link : Single Engine Fighter Cancellation Provides An Opening For Tejas MK-2
Single Engine Fighter Cancellation Provides An Opening For Tejas MK-2
Source:-Single Engine Fighter Cancellation Provides An Opening For Tejas MK-2
The recent withdrawal of the move to import 114 ‘single-engine fighters’ (SEF) by India’s Ministry of Defence (MoD) opens a window of opportunity for the Aeronautical Development Agency (ADA), controlled by the Defence Research & Development Organization (DRDO), to rekindle its effort to develop a MK-II variant of the Tejas light combat aircraft (LCA). Because, even though reports suggest that MoD is planning to replace the SEF competition with a larger competition that will see both single and twin- engined jet fighters in contention (in a manner reminiscent of the failed multi-role medium range combat aircraft (MMRCA) tender from a decade ago), the most realistic way to augment the Indian Air force’s (IAF’s) combat strength continues to be the building of more Tejas variants, as we have argued before. As such, it is now time for DRDO to use its internal allocations to fund the further development of the Tejas MK-II, with full support from MoD, in order to be future ready given that fighter import tenders take a lot of time in India and may never actually reach fruition, judging by recent experience.
The MK-II design must return
ADA, has long proposed a Tejas MK-II with a more powerful engine than the baseline MK-I, as well as aerodynamic refinements, to address the IAF’s 1995 air staff qualitative requirements (ASQR) with respect to kinematic performance. After all, one of the regrets of the IAF has been the fact that the MK-I design does not meet the ASQR in terms of sustained turn rate (STR), transonic acceleration and climb rate. The developers of the Tejas, i.e. ADA, however believe that the MK-II design, which will also incorporate a pair of canards, will be able to address MK-I’s shortfalls in terms of aerodynamic performance. The 1995 ASQR apparently requires a STR of 18 degrees per second (same as the F-16’s) and Mk-II will close in on that. The climb rate will also be more or less satisfactorily reached. Transonic acceleration is expected to be realized fully. Moreover the Mk-II airframe will be able to reach a top speed of Mach 1.8 at altitude.
Development work on MK-II had been progressed by ADA over the years as part of the overall allocations for the LCA programme. Currently, ADA’s work on the Tejas is being financed via the LCA Phase-III project which was sanctioned in November 2009 with an allocation of Rs 2431.55 crores and is scheduled to be complete by December 2018. Most of this allocation has gone towards developmental activities related to achieving operational clearances for the MK-I design as well general development work on the Tejas design family (Air force version). However, while funds from this allocation have helped advance the Tejas MK-II design to a level where the ‘inboard’ i.e the complete layout for Mk-II is ready and plenty of wind tunnel work into adding a pair of canards has also been done, it is not enough for ADA to develop a pair of MK-II prototypes. For that, fresh allocations are required.
ADA’s confidence with respect to this timeline also stems from the fact that modifications to the 98 kilo newton generating F414-GE-INS6 (F414), in order for it to fit the MK-II design, have already been certified by the Center for Military Airworthiness and Certification (CEMILAC). What is more, eight of the 99 F414 engines ordered by ADA earlier have already been delivered to it by GE. Clearly, ADA now has some engines waiting for an airframe, i.e MK-II. The F414-GE-INS6 is of course more powerful than the F-404-GE-IN20 (F-404) engine that currently powers MK-I.
Moreover, the Mk-I design has some 25-30 percent commonality in parts with MK-I and these parts (i.e not requiring any modification) are already in production. For the MK-I parts that have to be replaced, thousands of new drawings have being worked upon jointly by
Not just more agile
While the Mk-II design is expected to achieve a 5 percent improvement in drag characteristics through ‘production improvements’ related to further streamlining (reduced contour variations etc) of the Mk-I airframe, it is actually a step up from the baseline MK-1 and even the improved MK-1A in other ways as well.
While HAL is looking to outfit MK-1A with an imported active electronically scanned array (AESA) and a foreign self-protection jammer, MK-II should fly with the indigenous Uttam AESA being developed by DRDO’s Electronics and Radar Development Establishment (LRDE) and the ‘unified electronic warfare suite’ (UEWS) created by the Defence Avionics Research Establishment (DARE), another DRDO lab, in partnership with Israel’s Elisra. Uttam, which weighs 120 kg, has been put through extensive ground evaluation by LRDE and is reportedly ready for integration onto a Tejas test vehicle. UEWS is currently undergoing tests on the Tejas PV-6 prototype vehicle.
A modular ‘Make in India’
Not only is MK-II supposed to be a superior product in terms of performance, it will also lend itself to being produced quicker, as is the need of the day. ADA has done of a lot of work together with HCL with the objective of making the Mk-II design ‘modular’. In this modular scheme of things, HAL as the integrator will receive 8-10 Tejas MK-II ‘modules’ as sub-assemblies from domestic private companies such as L&T and will then put them together to build a complete aircraft ready for checkout and flight testing. Each of these module suppliers will therefore be ‘Tier-I’ suppliers to HAL and will receive LRUs from Tier-II suppliers (w.r.t to HAL) for integration into the modules, which will then be dispatched to HAL. According to Dr K.Tamilmani, former Director General Aeronautics, DRDO, ‘The idea is to ‘terminate’ things like electrical looms, hydraulic pipes, fuel line pipes etc. at the module level which can then be connected with other such modules.’
Of course, for the Tejas Mk-II program to be an all-round success in the industrial sense, the time has come for India to get GE to produce the complete F-414 engine on Indian soil in association with a domestic partner. In this light, the setting up of a joint venture between GE and Tata Advanced Systems Limited (TASL) in Adibatla for the manufacture of various components of GE engines looks like a timely development. This JV which will see the setting up of tooling that can produce F-414 parts, can be encouraged by the Indian Government to take on the production of the entire F-414 engine under manufacturing know how transfer from GE.
The F-414 can actually be retro-fitted onto the Mk-I/IA airframes also since the existing intake of these aircraft can easily handle the additional mass flow from the F-414 as compared to the F-404. Of course, other modifications to the Mk-I/IA airframe will be required for this purpose. In the course of its lifetime any single-engined jet fighter needs about 3.5 jet engines. So a hypothetical run of at least 200 Tejas MK-II in addition to the 123 Mk-1/1A (modified to field the F-414) that are on order will mean that the IAF’s future fleet will require north of 1100 F-414 engines in the course of their service life. Clearly, GE should not have any compunctions in transferring know how for even the F-414 core for an order of that size. Perhaps, the India-US ‘joint working group on jet engine technology’ should burn some midnight oil to explore this potential.
Saurav Jha is the Editor-in-Chief of Delhi Defence Review. Follow him on twitter @SJha1618
Source:- Delhi Defence Review
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