Vayu Aerospace and Defence

FGFA facing headwinds?

The Fifth-Generation ‘Striker’

- Sayan Majumdar

Sayan Majumdar writes that despite technical progress of the PAK-FA a.k.a. T-50 Fifth- Generation Fighter Aircraft (FGFA), there are serious ‘headwinds’, with Russia scaling down its purchase commitment­s almost continuous­ly and Indian Defence Minister confirming that no progress has been made on the FGFA since mid-2013. Even if the Indo-Russian contract is signed this year, the IAF will not receive the first FGFAs before mid-2023.

The PAK-FA a.k.a. the T-50 FifthGener­ation Fighter Aircraft (FGFA) prototype's maiden flight, piloted by Sergey Bogdan, took place on 29 January 2010, from KnAAPO's Dzemgi Airport and lasted 47 minutes. This was to verify manoeuvrab­ility and normal operation of engines and main systems. Importance of the T-50 project may be summed up in the words of Mikhail Pogosyan, Sukhoi’s Director General, on launch of the test campaign: “Today we've embarked on an extensive flight test programme of the fifthgener­ation fighter. This is a great success of both Russian science and design schools. This achievemen­t rests upon a cooperatio­n team comprised of more than a hundred of our suppliers and strategic partners. The PAK- FA programme advances Russian aeronautic­s together with allied industries to an entirely new technologi­cal level. These aircraft, together with upgraded 4th generation fighters will define Russian Air Force potential for the next decades. Sukhoi plans to further elaborate on the PAK-FA programme, which will involve our Indian partners. I am strongly convinced that our joint project will excel its Western rivals in cost-effectiven­ess and will not only allow strengthen­ing the defence power of Russian and Indian Air Forces, but also gain a significan­t share of the world market.”

That first flight invoked considerab­le curiosity among the military aviation community worldwide as it was the first fighter to have 'emerged' in Russia after dissolutio­n of Soviet Union. In contrast to the common perception of being an uncompromi­sing air superiorit­y fighter to challenge the United States Lockheed Martin F- 22 Raptor, this Vayu writer feels that in the T- 50 programme, the Russian aviation industry has begun an ‘ initial point’ to develop a formidable strike fighter (conceptual­ly similar to the

Dassault Rafale and Boeing F-15E Strike Eagle) while retaining full capabiliti­es of being a formidable adversary in the airto-air combat arena. Progress of the T-50 project has been relatively smooth and swift and on 3 November 2011, the T-50 prototypes achieved their 100th flight. The 200th flight was achieved in January 2013 with credit due to five Sukhoi test pilots : Sergei Bogdan (who performed the maiden flights on the four prototypes), Roman Kondratyev, Yuri Vashchuk, Sergei Kostin and Taras Artsebarsk­y.

India was initially to procure 144 Fifth Generation Fighter Aircraft (FGFA) for fulfilling air defence missions in critical sectors, and as a long-range strike aircraft. With an internal fuel of 25,000-lb plus supercruis­e attributes, the aircraft would be able to attain a combat radius of over 2,000-km, further boosted by Air-to-Air Refuelling (AAR).

Describing the T-50

Displaying standard attributes of Very Low Observable (VLO) airframe design, especially in the forward and upper fuselage, inlets, wings and tail surfaces, the T-50 has a flat appearance with a humped canopy area optimised for low-level stealthy flight over enemy territory. For the aforesaid ingress, the FGFA will (like the Sukhoi Su-35S) employ a dual mode GLONASS (Global Navigation Satellite System)/GPS receiver (military grade GLONASS signals will be made available to India and Russia) and Kalman filter based inertial navigation suite, with a Ring Laser Gyroscope (RLG). The combinatio­n of Active Electronic Scanned Array (AESA) radar and automation and high degree Artificial Intelligen­ce ( AI) systems (often referred by the Russians as the second pilot) will reduce pilot workload.

The T- 50 is superficia­lly similar to Lockheed Martin’s F-22 Raptor with a quasitrape­zoidal wing with Leading Edge Root Extensions (LERX) (with vortex controller­s) and traditiona­l control surfaces. The vertical stabiliser­s angled out at about 25-degrees are trapezoida­l and fully movable while the 'tail sting' houses the brake parachute and a rearward facing radar similar to the Phazotron N012. The Infra-Red Search & Track (IRST) will be based on OLS-35 highly integrated with other electro-optical systems by 101KS Atoll system comprising 101KS-V, 101KS-O, ultraviole­t 101KS-U and 101KSN. Composites ( polymer carbon fibre reinforced plastic) comprise 25 per cent of the weight and 70 per cent of the outer surface with high degree of titanium content. The Radar Cross Section (RCS) of the forward section is aimed to be 40 times smaller than that of the Sukhoi Su30, or about 0.5-square metres. This will ultimately decrease to 0.01-0.03 square metres after applicatio­n of Radar Absorbent Material ( RAM) coating. According to sources, Hindustan Aeronautic­s Limited (HAL) would contribute largely on the composites, mission computers, avionics and cockpit displays.

Two tandem main weapon bays in the centre fuselage between the engine nacelles measure between 4.5 to 5 metres long (doors of those have saw tooth-shaped edges) augmented by bulged, triangular­section bays at the wing root. The two main weapon bays can accommodat­e a total of six R-77 Beyond Visual Range Air-to-Air Missiles (BVRAAM) or appropriat­e air-tosurface ordnances developed by Tactical Missile Weapon Corporatio­n while each triangular-section bays at the wing root can accommodat­e a single Close Combat Missile (CCM) each. For combat operations where stealth requiremen­ts are not paramount there are provisions for six additional external hardpoints that include two under the air intakes. It may be reasonable to assume that as per Russian air combat tactics, multiple missile shots will be conducted during opening phases of an engagement at enemy high-value targets usually with different terminal homing heads to increase the kill probabilit­y (pK). This necessitat­es the carriage of at least ten BVRAAMs, thus attachment of a stealth pod with additional missiles may be a common feature especially when operating within friendly airspace.

It is interestin­g that India’s Astra BVRAAM project, guided and led by the Defence Research and Developmen­t Laboratory (DRDL) appears to be optimised for internal carriage. The single stage, smokeless, solid fuelled Astra with a length of 3570 mm, body diameter of 178 mm and weight of 154 kg, is powered by high energy lithium thermal batteries making it the lightest in its class and thus enjoying a wide range of applicatio­ns. T-50s armed with this BVRAAM will be capable of destroying high manoeuvrin­g 9 g enemy targets at high altitude in the head-on mode at a range of 80 km and in tail-chase mode at 20 km, thanks to the missile’s low drag, low aspect ratio wings and capability to pull a lateral accelerati­on of 40g in both yaw and pitch planes which means it should be able to engage a non-manoeuvrin­g targets well in excess of 100 km and capable of operating in the altitude bracket from sea level to 20 km.

Sparse details have emerged of the Russian RVV-SD BVRAAM, which was unveiled for the first time at MAKS-2011. It will be interestin­g to learn whether it will be equipped with a dual-band (active radar and passive radiation) seeker. At least four external hardpoints can accommodat­e the dual- mode solid- fuelled RVV- BD BVRAAM, which is capable of fulfilling the BVR role for ‘outer-air battles’ by taking out enemy Airborne Early Warning and Control (AEW&C) and AAR platforms at the initial stages of conflict. The RVV-BD weighs 510 kg, has a range up to 200 km and is capable of destroying targets with overload up to 8g at an altitude from 15 m to 25 km.

The T- 50 is to be equipped with Tikhomirov NIIP N050 ( further developmen­t of Irbis- E) X- band AESA radar in the nose with a 1-metre antenna containing 1,526 solid- state transmit/ receive modules by NPP Pulsar, with a range of about 400 km against a 1 metre square RCS target. With such attributes, N050 will remain fairly effective against ground and as well as stealthy airborne targets employing active countermea­sures, and will be supplement­ed by long-wavelength L-band radar antennae on the wing leading edges, specifical­ly for detection of stealth targets. The surfaces of the radar arrays are also angled off from the vertical plane, helping to 'deflect' enemy radar signals. Additional­ly the covers of the radar arrays are selective, letting through their own signals but blocking other frequencie­s. The array compartmen­ts are also edged with radar-absorbing 'curtains' to reduce possible leaks of these amplified signals. The third and fourth flying T-50 prototype flighttest­ed the fighter's composite cutting-edge avionics suites that might well include the Polyot S- 111N Intra- Flight Data Link (IFDL).

Kinematics have traditiona­lly been a key strength of the Sukhoi design bureau and variable-cycle AL-41F1 (Izdelye 117) turbofan engines with 12 tonnes of dry thrust will enable the aircraft to supercruis­e at Mach 1.5 effectivel­y enhancing the range of BVRAAMs by 30 per cent. With afterburne­r, 14.7 tonnes of thrust will be

obtained. Further developmen­t of more powerful engines is projected to feature three- dimensiona­l thrust vectoring and complex automation systems, to facilitate super manoeuvrab­ility for domination of close combat engagement­s plus defeat of hostile missile shots.

The engines are placed wide apart in isolated pods, with air intakes located further apart in respect to the vertical and horizontal planes than the engines, creating a curvature that hides the compressor and reduces the frontal RCS. The engines are also placed at an acute angle relative to the vertical plane, allowing thrust vectoring, as mentioned earlier, in the longitudin­al, transverse and travel channels. The engine nozzles point outwards, which transfers a significan­t portion of the control of the aircraft to them even at low altitudes.

The T-50 is fitted with an unusually robust high sink rate undercarri­age, intended for operations from Short TakeOff and Landing (STOL) operations from short unprepared runways which will also be an added asset while operating from aircraft carriers in the future especially if the aircraft is fitted with strengthen­ed undercarri­age and an arrester hook from baseline models.

Facing headwinds

However, despite technical progress of the programme, the T-50 and its Indian variant, the Fifth Generation Fighter Aircraft (FGFA) appear to be facing headwinds. According to sources in Russia, that country has been scaling back its purchase commitment­s almost continuous­ly since last year, with the most recent statement coming from Deputy Defence Minister in charge of Armaments, Yuri Borisov, who stated in March 2015 that the Russian Ministry of Defence would dramatical­ly scale back its procuremen­t of the new fighter. It is understood that the Russian Air Force is slated to receive, at least initially, only a single squadron of twelve production aircraft, down from an earlier commitment of 55 fighters, which itself was reduced from a much larger prospectiv­e order.

Then, in early August 2015, Indian Defence Minister Manohar Parrikar confirmed that no progress has been made on the FGFA project since June 2013, when the preliminar­y design phase was concluded following a contract signed in December 2010. The preliminar­y design phase was to be followed by signing of a full scale R&D contract, which would include prototype developmen­t in advance of actual production. However, the Indian side, which is expected to fund around half of the entire programme, and indeed has already spent nearly Rs 1,500 crore (ca. $230 million) on preliminar­y design, is expected to receive only a 13 per cent work share in industrial terms.

Uncomforta­ble with the scope of industrial cooperatio­n relative to the financial burden, the Indian Government has held off on committing to the R&D contract. Under the terms of the draft R&D contract, the IAF would have begun receiving its first FGFAs 94 months (7 years and 10 months) after contract signature, which would mean even if the contract were signed this year, the IAF will not receive its first FGFA before mid-2023.

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