ADA Tejas (LCA) News and Discussions

Which role suits LCA 'Tejas' more than others from following options?

  • Interceptor-Defend Skies from Intruders.

    Votes: 342 51.3%
  • Airsuperiority-Complete control of the skies.

    Votes: 17 2.5%
  • Strike-Attack deep into enemy zone.

    Votes: 24 3.6%
  • Multirole-Perform multiple roles.

    Votes: 284 42.6%

  • Total voters
    667
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harish.kaks

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Hi , can some body tell me When Tejas will get IOC-2, As the LSP-8 has taken flight more than a month back and it was as per the expectations. Can we expect that with in a month or two?
 

Kunal Biswas

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3-6 months since LSP-8 made its flight..

Hi , can some body tell me When Tejas will get IOC-2, As the LSP-8 has taken flight more than a month back and it was as per the expectations. Can we expect that with in a month or two?
 

ersakthivel

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The two basic reasons for the outstanding performance of F-16XL were the large wing area and 3* canted tail which caused the thrustline to go below the C of G of the aircraft there by giving it a nose up thrust vector obviating the need for elevators to compensate for strong nose down pitch moment of the wing in flight at high speeds which is hall mark of such cranked delta planforms. It was for this reason that F-16XL was the first ac in the world to supercruise. This low thrustline also gives outstanding take off performance as it effectively adds to the elevator authority.
Having the thrust line right below the Cg will remedy this problem to some extent, But will it completely solve it?

Only detailed wind tunnel modelling will clarify these things.

Even though it may result in a force couple to lift the fighter, the continued presence of CG in front of the CP will give a nose down momentum which will act against the pilot's effort to obtain higher AOAs quickly.

In RSS fighters the presence of CG behind the Center of Lift or pressure will aid the pilot's effort to attain higher AOA in all flight profiles.

More in number controlling surfaces assist in maneuvering quickly coupled with the higher agility of the RSS airframe.


The Mirage 2000 features a low-set thin delta wing with cambered section, 58 degrees leading-edge sweep and moderately blended root; area-ruled; two small canard wings, fixed, placed just behind the air intakes. The flight controls on the wings are: four elevons (+15/−30°), four slats.

In the 1982 summer, at the Farnborough Airshow, this machine displayed not only excellent handling capabilities, but also a full control at 204 km/h and 26 degree angle of attack.

This was totally unexpected in a delta-wing fighter, and proved how CCD controls were capable of overcoming the delta wing shortcomings related to poor low-speed control, while retaining the advantages, such as low-drag, low radar cross section, ideal high speed aerodynamics and simplicity, provided by the absence of horizontal tail surfaces


Its neutral point is in front of its center of gravity, giving the fighter relaxed stability to enhance maneuverability. It incorporated negative stability and fly-by-wire controls with four analog computers. An airbrake is fitted above and below each wing in an arrangement very similar to that of the Mirage III. A noticeably taller tailfin allows the pilot to retain control at higher angles of attack, assisted by the small strakes mounted along each air intake.
The mirage-200 has low enough thrust line, still it's designers went for RSS. WHY?
 
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ersakthivel

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http://164.100.24.208/ls/CommitteeR/Defence/17threport.pdf

The above PDF link holds the following report,

STANDING COMMITTEE ON DEFENCE
(2006-2007)

(FOURTEENTH LOK SABHA)
MINISTRY OF DEFENCE
IN-DEPTH STUDY AND CRITICAL REVIEW OF
HINDUSTAN AERONAUTICS LIMITED (HAL)

SEVENTEENTH REPORT
Pages-41 to 45 of this report details all the important milestones in time periods for the tejas project.It also details what is the reason for the missing deadline in detail


"¢ Redesign of Composite Wings to cater for Weapon definition changes
specified by Indian Air Force (IAF) during Jan 04.
the page number -43 of the above report states many true facts opposed to loads of BS heaped on LCA Tejas by many people all over the net calling it as 40 years old, and 30 years old obsolete project.

Exposing the BS being heaped on LCA tejas as a project failed to meet the original ASR of 1986. Infact it's weapon definition was revised by IAF as late as 2004 resulting in the redesign of it's wings leading to more weight and further delay.

ANd it explicitly states that wings were redesigned to cater to the weapon definition changes specified by the IAF during Jan 2004.



ADA has provided a detailed cost breakdown. The LCA project began in 1983 (the name Tejas only came later) with a preliminary allocation of Rs 560 crore for "feasibility studies and project definition". Subramanyam complains that accusations of cost overruns stem from the misperception that Rs 560 crore was the entire budget for developing the Tejas. In fact, this was merely for defining the project and creating the infrastructure needed for designing, building, testing and certifying a fighter.

Only after a decade of infrastructure building did the design work start, when the MoD sanctioned Rs 2188 crore in 1993 (which included the initial Rs 560 crore). This allocation was to fund the building of two "technology demonstrator" Tejas fighters.


from here – http://ajaishukla.blogspot.in/2011/02/cost-of-tejas-myth-and-reality.html
http://www.dnaindia.com/bangalore/1399182/report-tejas-cockpit-will-be-a-pilot-s-delight
the above link details how the cockpit of tejas was designed with intensive interaction with IAF test pilots.

So till 2004 IAF's newer demands were accepted by ADA to include much more demanding performance specs. But concealing all these hard facts some fake experts still conveniently argue that LCA is yet to meet the original 1986 ASR!!!!!!!!


This report was mentioned by the defenders of the LCA TEJAS project in the following interesting blog,
http://tkstales.wordpress.com/2012/05/11/the-tejas-debate-continues,
when professsor PRODUYT DAS who wrote an overtly critical article on Tejas on Vayu is being countered with authentic facts in the above blog,

Infact the blog,

http://tkstales.wordpress.com/2012/05/11/the-tejas-debate-continues/

is a must read for all people who want to know the true story behind the challenging period which lies behind the development of Tejas.
Light Combat Aircraft (LCA) (Tejas)
LCA is a light weight, highly agile, multi-role supersonic fighter. It has
quadruplex digital fly-by-wire Flight Control System (FCS) with associated
advanced flight control laws. The aircraft with delta wing is designed for 'air
combat' and 'offensive air support' with 'reconnaissance' and 'anti-ship' as its
secondary roles. Extensive use of advanced composites in the airframe gives
a high strength to weight ratio, long fatigue life and low radar signatures.
Aeronautical Development Agency is the designated project manager for the
development of LCA.

The project definition phase of the programme was launched in 1987. In 1991,
Full Scale Engineering Development (FSED – Phase 1) was launched at a
project cost of Rs. 2188 Cr involving design, production of 2 technology
demonstrators, 2 prototype vehicles, one static test specimen and associated
ground and limited flight tests. This work was completed in 2005.

In 1999, FSED-Phase 2 was launched at a project cost of Rs. 3302 Cr involving
3 additional prototype vehicles (including a trainer variant) and production of 8
aircraft under limited series production.
Currently, two TDs and two prototype vehicles (PVs) are undergoing flight
evaluation and a cumulative of 567 flights have been completed as of end Oct
06 covering a flight envelope of 1.4 Mach and 15 Km altitude. The trainer
variant : is under build and is expected to be ready for engine ground run by
Dec 2006. Further a programme for design and development of naval variant of
LCA has been launched subsequently in 2003 at a project cost of Rs.949 Cr
involving development of two prototypes.

It is expected that Initial Operation Clearance (IOC) for the LCA is achievable in
2008. To expedite achieving IOC, monthly review of the programme by a joint
committee comprising of Chairman, HAL, Deputy Chief of Air Staff and Chief
Controller(R&D) is being carried out.

The number of aircraft requirement projected by Services is 220 aircraft .
LSP of 8 aircraft has been taken up against MOU signed with ADA and the 1
st
aircraft is expected to be delivered in 2006-07. Further a contract for supply of
20 aircraft at a value of Rs. 2701.70 Cr has been concluded with IAF in Mar
2006 . These 20 aircraft are scheduled for delivery during 2010 – 2012.

5.3 During examination of Demands for Grants (2004-05), the Committee were
informed that initial operational clearance of Light Combat Aircraft (LCA) is planned by
2006 and final operational clearance by 2008. In Action Taken Reply to the same
Report, the Ministry furnished revised schedule stating that initial operational
clearance of LCA would be over by March 2007 and final operational clearance by
2009. During examination of Demands for Grants (2005-06), the Committee were
informed that initial operational clearance would be over by the year 2010. In Action
Taken Reply to this Report, the Ministry informed that initial operational clearance is
planned by 2008 and final operational configuration by 2010.
5.4 The Ministry has furnished reasons for delay in induction of Light Combat
Aircraft (LCA) as under:
Reasons for delay in Full Scale Engineering Development (FSED) of LCA are
"¢ Technology difficulties
"¢ Non availability of systems design & high safety standards

"¢ Foreign Exchange crunch of 1991
"¢ Revision of development strategy by increasing indigenous content in
aircraft & ground facilities
"¢ Sanctions imposed by USA in 1998
"¢ Redesign of Composite Wings to cater for Weapon definition changes
specified by Indian Air Force (IAF) during Jan 04.
"¢ Indigenous development & integration of Obsolescence-free Open
Architecture Avionics Systems
"¢ Integration of interim Electronic Warfare (EW) equipment specified by
IAF during 2005
"¢ Extensive on ground evaluation, simulation & testing of indigenous
equipment, systems, software & aircraft.
"¢ Extensive Independent Verification & Validation (IV & V) of complex
airborne software to ensure fight safety
"¢ Co-ordination & integration effort by many work centres to type certify
indigenous equipment systems.
The present status of this project is as given below:
"¢ Flight Test Phase (FTP) of FSED Phase 2 is in progress. As on 30 Nov 06,
572 Flight Test (313 Hrs 24 Min) have been completed utilising 2
Technology Demonstrators and 2 Prototype Vehicles. Handling Quality
(HQ) of LCA has been adjudged as "Very Good" by 11 Test Pilots of IAF &
Indian Navy.
"¢ Third Tejas (Prototype Vehicle) has completed High Speed Taxi Trials
(HSTT) and is ready for its maiden flight. Development of 2 Trainer Variants
is in progress and the first Trainer is expected to fly in 2007. Integration of
IAF specified Sensors & Weapons is progressing satisfactorily

"¢ During FSED Phase 2, manufacture of 8 limited Series Production (LSP)
standard Tejas aircraft and establishment of 8 aircraft per annum production
facility has been initiated concurrently to gain time advantage during
Production Phase. Four Tejas (LSP) aircraft are expected to join Flight test
phase during 2007.
"¢ Confidence in LCA as a flying machine is high and IAF has placed
procurement order for 20 LCA with the manufacturing agency (M/s
Hindustan Aeronautics Ltd.) for inducting one LCA Squadron into
operational service. Production Phase of LCA has also been initiated
concurrently with FSED Phase to gain time advantage.
"¢ There was no cost over-run in LCA FSED Phase 1 programme. As on
date, there is no cost over-run in LCA FSED Phase 2 Programme also.
43
"¢ Production Standard LCA comprises 65% of indigenous equipment (Line
Replaceable Units

Kaveri Engine:
HAL is providing manufacturing support for fabricating certain modules
of the prototypes of Kaveri being designed by GTRE. Following Seven Modules
of Engine have been supplied for the prototypes
Oil Tank (Titanium)
Jet Pipe
Turbine
Exhaust
Rotational System Internal Flow
(RSIF)
Convergent Divergent Nozzle
Fan
Apart from manufacturing of modules, HAL, Engine Division is also supporting
GTRE in Assembly of LP Turbine Disc, Integration of Jet Pipe and
Convergent-Divergent Nozzle and Shroud Segments on Turbine Casing."
5.5 About the status on Kaveri Engine, the Ministry has stated as under:
"¢ Currently, 4 Engines are running on test bed at the Gas Turbine Research
Establishment (GTRE), Bangalore, while 2 engines are being manufactured.
These engines fall short of design intent by a small margin. However, their
performance may be adequate to fly the Light Combat Aircraft over a limited
flight envelope. Therefore reliability and safety tests are being carried out to
demonstrate compliance to the strictest standards in this direction.
Simultaneously efforts are being made to improve thrust and reduce weight.
"¢ Request for Proposal (RFP) to international engine house to partner GTRE
and HAL to meet full performance requirement in accelerated timeframe for
development, test and evaluation and production is under process.

5.6 Regarding capabilities of HAL in development and manufacturing engines for
Aircraft, Secretary (Defence Production) further apprised the Committee during Oral
evidence as given below:
"As regards engine manufacturing or indigenous engine development, we have
been at it for quite some time but we have not reached 100 per cent success so
far in Kaveri engine. Once we master the technology of engine, whether it is
Kaveri engine or any variant of that, then it will be possible to be able to make
other variants of those engines. DRDO, of course, is more competent to
answer the questions as to why we have not been able to do it; what are the
difficulties that we are facing; and how we are resolving those difficulties. Once
we achieve it, we can see how its capacity can be created to be able to do its
variants also."
445.7 While replying to a query of a Member in regard to delay in prototype designs of
LCA and flight testing, Chairman (HAL) informed the Committee during Oral evidence:

"We first do the design. Then, we have to construct the aircraft like
constructing a house. Then, you put all the equipment. In fact, in this specific
project, we benchmarked ourselves this prototype design, and prototype flying
was done in the fastest possible time we could imagine. From the time we
finished our design, we cut the metal into the first prototype in just 18 months'
time. In think, it was the world record as far as design and development are
concerned in the Intermediate Jet Trainer. The process is, you design the
aircraft; construct one prototype; start flying that; and in the second prototype,
you use the same tooling what was used for the first prototype, and then you
start flying. In fact, we were very pleased that this project has been done so
fast.
The second question was on the selection of the engine. When the design was
conceptualized we took stock of what engines are available in the market.
They were all in the 1500 kg class. We started our prototype development with
what was existing but ultimately it emerged because of the requirements of the
specification that we needed an engine with much higher power. That was how
we went ahead."
5.8 About the present status of LCA and its induction plan in Air Force, Secretary
(DRDO) further informed the Committee during Oral evidence:
"In the earlier presentation, I had said very clearly that we have taken up the
policy decision that the first two squadrons of LCA will go with General Electric
engine, with which it is already flying.
It would be covered by the end of 11
th
plan. By the time we have built two
squadrons, we would know the capability of Kavery for a repacelment. The first
squadrons means 40 aircraft with GE engine. We can think of a Kaveri type of
engine only beyond 40 aircraft."

- UNQUOTE
 
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ersakthivel

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here is what P Rajkumar (IAF) who was involved with the LCA says -

quote -

Philip Rajkumar on May 1, 2012 at 6:01 am said:

philip rajkumar

I worked in the LCA project for nine years from 17 Sep 1994 to 31 Aug 2003 (actually 17 days short of nine years!). I was deputed to ADA by the IAF to oversee the flight test programme of the Technology Demonstration phase of the project. Having been on both sides of the fence i have a few points to make.

1. Development of a capable aeronautical industry is a small step by small step evolutionary process.Infrastructure and skill sets of the work force have to be built up over decades with considerable effort. All this requires investment of money and managerial resources.

Mainly due to financial constraints and lack of vision in the IAF, HAL and the GOI we allowed capabilities built up during the Marut and Kiran programmes to atrophy. While the world leapt ahead with several technological innovations like fly by wire,digital avionics and use of composites for structures HAL did not run a single research programme because it was not the practice to do research unless it was linked to a specicific project.


2.The LCA project is where it is today thanks to one man-Dr VS Arunachalam who as the SA to RM in 1985 had the gumption and clout to go to the GOI and convince them that India could build a fourth generation fighter. It was a leap of faith no doubt.

3. HAL feels wronged about being asked to play second fiddle to ADA. This pique continues to hurt the project even today.

4. Without help from Dassault of France,BAE Systems UK, Lockheed Martin of the USA and Alenia of Italy we would not have succeeded in developing the fly by wire flight control system,glass cockpit,and composite structures for the two TD aircraft.

5. So far the flight safety record of the programme has been good. I pray every day that it remains that way. The loss of an aircraft early in the programme would have surely lead to its closure.


6.All pilots who have flown the aircraft say its handling qualities are very good. It means it is easy to fly and perform the mission.

7.It needs to be put into IAF sevice as soon as possible to gain more experience to iron out bugs which are sure to show up during operational use.

8.Programme management could have been better. IAF is to blame for washing its hands off the project for 20 years from 1986-2006. A management team was put in place at ADA in 2007.

9.Dr Kota Harinarayana and all those who have worked and continue to work have done so with great sincerity and dedication.

10.Indian aeronautics has benefitted immensely from the programme. It is a topic for separate research.

11. It was a rare privilege for me to have been given an opportunity to contribute to the programme by setting up the National Flight Test Centre and putting place a methodology of work which has ensured safety so far.

12. According to me the project can be called a complete success only when the aircraft sees squadron service for a couple of decades. We will have to wait but it is progressing on the right lines and we as a nation have nothing to be ashamed of.
 
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ersakthivel

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Lca is already operational. It has cleared all the test points that are required for IOC means , it is becoming operational. LSP-7 and LSP-8 are closest to freeze production design.The GE-404 IN engine is fully capable of meeting all the operational needes of LCA mk-1 with a thrust to weight ratio of 1.07 which is comparable to most of the modern fighters. Some fighters like MIG-29 have a Thrust to weight ratio of 1.2 and more. it is because they have smaller wings meaning lesser empty weight.

Since LCA has bigger wings weighing more it has a TWR of 1.07. But bigger cranked wings will generate more efficient lift to drag ratio like that of F-16 XL which will have it's own advantage.As explained below ,

http://www.airforcemag.com/MagazineArchive/Pages/1983/November 1983/1183f16xl.aspx

To say that Hillaker's design team achieved its objectives is an understatement. Example: For an air-to-surface mission, the F-16XL can carry twice the payload of the F-16A up to forty-four percent farther, and do it without external fuel tanks while carrying four AMRAAM (Advanced Medium-Range Air-to-Air Missiles) and two Sidewinder AIM-9 infrared missiles. With equal payload/weapons and external fuel, the mission radius can be nearly doubled. When configured for a pure air-to-air mission, an F-6XL with four AMRAAMs and two AIM-9s can go forty-five percent farther than an F-16A and can do so while conducting a combat action that is equal to thirty percent of its internal fuel.


As for penetration and survivability, the F-16XL can dash supersonically with a load of bombs at either high or low altitude. It can climb at high rates with the bombs aboard. And it has a speed advantage of up to eighty-three knots over the F-16A at sea level at military power setting and 311 knots on afterburner at altitude while carrying a bomb load.


Two additional capabilities of the F-16XL contribute to survivability. First is improved instantaneous maneuver ability coupled with greatly expanded flight operating limits (with bombs), and second is reduced radar signature resulting from the configuration shaping.


Importance of High Turn Rate


For a decade and a half, many fighter tacticians have stressed the paramount importance of being able to sustain a high turn rate at high Gs. The rationale was that with such a capability, enemy aircraft that cannot equal or better the sustained turn rate at high Gs could not get off a killing shot with guns or missiles.


With developments in missiles that can engage at all aspects, and as a result of having evaluated Israeli successes in combat, the tacticians are now leaning toward the driving need for quick, high-G turns to get a "first-shot, quick-kill" capability before the adversary is able to launch his missiles. This the F-16XL can do. Harry Hillaker says it can attain five Gs in 0.8 seconds, on the way to nine Gs in just a bit more time. That's half the time required for the F-16A, which in turn is less than half the time required for the F-4. The speed loss to achieve five Gs is likewise half that of the F-16A.


All of these apparent miracles seem to violate the laws of aerodynamics by achieving greater range, payload, maneuverability, and survivability. Instead, they are achieved by inspired design, much wind-tunnel testing of shapes, exploitation of advanced technologies, and freedom from the normal contract constraints.


The inspired design mates a "cranked-arrow" wing to a fifty-six inch longer fuselage. The cranked-arrow design retains the advantages of delta wings for high-speed flight, but overcomes all of the disadvantages by having its aft portion less highly swept than the forward section. It thus retains excellent low-speed characteristics and minimizes the trim drag penalties of a tailless delta.


Although the wing area is more than double that of the standard F-16 (633square feet vs. 300 square feet), the drag is actually reduced. The skin friction drag that is a function of the increased wetted (skin surface) area is increased, but the other components of drag (wave, interference, and trim) that are a function of the configuration shape and arrangement are lower so that the "clean airplane" drag is slightly lower during level flight, and forty percent lower when bombs and missiles are added. And although the thrust-to-weight (T/W) ratio is lower due to the increased weight, the excess thrust is greater because the drag is lower – and excess thrust is what counts.


The larger yet more efficient wing provides a larger area for external stores carriage. At the same time, the wing's internal volume and the lengthened fuselage enable the XL to carry more than eighty percent more fuel internally. That permits an advantageous tradeoff between weapons carried and external fuel tanks.


Through cooperation with NASA, more than 3,600 hours of wind-tunnel testing refined the shapes that Harry Hillaker and his designers conceived. More than 150 shapes were tried, with the optimum design now flying on the two aircraft at Edwards.


As an additional technology, the XL's wing skins are composed of an advanced graphite composite material that has a better strength-to-weight ratio than aluminum, is easier to form to the compound wing contours, and has higher stiffness to reduce undesirable flexibility effec




[http://www.airforcemag.com/MagazineArchive/Pages/1983/November 1983/1183f16xl.aspx

MK-2 is being developed according to the needs of the Navy which wants a bigger 100 plus Kn GE-414-IN S 6 engine for the naval version which needs to be strengthened more resulting in a heavier fighter, which will need more powerful engine.

The IAF seeing the benefit of the higher power engine for it's lesser weighing air force version is also going for mk-2 in higer numbers, which is just natural , since the Airforce version of Tejas MK-2 won't need the extra strengthening of the naval version(which needs to impact the carrier deck with higher force). So the airforce version with GE-414-IN S6 engine will have 40 percent more improved performance in all flight regimes along with increased weapon load and range.

The Kaveri engine has been delinked from tejas. because IAF doesnot want the delay in Kaveri to impact it's induction timeframe of tejas. But if GTRE succeeds in developing a better K-10 ,which will weigh lesser ,with 100 plus kn thrust . All tejas mk-1 and mk-2 which will need an engine change after a decade(since a jet engine wears out in a decade) those K-10 GTRE engine can be placed on them.
Even If k-10 doesnot come through there is no reason to worry. because considering th strategic ties US won't stop GE engine exports to India in a hurry.[/QUOTE][/QUOTE]

Anyone following the correct news on LCA project can easily know this is the present status of the program.The current LCA mk-1 itself is good enough to most of the jobs IAF ASR demanded from it.it has a bigger radar than the current Grippen C/D version doing service in the Sweedish airforce.And can launch python, R-73 , or any other type of air to air missile that can be launched by Su-30 MKi. It can do well if it is combined in mixed group operations with Su-30 MkI, as recently demonstrated by IAF vs USAF exercise. The bigger radar of Su-30 mki can be used to guide the longer range BVR missiles fired from Tejas mk-1 Tejas can fly farther ahead of the Su-30 mki undetected , due it's lower cumulative RCS than su-30 MKI. But it can extend the range of any BVr missile in IAF if it teams up with su-30 MKi in this fashion.

Currently no fighter in the IAF has a radar as modern as that of tejas mk-1's 120 km detection and tracking range.
tejas mk-1 has the lowest clean config RCS among all the planes in IAF.
 
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Ganesh2691

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LCA-Tejas has completed 2161 Test Flights Successfully. (14-May-2013).

(TD1-233,TD2-305,PV1-242,PV2-222,PV3-364,LSP1-74,LSP2-267,PV5-36,LSP3-130,LSP4-74,LSP5-172,LSP7-34,NP1-4,LSP8-4)
 

roma

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Lca is already operational. It has cleared all the test points that are required for IOC means , it is becoming operational. LSP-7 and LSP-8 are closest to freeze production design.........
the following is a simpleton question from a person who does not know anything much about LCA tejas:-

"can this forum-thread please help me confirm that LCA tejas MK 1 ( initial version ) is now indeed operational ( as someone has told me ) and if possible in which Air squadron and date of becoming operational"

- i would like to record this in my india vision and timeline record for the benefit of all of us and visitors ... many thanks in advance for your effort in replying
 
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Kunal Biswas

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The First of Tejas are Inducted in IAF with IOC-1 certification, The Induction took place Jan 10, 2011 ..


India's Light Combat Aircraft, Tejas, handed over to Indian Air Force by Defence Minister A K Antony after Initial Operational Clearance in Bangalore. This catapults India to a select club of nations that built a fighter plane from scratch.

AIR Correspondent reports that HAL will continue to upgrade the indigenous fighter as the Indian Air Force plans to induct close to 200 LCAs and 20 twin seater trainer versions in the long run. The historic first squadron will be stationed at Sulur near Coimbatore.

The second LCA squadron will be stationed at Kayathir near Tuticorin, where the IAF is developing a new fighter base. The mark II version of the LCA with a more powerful engine, better aerodynamics and advance avionics is also under development. The naval version of the LCA, to be used in aircraft carriers, is also under development..
Read more: India’s First LCA Tejas Inducted in IAF | Aviation & Air Force News at DefenceTalk

================================

At present the Tejas are not in full squadron strength number, Once it will be done then Tejas will be inducted into the 45th squadron, the Flying Daggers




this is a simpleton question from a person who does not know anything much about LCA tejas
can this forum-thread please help me confirm that LCA tejas MK 1 ( initial version ) is now indeed operational ( as someone has told me ) and if possible in which Air squadron and date of becoming operational - i would like to record this in my india vision and timeline record for the benefit of all of us and visitors ... many thanks in advance for your effort in replying
 
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roma

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I was about to get a bit proud of our tejas until i saw this below ( taken off https://www.defenseindustrydaily.co...10-but-foreign-help-sought-with-engine-01901/ ...and dated onlyone month back ! )


LCA Tejas: An Indian Fighter – With Foreign Help
Apr 23, 2013 15:55 UTC by Defense Industry Daily staff DII
Latest update [?]

A critical view –
from Pakistan
(click for video)

April 21/13: Tejas a lemon? The Sunday Standard reports external link that the Tejas is much farther away from viability than anyone is admitting, and says that DRDO's notional stealth AMCA (Advanced Medium Combat Aircraft) has been put on hold until the LCA project can be made to work. A stealth FGFA/SU-50 is already in co-development with Russia, so AMCA's value is unclear anyway. With respect to the Tejas LCA, the Sunday Standard's unnamed sources say:

"The plane cannot fly on its own. It needs a lifeline in the form of support and monitoring of its systems from the ground by technicians"¦. The common man thinks the plane is doing fine, its engine sounds great and the manoeuvres are perfect. But those flying and weapons firing displays are done with ground monitoring and support. The plane is still not ready to flying on its own""¦. the sources noted that LCA was grounded for three months between September and December 2012 following problems with its landing gear. "Normally, a combat plane is ready for its next sortie following a 30-minute [servicing]. In the case of LCA, after a single sortie of about an hour or so, it needs three days of servicing before it can go for its next sortie," they said."

These revelations come against a backdrop of pressure from India's defense minister Antony and India's government to buy designed-in-India items unless there's no other choice. He's selling changes to external link India's Defence Procurement Policy as an anti-corruption effort – but what do you call spending billions of dollars on politically-allied state organizations, who don't deliver on the critical defense projects assigned to them, and never pay any serious penalties for it? Their competitors in China and Pakistan are consistently faster and often better – while doing a better job developing their industries. See also India PIB external link.

March 20/13: More delays. A Parliamentary reply confirms the obvious, formally extending the scheduled end of the LCA's Phase 2 Full Scale Engineering Development from December 2012 to March 2015.

The IAF has ordered 20 fighters in "Initial Operational Clearance" (January 2011) status, and another 20 in "Full Operational Clearance" (i.e. combat-ready) configuration. Full Operational Clearance is now expected in December 2014. PTI, via Zee News external link | India MoD external link.
{^}
The above update is a recent abstract from our full article, itself part of our subscription offering. Keep reading to know more.
LCA Tejas Underside
Tejas LCA
(click to view full)

India's Light Combat Aircraft program is meant to boost its aviation industry, but it must also solve a pressing military problem. The IAF's fighter strength has been declining as the MiG-21s that form the bulk of its fleet are lost in crashes, or retired due to age and wear. Most of India's other Cold War vintage aircraft face similar problems.

In response, some MiG-21s have been modernized to MiG-21 'Bison' configuration, and other current fighter types are undergoing modernization programs of their own. The IAF's hope is that they can maintain an adequate force until the multi-billion dollar 126+ plane MMRCA competition delivers replacements, and more SU-30MKIs arrive from HAL. Which still leaves India without an affordable fighter solution. MMRCA can replace some of India's mid-range fighters, but what about the MiG-21s? The MiG-21 Bison program adds years of life to those airframes, but even so, they're likely to be gone by 2020.

That's why India's own Tejas Light Combat Aircraft (LCA) project is so important to the IAF's future prospects. It's also why India's rigid domestic-only policies are gradually being relaxed, in order to field an operational and competitive aircraft. Even with that help, the program's delays are a growing problem for the IAF. Meanwhile, the west's near-abandonment of the global lightweight fighter market opens an opportunity, if India can seize it with a compelling and timely product.
Displaying 633 of 16,752 words (a
 

p2prada

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the following is a simpleton question from a person who does not know anything much about LCA tejas:-

"can this forum-thread please help me confirm that LCA tejas MK 1 ( initial version ) is now indeed operational ( as someone has told me ) and if possible in which Air squadron and date of becoming operational"

- i would like to record this in my india vision and timeline record for the benefit of all of us and visitors ... many thanks in advance for your effort in replying
LSP-8 was the first aircraft to achieve downgraded IOC specs. LSP-6 is expected to achieve IOC's actual specs. As of today LCA flies at the same level as a Hawk trainer, which is enough for early inductions.

Either at the end of this year or early next year, HAL will deliver the first two Serial Production models called SP-1 and SP-2 to the IAF and a squadron will be raised with the induction of 20 SP models. The squadron will be the No 45 Flying Daggers and the pilots will convert from Mig-21bis to LCA.

Date won't be available until LCA's deliveries start. It should take two to three years after that, so in the 2015-16 period.
 

roma

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LSP-8 was the first aircraft to achieve downgraded IOC specs. LSP-6 is expected to achieve IOC's actual specs. As of today LCA flies at the same level as a Hawk trainer, which is enough for early inductions.
Either at the end of this year or early next year, HAL will deliver the first two Serial Production models called SP-1 and SP-2 to the IAF and a squadron will be raised with the induction of 20 SP models. The squadron will be the No 45 Flying Daggers and the pilots will convert from Mig-21bis to LCA.
Date won't be available until LCA's deliveries start. It should take two to three years after that, so in the 2015-16 period.
many thanks to your good-self and Mr Kunal for good info Sirs, - as a non-expert i would merely ask if the members of this forum are satisfied with the time-frame as quoted above - not that anythng mush can be done about it but is it in keeping with most international standards .

the reason i am asking is that it seems to me (again being aware im not an expert ) that we took our own sweet time to rectify the "flying coffin" Mig 21 syndrome and when we do have a good replacement we take our time abaaout getting it verified and into service - not that im asking for any of the commissioning processes to be lessened in thier rigour, but we seem to be in no hurry to replace the Mig21 which WAS great, but is a 1970's era machine - and this being 2013 we are in no hurry ?
 

Kunal Biswas

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That is because this Out Government is not very keen to have a developed Defense Industry so does IAF for 100% foreign hardware..

Tejas, was neglected from beginning so does there scientist working for it ( Like Infrastructure with snakes and old warehouse given for research in some isolated part of the county ), Tejas start flying only a decade ago, Its only really started a decade ago before that everything was conceptional, If IAF wanted it could have induct Tejas earlier with Russian engines and radars to avoid silly MIG-21 crashed and loss of invaluable Pilots ( Which IAF no reserves for and it knows ), Things are linked with corruption and lack of vision..

but we seem to be in no hurry to replace the Mig21 which WAS great, but is a 1970's era machine - and this being 2013 we are in no hurry ?
 

ersakthivel

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I was about to get a bit proud of our tejas until i saw this below ( taken off https://www.defenseindustrydaily.co...10-but-foreign-help-sought-with-engine-01901/ ...and dated onlyone month back ! )


LCA Tejas: An Indian Fighter – With Foreign Help
Apr 23, 2013 15:55 UTC by Defense Industry Daily staff DII
Latest update [?]

A critical view –
from Pakistan
(click for video)

April 21/13: Tejas a lemon? The Sunday Standard reports external link that the Tejas is much farther away from viability than anyone is admitting, and says that DRDO's notional stealth AMCA (Advanced Medium Combat Aircraft) has been put on hold until the LCA project can be made to work. A stealth FGFA/SU-50 is already in co-development with Russia, so AMCA's value is unclear anyway. With respect to the Tejas LCA, the Sunday Standard's unnamed sources say:


The above passage proves this report is anything based on truth.

Reasons ,
IOC means the plane has behaved as predicted with minor modifications as per the design through the partially tested flight envelope. That is the meaning of the term IOC. Since the plane met all test points specified for it , IT WILL BEHAVE IN THE SAME WAY AND VALIDATE ALL THE REMAINING TEST POINTS , and complete FOC .

All fighter programs follow the same procedure.All test points are divided in two sections,
1.before IOC,
2.IOC to FOC.
Extreme performance specs like high AOA testing and testing the fighter at the edge of it's performance envelope like
1. top speeds at high altitude,
2.spin testing to study the departure predictions i.e stall testing
3. Long range air to air roles ,
4. High G turns testing the fighter at the edge of it's G attaining capacity,
are always carried out after the IOC , and once these testing are completed and FBW is validated , FOC is given.

You may ask why? the reason is first you test the fighter within 70 to 80 percent of it's operating capability to check whether your design specs are properly translated in production version.If there are any shortcomings found , then alter the fighter to achieve the goals. Once it completes the 80 percent of the operating capacity , then it means that your design is working as you predicted in software simulations and wind tunnel testing. So it will continue to work in the same way you predicted in the rest of the 30 percent untested flight envelope.

World over this is the norm in all test flight programs.

If you want a real world analogy , lets say ferrari designs and builds a sports car that can reach 0 to 400 km speeds in 6 seconds.And will remain in control with say 200 km per hour speeds while cornering bends with certain angle.

The same design process will give some intermediate targets as well, like-- 0 to 200 in 3 seconds, 0 to 300 in 4.5 seconds

How will they proceed wit the testing?
there are two ways of testing it.

1. They will just take the first model and press the pedal to the bottom to check whether it reaches reach 0 to 400 km per hour in 6 sec,
And ask the driver to throw the car around at 200 km per hour at the first bend in the road he sees .

or,

2.They will first test whether the car reach 0 to 200 in 3 seconds ,
and if the t target is not achieved ,
then they will analyze the problem and solve them by design modifications,
and test it again to satisfy themselves whether it reaches those targets, before proceeding to next test point of 0 to 300 km per hour and , 0 to 400 km per hour.

Before testing whether it corners solidly at 200 km per hour, they will test it's cornering ability at say 70 km hour and satisfy themselves, then 150 km per hour and if there are any problems modify the suspension and weight distribution and validate it. And then finally they go for 200 km per hour at cornering.


What do you think a rational Eng Design team will do? A test flight is thousand times more complex than driving a new ferrari on the road. it involves the pilot's life as well. So with meager resources available to ADA , what it will do?

Another wrong assumption is FGFA will do all AMCA can. How did the reporter found this out? FGFA will have inferior stealth specs even compared to the much lampooned F-35.

AMCA wil be many times more stealthier than FGFA.And the ASR forming for AMCA is going on for ten years from 2002 to 2012.

And just now it's specs were freezed and funds released for FSED phase.There are two design teams working separately on AMCA and LCA. So no one will pluck members from AMCA team and plant them midway in LCA mk-2 team.

And the reason for the delay in LCA mk-1's IOC is slow production rate of LSPs by HAL, which was due to the time taken to validate minor design changes, not due to lack of design effort as few people mike to mislead others into believing.
"The plane cannot fly on its own. It needs a lifeline in the form of support and monitoring of its systems from the ground by technicians"¦. The common man thinks the plane is doing fine, its engine sounds great and the manoeuvres are perfect. But those flying and weapons firing displays are done with ground monitoring and support. The plane is still not ready to flying on its own""¦. the sources noted that LCA was grounded for three months between September and December 2012 following problems with its landing gear. "Normally, a combat plane is ready for its next sortie following a 30-minute [servicing]. In the case of LCA, after a single sortie of about an hour or so, it needs three days of servicing before it can go for its next sortie," they said."

This is the most dumbheaded part of the report. Plane flies on it's own. many of it's flight parameters are monitored and relayed to ground via telemetry systems on board Tejas,to check whether all subsystems perform as per design specs.

And this is the reason for flight test program. if the plane needs no monitoring , How will it fly? The TEJAS LSP-7 took part in IORNFIST exercise and did missile firing and ground bombing far away from the ground handling canter in bangalore, Who was helping it at that time?

And this testing and telemetry equipment on board tejas weighs more than 300 KG. If they are removed it will only improve the flight specs of TEJAS, not degarde it.

Entire SUKHOI and mirage fleets were grounded after a few crashes, Does that mean they are substandard projects?the reason for the grounding was the rearrangement of fuel lines after a fuel leak was found on just one of the LSps and the HMDS overshoots the pilot's seat and will be a safety hazard incase of an emergency for pilots.

it has been proved that many tejas LSps took off many times in the same day and did the assigned jobs. Most of the flight test have a day or twos time in between. the reason is for analyzing the previous flight's data and to set parameters for the next flight according to that.For God's sake , it is flying on world renowned GE engines, so what is the reporter attempting to cook here?

Problems like this are not peculiar to Tejas, due to unresolvable vibration issues all royal Airforce TYPHOONs are flying at just 80 percent of the capacity, There were many cracks found on the Naval hornets bound for US navy,And a pilot death is speculated to have happened on F-22 due to faulty OBORG system.

Less said the better about the russian fighters operating in IAf, hundred MIG-23s were grounded (after a group captain was killed in a crash)prematurely because their engines had unresolvable problems,


Su-30 MKi often return to base with one engine, due to engine shaft failures, and a couple Su-30 MKI crashes leading to death of IAF pilots was determined to have resulted from FBW bugs.

During those times the entire sukhoi-30 MKi fleet is grounded.You would have read what is happeneing with Dremliner civilian planes in broadsheets.

The less said the better about the state of our MIG-21 fleet.Despite decades of induction , only last year IAF achieved least accidents comparable to world standards.

Shall we say all these products are useless.
These revelations come against a backdrop of pressure from India's defense minister Antony and India's government to buy designed-in-India items unless there's no other choice. He's selling changes to external link India's Defence Procurement Policy as an anti-corruption effort – but what do you call spending billions of dollars on politically-allied state organizations, who don't deliver on the critical defense projects assigned to them, and never pay any serious penalties for it? Their competitors in China and Pakistan are consistently faster and often better – while doing a better job developing their industries. See also India PIB external link.

All of India's defence procurement is riddled with corruption and it will be so as long as we buy billions worth stuff from abroad.

And no anti corruption effort is going to prevent it as long as we are governed by corrupt leaders, tejas program has nothing to do with it.

So this GOD given revealations have nothing to do with tejas program .

The initial 40 SUKHOIs delivered to india ten years before had no weapons on them and are decidely inferior to SU-MKI specs and spent ten years wasting Indain tax payer's money under the guise of honing tactics in IAf fleet, They were recently returned to Russia to be as secondhand stuff to some other nation and are being replaced by new ones in SU-30 MKi standards.

Guys salivating over foreign mall and saying tejas completed IOC with relaxed or inferior specs will keep all their holes shut , if you confront them with fact like this..

The reason is all new equipment will mature over years in deployment.
RAFALE has F-1, F-2, F-3 phases of development,
Grippen A/B, C/D and now NG demo,
f-16--A/B ,,,,and Blk-40, Blk-52, blk-60.
Sukhoi line starts from SU-27 to , 30 , 30 MKI, Su-35 and now being evolved into FGFA.

If you want to buy fully mature weapon systems that have finished their developmental lifecycles and at the peak of their performance, you can buy F-16 and Mirage-2000 inducted in the seventies. not new models.
March 20/13: More delays. A Parliamentary reply confirms the obvious, formally extending the scheduled end of the LCA's Phase 2 Full Scale Engineering Development from December 2012 to March 2015.
This second phase began in 2004 only after IAf revised ASR to include more heavy, longer range, hihger launch stress inducing beyond visual range BVRs , leading to major redesign of composite wings, which is also specified by the same report of a parliamentary committee.
the reporter is showing his mischeavious intention by suppressing this vital fact.
The IAF has ordered 20 fighters in "Initial Operational Clearance" (January 2011) status, and another 20 in "Full Operational Clearance" (i.e. combat-ready) configuration. Full Operational Clearance is now expected in December 2014. PTI, via Zee News external link | India MoD external link.

{^}
The above update is a recent abstract from our full article, itself part of our subscription offering. Keep reading to know more.
LCA Tejas Underside
Tejas LCA
(click to view full)

India's Light Combat Aircraft program is meant to boost its aviation industry, but it must also solve a pressing military problem. The IAF's fighter strength has been declining as the MiG-21s that form the bulk of its fleet are lost in crashes, or retired due to age and wear. Most of India's other Cold War vintage aircraft face similar problems.
The LCA project was conceived in 1983 and due to inter departmental wrangling I posted in TKS tales link , and financial crunch of the 1990s , it's funding for TDs (FSED-1)was released only in 1993. The Td flew in 2001. And then again in 2004 IAF revised ASR resulting in FSED-2.And it is now being completed in 2013.

this is pretty much the norm for all fighter projects.

From FSED phase the grippen, Eurofighter TYPHOON and RAFALE all entered service only after around 17 or 18 years and are still being upgraded in phases in newer versions.

But tejas ASr was upgraded in 2004 itself. it is akin to jumping directly to F-16 blk 52 without operationalizing F-16 A/B.

So if the LCA program took 5 or 6 years extra , it compares quite well to other international program.
TYPHOON is yet to complete it's ground bombing role , which tejas did before IOC, SO why the howling cries for tejas's head?
In response, some MiG-21s have been modernized to MiG-21 'Bison' configuration, and other current fighter types are undergoing modernization programs of their own. The IAF's hope is that they can maintain an adequate force until the multi-billion dollar 126+ plane MMRCA competition delivers replacements, and more SU-30MKIs arrive from HAL. Which still leaves India without an affordable fighter solution. MMRCA can replace some of India's mid-range fighters, but what about the MiG-21s? The MiG-21 Bison program adds years of life to those airframes, but even so, they're likely to be gone by 2020.
The troubles with MIG-21 fleet is du to the piss poor engineering design qualities of it's aerodynamic config and unreliable parts supplied by russian firms and it's faulty aerodynamic layout of pre historic era. Just laying all these at tejas's door is simply a motivated lie.
That's why India's own Tejas Light Combat Aircraft (LCA) project is so important to the IAF's future prospects. It's also why India's rigid domestic-only policies are gradually being relaxed, in order to field an operational and competitive aircraft. Even with that help, the program's delays are a growing problem for the IAF. Meanwhile, the west's near-abandonment of the global lightweight fighter market opens an opportunity, if India can seize it with a compelling and timely product.
Displaying 633 of 16,752 words (a
Tejas has achieved it's goal of developing a viable aerospace industry,
giving the country a fighter to export ,
giving a worthy fighter for it's total lifecycle cost for IAF and NAVY,
and built design capabilities for 4.5th gen fighter which will fructify into 5th gen AMCA.

So it doesnot needs the reporters crocodile tears to do all these.
 
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