well guess what IAF has already orderred 40 LCA MK1 nad 83 MK1a (with AESA"we already have tested indian LRDE made UTTAM GaA based AESA & in deal with israelies to get EL 2052 AESA" and other imprrovements in weight reduction and with OBOGS & IFR and new lighter but stiffer landing gear)
and when MK2 version comes 120 more to be orderred as for IN it has just stopped LCA from aircraft carrier roles due to troublesome landing gear but has already orderred 40 for shore defnce so get your facts right kid
now we are buying F16blk 70 to fill in numbers and to prepair a two front war and tejas are for replacement of Mig21s only and that means for point defnce meeaning homeland security only not for SEAD/DEAD or precission bombings or attacking enemy postions for that role MKI , jaguars , Mig29, M2K , rafale and F16 & FGFA in future will do the Jib but tejas will never do that job hope you get it this time
View attachment 407567
LCA AF MK2
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The MK2 is an improvement over LCA AF Mk1 with higher thrust engine. This aircraft will have improved survivability, maintainability and obsolescence mitigation. Active Electronically Scanned Array (AESA) Radar, Unified Electronic warfare Suite (UEWS) and On-Board Oxygen Generation System (OBOGS) are some of the state of the art technologies planned to be integrated. The cockpit design has been improved with bigger size, smart Multi function Displays (MFD) and smart Head Up Display (HUD).
The scope of FSED Phase 3 as per project sanction is as follows:-
Design, develop and build two aircraft with
New Engine
Necessary changes in the structure and systems to integrate the new engine
Weight reduction to improve performance
Unified EW Suite (UEWS)
Development of new DFCC, its test facilities and integration
Upgrade/modification/maintenance of test facilities.
Extensive studies were carried out at ADA to make suitable changes in LCA AF Mk2 to address the maintainability issues observed in LCA AF Mk1, improve the systems like fuel, landing gear and brakes, electrical, armament etc. Also a number of new/upgraded systems have been incorporated to make the aircraft more contemporary. As a result, the scope for FSED Phase 3 increased substantially due to extensive changes incorporated to have an improved aircraft with improved performance in all aspects. Important new/ upgrades of systems are listed below:
Introduction of 500mm plug in fuselage
Active Electronically Scanned Array (AESA) radar
On Board Oxygen Generation System (OBOGS)
New Cockpit with larger size smart displays
One Mission Management and Display Computer (MMDC) in place of two Open Architecture Computers
HMDS based on optical sensor
Smart HUD with improved Field of Vision
Higher power Jet Fuel Starter
Servo controlled Airbrake under the command of DFCC control
Pressurized Fuel System
Unified Pylon Interface Computer (UPIC) in place of individual Pylon Interface Boxes
Combined Interrogator Transponder (CIT)
Indigenous Actuators
NVG(Night vision Goggle) compatible lighting
Activities carried out
Presently, the configuration of LCA AF Mk2 has been frozen with all the design improvements and Preliminary Design Review (PDR) has been carried out in June 2014 and detail design is in progress. GE-F414 engine was selected as the higher thrust engine for LCA AF Mk2 and a contract was signed with M/s GE, USA in September 2012. The CDR of alternate engine has been completed. Engine is undergoing final qualification and lifting evaluation tests.
Aerodynamics
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A number of aerodynamics improvements have been carried out to reduce drag and improve performance:
Drag reduction studies have been completed. Canopy reshaping, outer cowl modification, actuator fairing extension and supersonic pylons have resulted in approx 20 counts (8%) drag reduction in supersonic regimes.
Wind Tunnel studies have been completed.
Aero loads computations have been completed
Airframe
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Three doors AAID finalized.
BMI material developed for high temperature applications.
Composite pipelines developed for ECS.
Spine widened for providing accessibility and maintainability.
Pilot step provided for pilot's emergency egress.
SPS bay redesigned to improve maintainability.
Engine
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Aircraft engine bay ventilation scheme has been finalised.
Engine-Airframe Interface Control Diagram (ICD) has been prepared.
Aircraft Qualification Tests have been completed. ASMET (Air c r a ft Simulated Mission Endurance Tests) results are under discussion.
New JFS with higher torque GTSU- 135 is under development.
Mechanical Systems
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Layouts preparation and detail design is in progress.
Feasibility to increase wheel size for increasing the capacity of brake system are in progress.
Trials to offload one hydraulic system to reduce the load on JFS during starting are going on. This will help in cold weather high altitude operations.
Liquid Cooling System configurations, separate for AESA and UEWS have been finalised.
Studies to shift the Air to Air refueling probe to right are in progress to obviate probe coming in Field of View of Head Up Display (HUD).
Integrated Flight Control System
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DFCC: CDR completed Realization st of QT unit by 31 Dec 2016.
Indigenous Actuators: Primary Actuators QT completed, Iron Bird testing completed. Being evaluated on LCA Mk1. Secondary Actuators under development.
Avionics
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Avionics architecture has been finalized.
New cockpit with bigger size (6”x8”) displays has been designed.
Development of new LRUs is in progress.
Avionics will be ready by Dec 2018.
Configuration of Active Phased Array based Unified Electronic Warfare Suite (UEWS) finalised.
The number of elements that can be incorporated with the existing geometry for the Antenna Array unit of AESA Radar has been finalised and performance parameters like range and Effective Radiated Power (ERP) computed.
Night Vision Goggl e (NVG) compatible L E D lights for Navigation lights and Taxi / Landing Lights are being developed. Engineering models have been developed. Performance is being evaluated.
Conformal antenna developed for V/UHF.
Under development Technologies for LCA
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Development of critical advanced technologies for indigenous equipments and systems is in progress. Project sanctions for development of technologies have been given to identified work centers. The following project s has been completed;
DALIA actuators
Indigenous development of high strength titanium alloy Ti-10
Development of Friction Stir Waelding Technology for Aircraft Structures
Aerodynamic studies of performance of LCA wing with Vortex Generators
LCF data generation testing on 15-5 PH steel
Digital Communication Scheme for Tejas
On-going Projects
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The following major projects have been initiated and are in progress
Development of V/UHF Conformal Antenna
Development of Digital Audio Control System (DACS)
Digital Liquid Oxygen (LOX) Indicators/ Transmitters
Development of improved RAM
Fatigue data generation on AA 7010 Aluminium alloy
Development of Zn-Ni plating as an alternate to cadmium plating
Development of high temperature beta titanium alloy DMR 700
Development of On-Board Oxygen Generation System (OBOGS)
Development of Cabin Shut Off Valve (CBSOV) of ECS,
Development of AMAGB Bearings
Advanced Subminiature Telemetry System,
Jet Fuel Starter (JFS) Mark 2
Development of MEMS based Pressure Transducers and temperature sensors for Hydraulics system.(Ps all this data shown is of late 2014 rest specualte yourself )