AMCA And Tejas MK II – Challenges And Options
The Balakot air strikes in February 2019 and the air combat thereafter in which a MiG 21 Bison of Indian Air Force (IAF) had to engage a much more modern F-16 of Pakistan Air Force (PAF) has once again brought IAF modernisation back into focus.
The then IAF Chief, Air Chief Marshal BS Dhanoa, has said in many forums that IAF has hit an all time low of 30 fighter squadrons vis-a-vis the government authorised 42. He has highlighted the convergence of strategic interests between China and Pakistan and their rapidly modernising air forces. IAF on the other hand has been slowly losing the clear combat edge that it had enjoyed over Pakistan in 1971 both in terms quality and numbers.
Aerospace is the domain of the future and the one who controls it will control the planet. It is clear that IAF must win the air war for the Army and Navy to win the surface war. Technology intensive air power requires faster replacement of assets due to quicker obsolescence. While IAF has a plan ‘B’ to fight with what it has, if forced into conflict, but numbers are clearly not adequate to fully execute an air campaign in a two-front scenario. It is incumbent upon the nation to provide IAF assets for the task it has been entrusted. It is imperative that IAF quickly rebuilt the squadron strength and acquire modern fighters that are as good or better than the adversaries.
Developing indigenous aircraft is critical for India to become a global power. China has already moved way ahead. The Light Combat Aircraft (LCA) ‘TEJAS’ and the Advanced Medium Combat Aircraft (AMCA) are the main two aircraft projects. It is important to continuously monitor their progress.
4th And 5th Generation Fighters
The ‘TEJAS’ was envisaged to be a 4th generation fighter and the AMCA is meant to be a 5th generation fighter. 4th generation fighters are mostly multi-role; use ‘Energy-Manoeuvrability’ concept for performing ‘fast transients’ – quick changes in speed, altitude, and direction – as opposed to just high speed; lightweight aircraft with higher thrust-weight ratio, and use digital Fly-By-Wire (FBW) flight controls which allow relaxed static stability flight and in turn agility.
They have electronically managed power-plants. Pulse-Doppler fire-control-radars give look-down/shoot-down capability. Head-up displays (HUD), hands-on-throttle-and-stick (HOTAS) controls, and multi-function displays (MFD) allow better situational awareness and quicker reactions. Composite materials help reduce aircraft weight. Improved maintenance design and procedures reduce aircraft turnaround time between missions and generated more sorties. The F-16, F-18, MiG-29, SU-30 MKI and Mirage-2000 are all in this category. A sub generation called the 4.5th generation fighters evolved in the last decade, which saw advanced digital avionics, newer aerospace materials, modest signature reduction, and highly integrated systems and weapons. These fighters operated in network-centric environment. Key technologies introduced include multi-function active electronically scanned array (AESA) radars; longer range BVR AAMs; GPS-guided weapons, solid-state phased-array radars, helmet-mounted sights (HMDS), and improved secure, jamming-resistant data-links.
A degree of super-cruise ability (supersonic without afterburner) was introduced. Stealth characteristics focused on front-aspect radar cross section (RCS) reduction through limited shaping techniques. Eurofighter Typhoon, Dassault Rafale and Saab JAS 39 Gripen were in this category. Many 4th generation aircraft were also upgraded with new technologies. Su-30MKI and Su-35 featured thrust vectoring engine nozzles to enhance manoeuvring.
The fifth generation was ushered in by the Lockheed Martin/Boeing F-22 Raptor in late 2005. These aircraft are designed from the start to operate in a network-centric combat environment, and to feature extremely low, all-aspect, multi-spectral signatures employing advanced materials and shaping techniques. AESA radars are with high-bandwidth low-probability of intercept.
IRST and other sensors are fused in for Situational Awareness and to constantly track all targets of interest around the aircraft 360 degree bubble. Advanced avionics and glass cockpit, and improved secure, jamming-resistant data-links are other features. Avionics suites rely on extensive use of very high-speed integrated circuit (VHSIC) technology and high-speed data buses. Fifth-generation fighters target “first-look, first-shot, first-kill capability”. In addition to high resistance to ECM, they can function as a ‘mini-AWACS’. Integrated electronic warfare system, integrated communications, navigation, and identification (CNI), centralised “vehicle health monitoring”, fibre-optic data-transmission, and stealth are important features. Manoeuvre performance is enhanced by thrust-vectoring, which also helps reduce takeoff and landing distances. Super-cruise is inbuilt.
To maintain low signature primary weapons are carried in internal weapon bays. The current fifth-generation fighter projects include Lockheed Martin F-35 Lightning II, Russia‘s Sukhoi PAK FA (SU-57), China’s Chengdu J-20 and Shenyang J-31, and India’s AMCA. Japan is also exploring technical feasibility to produce fifth-generation fighters.
IAF has committed for 200 TEJAS Mk-II aircraft, taking the total requirement of TEJAS to over 300. TEJAS Mk II was originally planned to retain basic aircraft shape and incorporate the larger and more powerful 98 kN thrust GE F414 engine, which was more likely to meet the TEJAS originally agreed specifications.
This would have meant significant change to the air inlets and also the aircraft dimensions and weight would have to increase. At the Aero India 2019, ADA unveiled a new model of the TEJAS’s Mk-II, and called it a Medium Weight Fighter (MWF). This aircraft was expected to fit into IAF’s requirement for the Medium Multi-Role Combat Aircraft (MMRCA).
This enhanced version of TEJAS, the TEJAS Mk-2 MWF would be 14.6m long with a wingspan of 8.5m (compared with 13 m and 8.2 m respectively for the TEJAS and 14.36m and 9.13m for Mirage 2000). The aircraft will have a compound delta wing with close-coupled canards. This would reduce drag in all angles of attack it was announced. The longer fuselage will allow for more fuel behind the cockpit. The Mk II would carry much more internal and external fuel.
The maximum weight of the aircraft would be 17.5 tonnes (compared to Mk 1’s 13.5 tonnes). Its external stores carrying capacity will increase from 5.3 to 6.5 tonnes. It will be equipped with a higher thrust General Electric GE-F414-INS6 engine that features a Full Authority Digital Electronics Control (FADEC) system.
Source:- Indian Defense News