Tracking The Tejas: The Design Evolution Of An Indian Fighter Part-I | Delhi Defence Review
Tracking The Tejas: The Design Evolution Of An Indian Fighter Part-I
By
Indranil Roy & Nilesh Rane
-
February 22, 2019
It is no overstatement to say that the Tejas Light Combat Aircraft (LCA) program has made significant progress of late with the Mk1 variant being officially granted Final Operational Clearance (FOC) on February 20, 2019 and its production picking up pace at Hindustan Aeronautics Limited (HAL). Seven of the thirteen Initial Operational Clearance (IOC) standard Tejas Mk1 already in service with No. 45 squadron or the Flying Daggers of the Indian Air Force (IAF) were handed over in the last 11 months alone. The remaining three IOC-standard single-seater aircraft meant for the Flying Daggers are slated to join the squadron by the end of April 2019. The Tejas MK1 is now also a regular at IAF air exercises, raking up high range scores and generally winning the confidence of its users. As such, the focus has now shifted to the development and production of the Tejas Mk1A variant since India’s Defence Acquisition Council has accorded approval for the acquisition of 83 units of the type by the IAF. Before we turn to analyzing developments related to the Mk1A and further evolution of the Tejas platform, it is important to profile the current capabilities of the baseline Mk1 itself.
LCA Tejas Mk1
Tejas Mk1 is a ‘fourth-generation lightweight, single-engine, multi-role, tactical fighter aircraft. It employs an unstable tailless compound delta-wing configuration, optimized primarily for maneuverability and agility’. Over 90 percent of its surface, and over 45 percent of its airframe by weight is made of composite structures. This is one of the highest usage of composites in an aircraft of any kind, anywhere in the world. This extensive use of composites has lowered the aircraft’s weight by 21 percent and reduced its part count by 40 percent, as opposed to what would have been the case had it been of all-metal construction.
The aircraft has intentionally been made longitudinally unstable to enhance maneuverability. In fact, its static margin, i.e. a measure of its instability (and hence maneuverability) is also one of the highest for any modern fighter aircraft [18]. To recover stability and provide good handling qualities, it is equipped with a fully redundant quadruplex digital fly-by-wire flight control system (FCS). This FCS is one of the biggest accomplishments of the LCA program. Its robustness has ensured an accident-free test record of over 4,300 test flights. The aircraft has also been equipped with advanced autopilot capabilities like auto-level (in case of pilot disorientation), safe altitude recovery (which automatically pulls up the aircraft if it comes too close to the ground) and auto navigation modes.
In-service aircraft are certified to fly from -3.5 to +8.0 Gs, up to an altitude of 50,000 feet, a top speed of Mach 1.6, and an angle of attack (AoA) of up to 24 degrees. The test pilots have stretched the prototypes even further, up to 8.5 Gs, and 26 degrees AoA. At the 2016 Bahrain Air Show, the Mk1 had even demonstrated a low speed pass at 110 knots. The FCS has now been updated to lower the minimum speed to 100 knots, at which point auto recovery is initiated. The 2016 demonstration at Bahrain also showcased another important feature: Following the above-mentioned low speed pass the aircraft immediately proceeded to accomplish a vertical climb. The ability to accelerate while in a climb is a virtue that only fighters with a thrust to weight ratio (TWR) of above 1.0 possess. At Bahrain, the Mk1 also showcased an instantaneous turn rate (ITR) of near 30 degrees per second and a sustained turn rate (STR) of between 15 to 16 degrees per second. A minimum radius turn of 350 metres (m) radius was also exhibited. All of these are extremely respectable numbers for air to air (A2A) combat roles.
The Mk1 is equipped with a powerful MultiMode Radar (MMR) which has A2A, air to sea, and air to ground (A2G) target detection modes. In A2A, the Tejas Mk1 is currently capable of firing R-73 close combat missiles (CCMs) and Derby beyond visual range A2A missiles (BVRAAMs). In the future, the Mk1 is likely to be integrated with India’s Astra BVRAAM as well. Together, with state-of-the-art helmet mounted display and sight (HMDS) and hands on throttle-and-stick (HOTAS) controls, and coupled with navigation aides like Very High-Frequency (VHF) Omnidirectional Range (VOR) / Instrument Landing System (ILS) and tactical air navigation system (TACAN), Tejas Mk1 allows the pilot to concentrate on “head-down” mission-critical requirements rather than worry about basic flying.
One of the Tejas’s greatest strengths is its A2G weapon delivery accuracy. In all flight tests and air exercises so far, the Mk1 has consistently garnered some of the highest range scores of all the aircraft in the IAF’s inventory. Not only can it carry 250 kg and 450 kg dumb bombs, but also laser guided bombs (LGBs) which are guided to their targets using a Litening laser designation pod (LDP). A single LGB can be carried on either the center-fuselage, wing-inboard or midboard weapon stations. For dumb bombs, two can be carried in tandem in the wing-inboard pylons, whereas one each can be carried in the center-fuselage and wing-midboard locations.
The Mk1’s all-weather and day/night capability has been proven in various extreme hot and cold weather trials, from Jaisalmer to Leh. For example, in Leh, the aircraft was successfully started after a cold soak of 42 hours where the temperature reached near -20°
C . In each of the three attempts, the aircraft started effortlessly even on a partially drained battery. The reader might be reminded that a few Multi-Medium Role Combat Aircraft (MMRCA) contestants had actually failed this test during trials for that tender. Similarly, in hot and high trials, the aircraft took off with 1.9 tons (50 percent) of its max payload, which is an astounding feet given its highly swept delta wings.
The Tejas Mk1 has a total of five ‘wet’ points: one underneath the fuselage and two underneath each wing. The hardpoint underneath the fuselage can carry a 725 litre (L) subsonic drop tank or a 710 L supersonic tank (still under development). The wing inboard pylon can carry a subsonic drop tank of 1200 L while the midboard can carry a drop tank of 800 L. Although the MK-1’s developer, the Aeronautical Development Agency (ADA) publishes a conservative ferry range of 1750 km, ferry flights of ranges of nearly 2100 km have been completed in the past. The FOC version of the Tejas MK-1 has also been fitted with a fixed refueling probe which can be used to refill all of it internal and external fuel tanks, effectively doubling its range and endurance.
Enter the Tejas Mk1A
Now even while ADA was developing the Tejas Mk2 for the IAF, HAL proposed a simpler interim upgrade. Thus emerged the Tejas Mk1A which will be equipped with an ELTA EL/M- 2052 active electronic scanned array (AESA) radar along with a compatible electronic warfare suite, which would include a self protection jammer (SPJ) pod carried on the outboard wing pylon. This position was found to derive maximum performance out of the pod. On the the outboard pylon, two CCMs would be carried on a dual-rack pylon as shown in Figure 1. This configuration was found to have lowest drag penalties among a variety of studied configurations [19].
In addition to the above changes, HAL would upgrade some line replacement units (LRUs) to cater to obsolescence management, weight reduction, ease of manufacture and maintenance. The aircraft would also be fitted with an Onboard Oxygen Generation System (OBOGS) which would allow pilots to undertake long endurance flights. The turnaround time of the aircraft has also been reduced by means of hot refueling, a feature that SAAB wanted to showcase on its Gripen fighter during the MMRCA competition. At the time, the permission was denied by the IAF since it did not have a standard operational procedure (SOP) set up for the same. This hot refueling capability has now been showcased on a Tejas test aircraft.
Figure 1: One jammer and a twin-assembly of two CCMs at the O/B stations of the aircraft [19].
The initial road to the Mk2
However, to meet the IAF’s stringent air staff qualitative requirements (ASQR) for the LCA project, ADA knew that substantial changes to the basic Mk1/Mk1A airframe were required and that is where the genesis of the Tejas Mk2 development program lies. There were two primary concerns: the IAF wanted a fighter that had faster transonic acceleration and a higher STR of about 18 degrees per second. As late as Aero India 2017, ADA displayed scale models that aimed to achieve this by extending the Mk1 with a 0.5 m fuselage plug and fitting a more powerful F414 engine with a maximum rated thrust of 98kN. The plug was to be inserted just behind the canopy where the area curve had the highest discontinuity (see Area curve in Figure 2). In addition to the plug, ADA studied a bulged canopy to improve area ruling even further. The combined effect was 6 percent lower supersonic drag, which in turn led to a 20 percent improvement in transonic acceleration and 2 percent improvement in maximum speed [4]. The fuselage plug and bulged spine would also provide space for more internal fuel and LRUs.
Figure 2: Canopy optimization study shows a bulged canopy improving the area ruling results in 6% reduction in drag, 20% increase in transonic acceleration and 2% increase in max speed[4].
Similarly, it was observed that there was a sudden kink in the aft bottom of the fuselage in Mk1 as shown in Figure 3. By eliminating this kink and identifying an optimized smoothened aft fuselage, an improvement of 4.9 percent was predicted in the supersonic drag on the aft body region.
Figure 3: Assessment of aft body optimization for supersonic drag reduction. Comparison of Surface Cp contours near the aft region for base configuration and that of optimized aft region at M=1.2, AoA= 3 [cite].
Besides clean configurations, studies were also conducted to decrease the drag of loaded configurations. For example, it was realized early that by replacing the current ‘blunt’ pylons on Mk1 with more aerodynamically shaped pylons, significant drag reduction could be affected in supersonic regimes[18]. Figure 4 shows the inboard pylons before and after the reshaping. These new pylons have already been realized and are expected to even become a part of the MK1/1A platforms. One such pylon for the center fuselage has been put on display in Aero India 2019.
Figure 4: wing inboard pylon: before and after reshaping for better supersonic drag [18].
Credits & Thanks to Indranil & JayS from BR
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