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
Status
Not open for further replies.

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
No where did the cemilac paper said that the designs are being implemented in mk1. The design features are being implemented on newer variants, like mk2 (added length) and levcons (naval variant), something your pea sized brain cannot comprehend.
when did the cemilac paper said it is being implemented in mk-2? use your super sized brain and please inform the forum.

Dont hide like a coward like the way you refused to post the exact percentage of composites in the grippen.since you are the one who quoted to the post you should quote the percentage to forum members. You can use the time you took to think about who wipes my bottom to do some honest posting.


And dont lie like the way you do when you said that RCS enhancing canards and matchbox shaped air inlet of grippen is will result in a lower than tejas RCS.

that is not the way scholarly debates are conducted. quoting a technical paper for the identification of a problem, and refuting the technical paper when it says it is being implemented.

So you are admitting that all the grippen c/d variants are junks with lesser thrust to weight ratios, and their landing gers cannot be relocated, and once again sensor fusioned video games play station as they always were.


other wise admit that all your ng specs for grippen are from a prototype that hasn't entered production and yet to be validated and also the faact that not a single GRIPPEN NG has entered squadron service with foreign airforce. and two developmental aircrafts of grippen NG are expected to fly in 2013 !!!!!.

link--http://www.defenseindustrydaily.com/the-jas39-gripen-swedens-4th-generation-wild-card-02401/


You have already decided that there will be no issues that wont crop up in this NG version. Where a developmental air craft is expected to fly in 2013. Further validations of modified FCS wont throw out any issues and all are as good as finished.

But a nose plug implementation involving increasing the dimension of LCAA is beyond the competency of ADA.

Once you throw invectives it is guarenteed that you are covering your lies.
 
Last edited:

A chauhan

"अहिंसा परमो धर्मः धर्म हिंसा तथैव च: l"
New Member
Joined
Oct 10, 2009
Messages
9,533
Likes
22,583
Country flag
@ ersakthivel,

Please report the offending posts ! the discussion should go on in a civil manner. No one is entitled to abuse no matter if he is a genius or something else. And please format your posts in an acceptable form. :)
 

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
So this nose plug insertion is no big issue at all. It has been done before in other fighters. So don't hide like a coward behind CEMILAC test paper by JEBAKUMAR.

Essentially the nose will be longer and hence sleeker, akin to the changes made to the Cheetah/Kfir from the original Mirage III, where the nose plug was added (the reason for that of course was mainly to add volume for the radar and avionics suite)

Try arguing with some facts insted.Dont throw personal abuses.
 

Twinblade

New Member
Joined
Dec 19, 2011
Messages
1,578
Likes
3,231
Country flag
when did the cemilac paper said it is being implemented in mk-2? use your super sized brain and please inform the forum.
I never claimed that the paper mentions specifically that the changes will be implemented in Mk2 for when the paper was writtem the mk2 was in its initial design phases. However empirical evidence from various news reports indicates that the changes recommended in that paper are being implemented in other variants like increased length ranging between half and one meter via nose plug.

AERO INDIA: ADA shows models of Tejas Mk II
The primary difference in configuration will be the Mk II's length, as it will be 13.7m long compared with 13.2m for the Mk I.
TRISHUL: Users Insist On Radical Makeover For Tejas Mk2
TRISHUL: Users Insist On Radical Makeover For Tejas Mk2
The Tejas Mk2 will have a length of 14.2 metres (1-metre more than that of the Tejas Mk1 for incorporating a stretched nose section and a modified fuselage section aft of the cockpit for housing an expanded complement of mission avionics LRUs)
The reports are inline with the paper's conclusions, whereas you have claimed that the changes have already been incorporated in mk1 and given no proof of such whatsoever. No link, no studies nothing. You haven't even reproduced any quote from the links I gave you in favour of your argument. This is blatant trolling.


Dont hide like a coward like the way you refused to post the exact percentage of composites in the grippen.since you are the one who quoted to the post you should quote the percentage to forum members. You can use the time you took to think about who wipes my bottom to do some honest posting.


And dont lie like the way you do when you said that RCS enhancing canards and matchbox shaped air inlet of grippen is will result in a lower than tejas RCS.
I am reposting the link for his highness Sultan of Jhumri Talaiya. The relevant information is on page 7 in a graph titled "India makes it to Global Composites Scene with LCA- Tejas Program"

http://www.icas.org/PDF-documents/ICAS%20Workshop%20presentation%2006%20Upadhya.pdf
I never claimed that Gripen has lower RCS than Tejas. Produce my exact quote, which you won't be able to, because I never claimed so. By doing so you are misquoting me which indicate either you are a compulsive liar or have really low comprehension of what is being discussed here.


So you are admitting that all the grippen c/d variants are junks with lesser thrust to weight ratios, and their landing gers cannot be relocated, and once again sensor fusioned video games play station as they always were.
Never said so, never claimed so and never presented any argument in that direction. This is a ridiculous inference which isn't even remotely related to what I have written. At this point I would like the mods to intervene because you are blatantly misquoting and flaming.

other wise admit that all your ng specs for grippen are from a prototype that hasn't entered production and yet to be validated and also the faact that not a single GRIPPEN NG has entered squadron service with foreign airforce. and two developmental aircrafts of grippen NG are expected to fly in 2013 !!!!!.
I have not presented a single spec from Gipen NG, at all.


You have already decided that there will be no issues that wont crop up in this NG version. Where a developmental air craft is expected to fly in 2013. Further validations of modified FCS wont throw out any issues and all are as good as finished.

But a nose plug implementation involving increasing the dimension of LCAA is beyond the competency of ADA.

Once you throw invectives it is guarenteed that you are covering your lies.
Never said so, never claimed so. On the contrary I have claimed that the nose plug is being incorporated in Tejas mk2. You on the other hand have claimed that nose plug would be incorporated in Mk1 post induction into IAF without giving any proof there of. This is your actual quote.
The sweedish airforce plans to upgrade 70 of it's grippens to NG standards. if grippen c/d can be upgraded to grippen ng with relocation of landing gear, bigger fuel tanks,more composites, then this nose plug cone can easily be applied to tejas. the report explicitly states that it is being done.And nothing forbids it to be done even later after the induction of mk-1. As grippen c/d s are going to be upgraded into the E/f standards.
Furthermore you are ill informed about Gripen's upgrade as well.


So this nose plug insertion is no big issue at all. It has been done before in other fighters. So don't hide like a coward behind CEMILAC test paper by JEBAKUMAR.

Essentially the nose will be longer and hence sleeker, akin to the changes made to the Cheetah/Kfir from the original Mirage III, where the nose plug was added (the reason for that of course was mainly to add volume for the radar and avionics suite)

Try arguing with some facts insted.Dont throw personal abuses.
I am not aware of any such upgrade involving increase of length. The only length specific modification I am aware of was from Mirage IIIC to Mirage IIIE which was a different variant and not an upgrade. Can you point me towards any online resource that points toward mid life fuselage extension upgrade of an in service fighter aircaft ?
 
Last edited:

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
repected twin blade

twin blade says in his post no----3056 13/1/12

I never claimed that the paper mentions specifically that the changes will be implemented in Mk2 for when the paper was writtem the mk2 was in its initial design phases. However empirical evidence from various news reports indicates that the changes recommended in that paper are being implemented in other variants like increased length ranging between half and one meter via nose plug.


Thee reports are inline with the paper's conclusions, whereas you have claimed that the changes have already been incorporated in mk1 and given no proof of such whatsoever. No link, no studies nothing. You haven't even reproduced any quote from the links I gave you in favour of your argument. This is blatant trolling.

E.R.sakthi vel says

Does your emprical evidnence also suggest that it is impossible to add nose cone plug for mk-1 even after FOC as it is already done in KFIR and MIRAGE-III. What you are doing is lying through your nose. Since you frequent other blogs too it is impossible that you dont know it has been done to other fighters like MIRAGE_lll and K fir.

I have noticed that even in other forums you are using the same arguments.

link-http://forum.keypublishing.com/archive/index.php?t-118205.html

I never claimed that Gripen has lower RCS than Tejas. Produce my exact quote, which you won't be able to, because I never claimed so. By doing so you are misquoting me which indicate either you are a compulsive liar or have really low comprehension of what is being discussed here.

Furthermore you are ill informed about Gripen's upgrade as well.
I am not aware of any such upgrade involving increase of length. The only length specific modification I am aware of was from Mirage IIIC to Mirage IIIE which was a different variant and not an upgrade. Can you point me towards any online resource that points toward mid life fuselage extension upgrade of an in service fighter aircaft ?


Your http://www2.foi.se/rapp/foir0338.pdf link is in not in english

xxxxxxxxxxxxxxx Language !!


Since you have caimed that you never said anything concrete anywhere ,what am I or MOD will do here?

So all I accept is that you have

1.never said anything regarding the percentage of composites in grippen, and you will never say so in future.

2.You never said that nose cone plug is implemented in mk-1 and you claim that you have nothing to add when I say


E.R.SAKTHI VEL says

Essentially the nose will be longer and hence sleeker, akin to the changes made to the Cheetah/Kfir from the original Mirage III, where the nose plug was added (the reason for that of course was mainly to add volume for the radar and avionics suite)
3. since the link you posted is in sweedish language I or any forum memeber for that matter too can never say anything authoritative about your PDF.


xxxxxxxxxxxxxxxxxxxxxxxxxxxx Language !!

xxxxxxxxxxxxxxxxxxxxxxxxxxxx Language again !!

But let me finish by saying----"BLESSED ARE THE ONES WHO NEVER SAY ANYTHING WHEN THEY HAVE NOTHING TO SAY"

This is what i found in a greeting card. So please adhere to the saying.

Since you are incapable of never saying anything concrete this finishes the debate between us.GOOD BYE

Mod: Finally. Thanks to both of you. May we please save this thread from ad hominem, rabid language and go back to the topic.
 
Last edited:

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
repected twin blade





Your http://www2.foi.se/rapp/foir0338.pdf link is in not in english

xxxxxxxxxxxxxxx Language !!


Since you have caimed that you never said anything concrete anywhere ,what am I or MOD will do here?

So all I accept is that you have

1.never said anything regarding the percentage of composites in grippen, and you will never say so in future.

2.You never said that nose cone plug is implemented in mk-1 and you claim that you have nothing to add when I say



3. since the link you posted is in sweedish language I or any forum memeber for that matter too can never say anything authoritative about your PDF.


xxxxxxxxxxxxxxxxxxxxxxxxxxxx Language !!

xxxxxxxxxxxxxxxxxxxxxxxxxxxx Language again !!

But let me finish by saying----"BLESSED ARE THE ONES WHO NEVER SAY ANYTHING WHEN THEY HAVE NOTHING TO SAY"

This is what i found in a greeting card. So please adhere to the saying.

Since you are incapable of never saying anything concrete this finishes the debate between us.GOOD BYE

Mod: Finally. Thanks to both of you. May we please save this thread from ad hominem, rabid language and go back to the topic.
I wont post any offensive words, please ask the other members to adhere the same. Thanks,
 

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
I asked both the guys twin blade and p2prada many time to not to post offensive language. But my warnings fell on their deaf years. That's why I paid them back in their own language that too only in sarcastic manner. I wont do even that in future.

I love your blog and blogs like these empower ordinary folks with a terrific amount of knowledge in the field of aeronautics.So I will debate in a scholorly manner with facts. Sorry if any of my post has offfended any one in this forum. I will also use multi quotes and make my points in a concise manner, posting link names without cutting and pasting long portions of it. I will also not post in multi colour.


apologies to anyone I offended.I wont do this again in this forum however stronger the provocation may be.
 

p2prada

New Member
Joined
May 25, 2009
Messages
10,234
Likes
4,017
This is blatant trolling.

By doing so you are misquoting me which indicate either you are a compulsive liar or have really low comprehension of what is being discussed here.

This is a ridiculous inference which isn't even remotely related to what I have written. At this point I would like the mods to intervene because you are blatantly misquoting and flaming.
He can't read, he can't comprehend and he can't discuss. He is hopelessly ignorant and has ZERO interest in learning anything.

@Ersakthivel

Three people have pointed out that you can't "read." Twin, Shiphone and myself. And in the entire time you were here, these are the three people you have "discussed" with. Go Figure!
 

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
He can't read, he can't comprehend and he can't discuss. He is hopelessly ignorant and has ZERO interest in learning anything.

@Ersakthivel

Three people have pointed out that you can't "read." Twin, Shiphone and myself. And in the entire time you were here, these are the three people you have "discussed" with. Go Figure!

from now on you and twinblade don't have to discuss anything with me. I too will not discuss anything with two of you guys. I will post general information regarding tejas with authentic source ,ofcourse. So far 56 members were able to read and appreciate my post,that's enough,you can give respect to their point of view. So many people have read and appreciated the posts of you,shipone and twinblade, I respect their point of view. please refrain from mentioning my name.

we both need not have to give certificate of literacy to each other. We are not university vice chancellors to give certificates of qualification to each other.I have already given an undertaking to the forum members,virendra,daredevil,and lurker baba regarding this. And I intend to follow it in letter and spirit.
Whatever we post here TEJAS will take it's place in the military aviation history ,no one is going to stop it.So refrain from personal attacks.

In technical field we fight authentic arguments with authentic arguments. That's all,

Bye ,Happy postings in the forum, However much you guys provoke me I am not going to stop posting.
 
Last edited:

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
MODs please warn P2PRADA not to start again,instead ask him to stick to the topic.
 

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
MODS please point out my posts that needs editing ,I will format them in proper form.
 

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
As a real life example, let's say you are in 12th standard(LCA's IOC) and are claiming to finish Engineering(LCA's FOC) after 12th. But you failed 12th standard exams. During supplementary you fail again. Then you will fail again the next time. Followed by another time and then another. If you can't even pass 12th standard(LCA's IOC) then how then heck will you even get into Engineering let alone clear it. So, this is where LCA is right now. ADA has been trying to get to IOC since 1999 or more recently 2005. Since 2005, they have only been giving dates one after the other. LCA was supposed to have achieved IOC in 2009, then it changed to 2010, then 2011. In 2011 they lied to IAF. IAF got angry and hence you see why ACM Naik is so unhappy. ADA promised full IOC in 6 months, that passed, now it is supposed to be March 2013. So, ADA will probably take 5 years just to finish 12th std. After that comes Engineering... hence we laugh at ADA.

So, the question is when will LCA achieve IOC? LCA is 60s technology, nothing more. And ADA is still trying to get the technology to work 50 years later. Just because it is 2012 does not make it an advanced aircraft. New aircraft have come and are going also, but still we are waiting for LCA's IOC.

Since I have already promised not to mention names ,I wont name anybody here.

Any one in this forum can go and see F-16 sites, grippen sites, mirage sites and see for themselves how aircrafts get updated thruogh out their service life with bigger engines and better ew suits, higher fuel capacity, longer nose cones , does that mean they have all failed the 12th exams and should have gone to tutorial colleges?

The IAF is spending 1.5 billion dollars on mirage updates. a 30 year old airframe. It has been posted in IDRW.org recently that what jags are going to get for updates and anyone can check it. how mirage -lll and kfirs extended their nose cones and even put more avionics inside it.

Is it fair to accuse that tejas wont get any bigger engines and get a nose job. Even actress SRIDEVI did one nose job before attaining stardom in BOLLYWOOD.
So why are respected forum members arguing to the contrary?

Grippen NG is just one prototype plane taking part in MMRCA competition with fancy specs. Will it also fail in it's 12th exam? Do you think that IAF selection committee is a body of budheads to allow grippen into it,they could have said since you have already crashed two prototypes in grippen A/B development ,you will crash more on in NG version and fail the 12th exam?

What I want to point out to the respected member who posted this stuff is when planners induct a platform they visualize it's future potential not what it did before IOC? Nowadays even bachelors don't ask their girl friends "what you did in the past relationship?"

What tejas has is immense potential for future growth. let me list out them for you

1. It will certainly get a more powerful engine slatted for AMCA in the form of snecma kavery-K-10. The french have conducted a through study of K-9 and concluded that hihger thrust versions are possible in 3 years development.Prat and whitney has already certified that this engine is world class and it has immense potential to improve.If higher thrust engine is put in it can easily excel in low altitude.

2.It will get the avionics and asea tech radar that will go in AMCA.Since miniaturisation in future will actually result in weight savings and not weight increase with this new improvements.

3. If still iaf want to improve the craft they can always rely on ADA, they wont charge more than the original price for updates like Foreign manufacturers do.
 
Last edited:

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
A respected member says,
If you have problems with my old posts, then ask what you want to know and I will tell you the reason why I posted that way. Don't generalize and give sweeping comments without knowing anything. Some of the posts were made when we knew lesser about LCA than what we know now. So, somethings may not be applicable in today's world. For eg: During IOC-1 nobody knew the empty weight of LCA was 6.5 tons. ADA released a new spec after the function which proved some people right and some people wrong.

Btw, that CEMILAC report about LCA's drag was only a suggestion and the conclusion only pointed out the paper suggestion could be correct. It is in no way an indicator that ADA used this report to fix the LCA exactly as it says.
Btw it is explicitly mentioned in the CEMILAC report that this problem can easily be fixed with the addition of nose cone plug, AND IT IS UNDERWAY. It may or may not have been fixed by ADA. That only ADA can officially clarify, not anyone else. Since it has been done on MIRAGE-lll and KFIRS and extra avionics were placed even increasing it's weight . So there is no better weight penalty for LCA here. Since the extended nose cone plug will only result in volume addition, not significant weight addition.

As ADA surprised many respected forum members with their IOC specs, it may even offer some pleasant or unpleasant surprises to respected forum members during FOC . I dont think that ADA has given an explicit guarantee that the length of LCA will be be exactly 13.2 meters and no nose cone plug modification will ever be carried out before FOC , and even if it is not carried out at FOC ,it wont be done through out the service life of the craft.

Since there are many fools in india who launch nuclear subs and who build low speed ballistic missiles(according to a respected forum member, not me) and even bud heads in ISRO who send CHANDRIYANS to moon, even 12th standard fail IITans and their 7000 salary receiving useless faculties who design substandard milimetric wave seekers that only few have in this world, for help. Putting all their useless heads together ADA may even end up solving this problem and surprise the respected forum members some day.

Considering this fact, instead of wasting it's time on this minor modification and delaying IOC and FOC further, ADA may have decided to continue with more important higher AOA ,flutter tests, and all important spin recovery tests, to validate these design parameters first and if some minor need for minor modifications,arise in these tests as well , they can club them together with nose cone additions in a single go.
That's what a sensible design organization do.First test your design fully to it's limit, identify all possible mistakes and correct them together or sequentially whichever way is proper.

Why this is made as such a big issue?

Thanks for admitting that some respected forum members didn't know tejas better before.I am delighted with their magnanimity after 40 pages of flaming. So to avoid further arguments they can try to know TEJAS better from now on instead of taking position in this forum like it is as if a trench warfare in world war -ll. This is a forum to further the knowledge of many people in aviation. Visitors don't come here to see our arguing skills and foul word vocabulary.
 
Last edited:

ersakthivel

Brilliance
New Member
Joined
Mar 6, 2011
Messages
7,029
Likes
8,764
Country flag
Respected forum member says
HF-24 was second generation. LCA is currently only a 4th gen on paper. It will be a 4+ only if it gets AESA. AESA is still a decade away, especially considering LRDE is still looking for a partner to provide T/R modules.
E.R.sakthivel says,
three MMRCA contenders arrived without ASEA and one chosen didnot have a functioning asea at the time of evaluation.
Respected forum member says
The only good thing on LCA is the Fly by wire and carbon composites. Fly by wire was designed by Indian scientists in Britain and the US, not in India.
E.R.sakthivel says,
Fly by wire is every thing in a fourth gen planem Every thing else is system integeration.

Respected forum member says
The higher drag of LCA results from it's higher wing area than grippen.
The higher wing area is there for a purpose.
Link? Because I am not aware of it(mostly because it is wrong).
E.R.sakthivel says,
From where does the drag produced generally in an aircraft?
Respected forum member says
MKI has a much larger wing area, it can probably carry LCA and still go supersonic(jk).
E.R.sakthivel says,
Dont compare twin engine birds. No one can certify that LCA cant go supersonic,yet.


.
Respected forum member says
If that is the case, then why does the N-LCA prototypes have LEVCONS? These do the work of canards.
E.R.sakthivel says,
ARE levcons and caards the same ,please ask any forum members, Levcons don't move and don't need any hydraulics
Respected forum member says
The absence of canards is only because canards were not needed for the role it was supposed to play, ie, an interceptor and point defence. It would have made the design unnecessarily complex too.
E.R.sakthivel says,
The absence of canard is due to the fact that it doesnot add any incremental value over it's weight penalty, that is ADA's position
Respected forum member says
We will see how good LCA's low speed capability is once information is given on it.
E.R.sakthivel says,
Well I like the tenor of the statement.

E.R.sakthivel says,
And software is Indain forte. Once the flight tests are over there is nothing that stops the country which has the world's largest number of software engineers from giving the best of support to it's avionics
respected forum member says,
Wrong. We just have a low paid workforce who mostly do testing and a little bit of development. The best software developers still belong in better countries
20 years before canadian stock exchange trusted TCS to their computerization.INFY's FINACLE is one of the best banking softwares in the world.
By the way what do you mean by we?
.

respected member say,
Software is still the forte of big design houses like LM, Boeing, Dassault, Saab, Sukhoi etc. ADA is still a fledgling compared to these biggies. If someone wants to design a software code for ATMs, then they will look to us, not for aircraft.
E.R.sakthivel says,
The F-16 test pilot commented that F-16 flies better with LCA software and even aerodynamically better. This is according to the designer KOTA HARINARAYANA's words in ADA article.
 
Last edited:

p2prada

New Member
Joined
May 25, 2009
Messages
10,234
Likes
4,017
Any one in this forum can go and see F-16 sites, grippen sites, mirage sites and see for themselves how sircrafts get updated thriugh out their service life with bigger engines and better ew suits, higher fuel capacity, longer nose cones , does that mean they have all failed the 12th exams and should have gone to tutorial colleges?
Look at when the first flight happened for these aircraft, all 70s and 80s. Any 4th gen aircraft which wasn't inducted in the early 2000s is a waste of time. Why do I say that? It is because 4th gen became obsolete the minute the F-22 was inducted in 2005.

Now combine 4th gen and light aircraft, that is beyond the word obsolete. It is like clearing 12th standard when you are 30 years old. Worthless?

The IAF is spending 1.5 billion dollars on mirage updates. a 30 year old airframe. It has been posted in IDRW.org recently that what jags are going to get for updates and anyone csncheck it. how mirage -lll and kfirs extended their nose cones and even put more avionics inside it.
All old frames can be upgraded for another 10 to 15 years of life. This makes sense because the frames have been in use for many years. All the protocols for training, maintenance and fighting a war were in place since decades. Comparatively LCA will be inducted in 2018 and will need another 10 years of service to have a similar level of training, maintenance protocols and war fighting capability in place. So, LCA will be a proven aircraft(say 2028) when superior aircraft like the F-16 and Mirage-2000 will actually be phased out of all air forces everywhere.

It's like Bangladesh making their first Maruti 800 today, when we have stopped production of the Maruti 800. The Bangladeshis can jump with joy, but what is the use of such a car today? Think? LCA is in that exact position.

Is it fair to accuse that tejas wont get any bigger engines and get a nose job.
Engine change is possible only after 2030, when LCA finishes 10-15 years of service life. Until then it will continue having the underpowered F-404.

It won't get a new nose either, because the changes need to be made before the final design is ready. Design changes are made only when the aircraft is still on paper. That's why all the problems on Mk1 will be fixed only on Mk2. Mk1 will stay as is.

Grippen NG is just ine prototype plane taking part in MMRCA competition with fancy specs. Will it also fail in it's 12th exam? Do you think that IAF selection committee is a body of budheads to allow grippen into it,sayimg since you have already crashed two prototypes ,you will crash more on in NG versiom amd fail the 12th exam?
Gripen C is far superior to LCA. Gripen NG is even more superior. It is meant for air forces that cannot afford a 5th gen platform like the F-35. Hence it is being made. LCA Mk2 will bring the aircraft to a Gripen C level.

This is a paper evaluation done by the Dutch on MRCA contenders.


In the above graph, see where Gripen C/NG is and see where heavier aircraft like Rafale and EF are. LCA Mk2 will be as low as Gripen C or MLU F-16. Mk1 won't even be in the graph.

What I want to point out to the respected member who posted this stuff is when planners induct a platform they visualize it's future potential not what it did before IOC? What tejas has is immense potential for future growth.
This is the Swiss result.
Rafale News: Switzerland, Armasuisse officialy ranks the Rafale first
Rafale and Eurofighter showed generally better performance than the F/A-18, Gripen worse"

"The performance of the Gripen in air-air engagements as well as attack missions was insufficient"

"The most limiting factors of the Gripen design were the operating time, the flight performance and the maximum weapon load"

"The Rafale is the only aircraft that has met the requirements of the Air Force in all types of applications"

3- The Gripen has serious weaknesses and is considered as a step back compared to the F/A-18 operated by the Swiss Air Force.
So, if an aircraft like Gripen NG was so inferior for an air force like Switzerland, then where does that put LCA Mk2? Do you get the point now?

1. It will defenitely get a more powerfull engine slatted for AMCA in the form of snecma kavery-K-10.
The Mk2 may, the Mk1 has even lesser chances. All of this may happen post 2030 when we may see the first 6th gen aircraft flying. So, no need to be so sure when I am using words like "may" here. Air forces don't work on concepts like "may."

Armed forces don't use words like "definitely." It is all about what you have "now." The reason why aircraft like Jaguar and Mig-21 are currently superior to LCA.

2.It will get the avionics and asea tech radar that will go in AMCA.Since miniaturisation in future will actualy result in weight savings and not weight increase with this new improvements.
Again, if you notice the ADA's poster for LCA Mk2 improvements that was posted in AI-2011, you will notice that there is no mention of AESA radar on it only a reference of the same old, same old.



LCA does not even need AESA. It is worthless. It does not have the payload or the range to use ESA's multi function advantages.

AESA is meant for aircraft that can carry 4+ A2A missiles and 2+ 500Kg LGBs and 2 drop tanks, so it can use the radar properly. Other than that AESA radars need a lot of cooling, so if we install AESA on the LCA's small nose, the radar will be less capable than a similar Mech scanned radar. What I am saying is a Mechanically scanned radar will be superior to the AESA because of size constraints, irony, because AESA is supposed to be smaller and lighter than MSA. Larger aircraft don't have such a problem.

So, can LCA carry this?


A big NO. So, is AESA useful? A big NO.
 
Status
Not open for further replies.

Articles

Top