km range, TV / laser guidance
Maximum of 6 carried, AGM.
FSUE LGB-250: 300 kg warhead, laser guidance
Maximum of eight carried, smart bomb.
FSUE KAB-500KR/OD: 500 kg warhead, TV guidance
Maximum of eight carried, smart bomb.
FSUE KAB-1500KR/LG: 1500 kg warhead, TV / laser guidance
Maximum of three carried, smart bomb.
S-25LD: 10 km range, laser guidance
Maximum of six carried, guided rocket.

500kg class bomb: Maximum of ten carried, gravity bomb.
250kg class bomb: Maximum of thirty-two carried, gravity bomb.
B-8M-1: Maximum of 120 carried in six dispensers, unguided rocket.
B-13L: Maximum of 30 carried in six dispensers, unguided rocket.
S-250FM-PU: Maximum of six carried, unguided rocket.

Lockheed F-35 Lightning II / X-35 JSF (Joint Strike Fighter)

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The F-35 Lightning II is a next generation multi-role platform appearing in three variants. It is a single-seat fighter offering up some of the most advanced technology and avionics systems available and incorporates new stealth elements and technology into its design. The system is predominantly being headed up by Lockheed Martin and partnered with UK firm BAe Systems and American firm Northrop. The system was born out of the Joint Strike Fighter program of the late 1990's, to which the system was then known as the X-35 and faced off successfully against Boeing's own X-32 technology demonstrator.

Visually, the F-35 Lightning II appears very much like its F-22 Raptor predecessor, incorporating the similar "diamond" angled shape into the fuselage and wings. The twin vertical tail surfaces are each angled and fitted over the supercruise-capable engine exhaust ports at rear. Angled intakes are mounted on either side and to the rear of the single seat cockpit area. The powerplant consists of a single General Electric/Rolls-Royce brand turbofan generating some 40,000lbs of thrust. The vertical take-off and landing model will feature an additional Rolls-Royce lift fan system fitted in the center of the fuselage and delivering some 18,000lbs of vertical thrust.

Based on lessons learned in the development of the F-22 Raptor, the F-35 Lightning II will also feature internal weapons bays, reducing the radar signature of the aircraft. Additionally, the system will also have provision for up to four external hardpoints if needed. A 25mm cannon will be made the standard close-in weapon. A variety of "smart" air-to-air and air-to-surface munitions will be the backbone of the Lightning II arsenal.

The Lightning II will be featured in three principle designs, each maintaining external similarities but differing in dedicated roles. The F-35A model is the true Conventional Take-Off and Landing (CTOL) variant model, operating from runways in the traditional role. The F-35B is the Short Take-Off and Vertical Landing (STOVL) derivative in the series, operating in the role most closely associated with the AV-8B Harrier II system. The F-35C model is a dedicated carrier-based (CV) model designed specifically for operations on aircraft carriers that require their systems to feature strengthened internal structures and landing gear and space-saving capabilities.

Some 3,100 F-35 systems are on order though it remains to be seen who many will actually be purchased and delivered for operational use. The system is slated to appear in the US military inventory in 2011. As a whole, the F-35 has a proposed technology shelf-life up until 2040. The F-35 Lightning II is named after the other famous Lockheed product (of World War 2) in the propeller-driven, twin-boom P-38 Lightning. The British Aircraft Corporation (or "BAC", a forerunner to BAe or "British Aerospace") also produced a Cold War fighter designated as the English Electric/BAC Lightning.