Tejas
Aircrafts already built and projected models to be built. Model designations, tail numbers and dates of first flight are shown.

Technology Demonstrators (TD)

    * TD-1 (KH2001) - 4 Jan 2001 (Retired from Program)
    * TD-2 (KH2002) - 6 June 2002 (Retired from Program)

Prototype Vehicles (PV)

    * PV-1 (KH2003) - 25 November 2003 (Not flown since 13-Jan-10, Airframe Preserved for Kaveri engine  intergration (??))
    * PV-2 (KH2004) - 1 December 2005
    * PV-3 (KH2005) - 1 December 2006 - This is the production variant.
    * PV-4 - Originally planned to be a Naval variant for carrier operations, but now a second production variant.
    * PV-5 (KH-T2009) - Fighter/Trainer Variant

Naval Prototypes (NP)

    * NP-1 - Two-seat Naval variant for carrier operations.
    * NP-2 - Single-seat Naval variant for carrier operations.

Limited Series Production (LSP) aircraft

Currently, 28 LSP series aircraft plus 20 aircraft are on order.

    * LSP-1 (KH2011) - 25 April 2007
    * LSP-2 (KH2012) - 16 June 2008 This is the first LCA fitted with GE-404 IN20 engine.
    * LSP-3 (KH2013) 23 April 2010 The first aircraft to have the Hybrid MMR radar and will be close to the IOC standard.
    * LSP-4 (KH2014) - 2 June 2010 The first aircraft that was flown in the configuration that will be delivered to the Indian Air ForceIn addition to the Hybrid MMR, the aircraft also flew with a functioning Countermeasure Dispensing System
    * LSP-5 - (KH2015) 19 November 2010 In addition to all the systems fitted in LSP-4, it will have night lighting within the cockpit, and an auto-pilot.
    * LSP-6 to LSP-28 - Planned to fly by late 2010.

Planned production variants

    * Tejas Trainer – Two-seat operational conversion trainer for the Indian Air Force.
    * Tejas Navy – Twin- and single-seat carrier-capable variants for the Indian Navy.
    * Tejas Mark 2- Featuring more powerful engine and refined aerodynamics.

The Tejas Mark-2 expected to be developed due to the inability of the Mark-1 to meet the revised Indian Air Staff requirements given out in 2004-6 period,  which required use of more heavier AAM (R-73 to R-77) and ASM and also capability to carry heavy and large bomb load . Tejas MK-2 will have a more powerful engine, refined aerodynamics and replacing other parts to reduce obsolescence according to an IAF spokesman.

The LCA's naval variant would be ready for carrier trials by 2013-14 period and will be powered by  Ge's F-414IN engines  and is slated for deployment on the INS Vikramaditya as well as the Vikrant class aircraft carrier.

Some of features of "Naval LCA Version":

    * Aircraft carrier operation with ski-jump and arrested landing
    * Nose drooped for better cockpit vision
    * Additional aerodynamic features like LEVCON and fore plane to reduce carrier landing speed
    * Maximum take off weight from carrier—12.5 tons[vague]
    * External store carrying capacity from carrier—3.5 tons
    * Strengthened fuselage
    * Stronger undercarriage due to higher sink rate
    * Arrestor hook for deck recovery
    * Fuel dump system




    * LSP-1 (KH2011) - 25 April 2007
    * LSP-2 (KH2012) - 16 June 2008 This is the first LCA fitted with GE-404 IN20 engine.
    * LSP-3  (KH2013) - 23 April 2010 first aircraft to have the MMR
    * LSP-4  (KH2014) CMDS Trails
    * LSP-5 (KH2015) IOC standard with all sensors inculding MMR and HMDS ,Radio aid will be used for Weapons Testing
    * LSP-6 will be used to increase the AOA
    * LSP-7/8 will be given for user trials

Planned production variants

    * Tejas Trainer – Two-seat operational conversion trainer for the Indian Air Force.
    * Tejas Navy – Twin- and single-seat carrier-capable variants for the Indian Navy.



Tejas Mark 2 Revealed @ Aero India 2011
Finally First anticipated Tejas MK-2 was revealed at this years Aero India 2011 ,

Improvements over Tejas MK-1 are As Below


Dimensions of Tejas Mk2

Span  :  8.20m
                                                      Length: 13.70m (Improvement from 13.20m in MK-1)
Height:  4.52m


    * Higher Thrust Engine ( GE F414-GE-INS6 Variant 98 kN up from 85kN)
    * Structural Weight Reduction
    * Aerodynamic Improvements (5 % larger Air Intakes)
    * Upgrade of Flight Control Computer
    * Electronic Warfare Suite (Indo-Israeli "Mayavi Suite")
    * Avionics Upgrade (New Pilot layout)
    * In flight refuelling retractable probe ( MK-1 will have "Fixed"  In flight refuelling probe  )
    * On board oxygen generation system (Already developed and certified)
    * Increased fuel capacity. ( Due to Lengthened Fuselage)