LCA Tejas: News and Discussions

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NRao
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Re: LCA Tejas: News and Discussions

Post by NRao »

Sure.. but they have never said they will not share nor they will openly.
The thumb rule is that *no one* will part with their IP that helps drive their MIC - no one.

The Indian request, from the US, was a serious enough for the SD to step in - France/Russia has got to have similar laws. Will France be more open? Do not know, but, I am betting that they too will go only so far and not beyond. Besides, the issue is not just about uprating an engine, it is about getting access to techs that India needs and also a growth path. I am not too sure, this is an educated(?) guess, but I feel that GE is well ahead of the curve. EJ can deliver a 110KN engine, what they can beyond that is the question.

---------------------------------

There was an article I came across that claimed that the Indians wanted to use the core from the Kaveri, along with techs from other nation/s to fill the gap. Have no clue how far it is true and how feasible is it, especially in the time frame.
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Re: LCA Tejas: News and Discussions

Post by tsarkar »

I would summarize as follows -

People need to stop saying that Tejas is delayed. No, its development is taking reasonable time what it would've taken anywhere in the world to develop a combat capable fighter.

People need to stop saying that Tejas is overweight. No, 6500 kg empty weight is normal for a fighter of its class as evidenced by its peers.

People need to stop saying that IAF requirements were unreasonable and added to the delay or weight. No, most of the requirements are very standard for a combat capable fighter.

Exception being the 5500 kg empty weight that IAF has itself waived off before IOC.
There is a marginally higher landing speed that IAF has accepted by waiving off original requirement.
There is a minor difference between design speed and achieved speed that IAF has accepted by waiving off original requirement.

With regards to AoA, ITR, STR, we need further information to conclude whether those requirements were reasonable or unreasonable.

People need to stop saying that IAF changed goalposts. No, CAG is clear on this. Except for weapons, specifically Derby & Python, no other goalposts were changed.

With regards to Derby, it was proving itself in service with the Sea Harrier around the same timeframe (~2009) when IAF specified it for Tejas. With the bad experience of R-77, I believe IAF did their due diligence for Derby. Hence it could not have been specified earlier.
Last edited by tsarkar on 07 Jul 2015 11:15, edited 1 time in total.
ramana
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Re: LCA Tejas: News and Discussions

Post by ramana »

Even the F-16 which flew early on and the one that was inducted were very different. So initial demonstrator and the actual one are expected to be different.

BTW saw a twitter report of an F-35 pilot grumbling about sluggish performance in dogfight situations due to insufficient energy! In other words STR was not achieved.


Again folks just as LCA is approaching FOC no point in blame games.

A lot of lesson have been learned.

tsarkar has summed it up.
Of these AOA is ~26(?) goal 28.
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Re: LCA Tejas: News and Discussions

Post by Singha »

if Eurojet = MTU + RR + hispano suiza, only RR makes the hot-section. RR has a long history but their best selling engines like spey, rb199 and adour are far lower than ej200 engine...and the ej200 is the most powerful they have.

they have excellent civilian side expertise in bigger engines but not military.

GE on the other hand has giant engines on military side also, the unselected F120 for F22 and F136 for jsf but they lost both deals to P&W so not sure what lucrative future they have in fighter engines now.
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Re: LCA Tejas: News and Discussions

Post by ramana »

Don't forget RR even on civilian side killed the L1011 plane with underperforming engine.
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Re: LCA Tejas: News and Discussions

Post by putnanja »

Ajai Shukla supporting LCA and AMCA ..

From Tejas to AMCA
Karan M
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Re: LCA Tejas: News and Discussions

Post by Karan M »

tsarkar wrote:^^ Karan, what you posted only corroborates that LCA TDs were science lab projects, and the process to make it a viable fighter started in the 2001-5 timeframe.
So? Boss, all throughout I have been making the EXACT point that the AF led decision to keep the TDs as science lab programs was FLAWED thanks to their desire to keep the program in a very "lets see and then decide manner" which is where the entire development process was doubled since basic technology had to be reworked or added in much much later.

ADA and HAL were completely inexperienced and went by consultant reccomendations & IAF manuals for existing airframes eg Mirage 2000 - when the IAF joined they wanted something better! If the IAF team had been part of the TD process itself & the TD process was not merely a "demo" but worked on in parallel with a clear roadmap (as versus waiting for FSED approval) we would have saved a heckuva lot of time.
The Mk-1 configuration aircraft started coming after I took over in 2005. The challenge started with PV-2, which is the present Initial Operational Clearance (IOC) configuration aircraft.
Confirms that process from TD to Mk1 started in 2005

So? That is why I posted it in the first place!
The rear fuselage too had to be changed to accommodate GE404-IN20 engine.
There was no Kaveri, and TDs flew with F-404F2J3 that was a temporary engine for the TDs.

As we all know.
Even the MMR (Multi-Mode Radar) underwent changes after the indigenous effort to make one did not succeed. So we had to go for Israeli Elta Radar.
Here is the program head saying we went for an Israeli radar.

As we all know. The Hybrid MMR is NOTHING but an ELTA 2032 with an Indian scanner. Multiple references to it exist.
Karan M wrote:many were late changes because the TD systems were revised completely once IAF came on board in 2006!!
correction. TD's did not have any combat capable systems.

What correction? Who claimed that TD had all combat capable systems?

The point all along which you don't seem to get is that the TD ->PV development choice was FLAWED to begin with since the IAF did NOT specify proper specifications for the TDs themselves to do the heavy lifting.

As such everything had to be redone.

And BTW: The TD's mission computing systems were leveraged for the MiG-27, Su-30 MKI and even DARIN-1 upgrade so with a bit of leverage they could become very well combat capable.

Redone for the LCA PV and will only appear on Super 30 for the Su-30
TD's did not have any radar. Initially it was provisioned for MMR, thereafter Elta 2032
TD's did not have any production standard engine. It flew with GE F-404F2J3, was was provisioned for Kaveri, finally required GE F-404IN20
TD's did not have any LDP.
TD's did not have any HMDS.
TD's did not have any MFD.
TD's did not have any RWR.
TD's did not have any CMDS.
TD's did not have instrumentation like VOR, DME & ILS
TD's did not have any stores capability, so to develop Mk1, stores separation trails were required.
TD's did not have any missiles.
TD's did not have any guns.

So which specific TD systems were revised completely are you referring to?
LOL, here I was pointing out that this was the exact flaw in the program that the TDs didn;t have adequate mission capable systems and you are repeating my words.

Next you just posted a list of handful of items and even there you are wrong. TD's didn't have MFD? What were they flying with, steam gauges?
The TDs had a complete mission computing, display suite which experience was used for upgrade programs.

PS: There is more to an aircraft than just the above avionics, putting them in a list may make them appear a lot but there are over 500 LRUs in the Tejas. That includes the hydraulics, the aggregates, the airframe systems, etc.

All these need to be integrated into a functional platform.

The IAF choosing the flawed TD to PV model ensured the actual FSED started much much later.

I could even post a list of changes from my own notes but this is ending up as a waste of time.
AF goalposts did not change, except for weapons. CAG is clear on that.

The work referred to by PS is the work that went in to make a combat capable aircraft from TD to Mk1.

Or are you saying that IAF should've inducted LCA TDs in squadron service, that did not have radar or a production engine and was completely unfit for combat service?
More circular merry go around.

Lets be clear here. The IAF's "goalposts" or any customers goalposts for anyone even remotely associated with the process of making things, are not an end in themselves. They had to be involved in the process and they weren't. In the case of the LCA, the IAF happily let things slide till 2005 before which they werent bothered with the program and hence it took FSED to actually make the LCA into a combat aircraft.

As versus having done a fair amount of the heavy lifting by TD stage itself and not using this sequential process to begin with!!

IAF came up with high level specs & then disassociated themselves from the program till 2005-6. "AF goalposts didn't change" except the fact that only they knew what their specific interpretation of many of these goalposts would be, which is typical for a program of this nature.

The IAF appointee to the program recently noted that the IAF joined in 2006 and reworked all the design logic and raised hundreds of engineering change requests for the program to make it a viable program. All good, but thats five years after 2001!

Anyways I have wasted enough time on this.

Hopefully ADA and the IAF won't be stupid enough to repeat this flawed, sequential process and the IAF joins the program too late for ALL items in the AMCA itself otherwise we will see more of the usual.

But hey, who knows. We seem to have done much the same for the T-50 with the IAF waiting & watching and as a result we now need an India specific FGFA with no clear timeline of when it will be inducted and what workshare we'll end up having because we lost so much time already and have to agree to whatever the Russians allow us.

As long as our Air Marshals and distinguished scientists and great engineers all sit in their respective ivory towers, we will end up in the same mess again and again.
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Re: LCA Tejas: News and Discussions

Post by ramana »

Why don't we map the IAF personnel assigned to LCA from TD phase onwards?


We can clearly identify Cdre. Balaji from IN.

BTW Cdre. is higher than Group Captain but lower than Air Vice Marshal.

In US its equivalent is Rear Admiral Lower Half.

I bet even Squadron Leader ranks from Engineering section (let alone Flying section) were not assigned.
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Re: LCA Tejas: News and Discussions

Post by ramana »

Question for UB, vina, Vivek Ahuja:

Was the decision to dispense with canards for LCA body a contributor to the STR issue?

My thoughts:
The delta wing form needs additional control surfaces. Gripen, Viggen, Rafale etc. all have canards to achieve this.

LCA dispensed with canards for following reasons:
- Two more extra control surfaces adds complexity
- LCA has sufficient control surfaces to achieve the required specifications.
- Will take care of it by the flight computer and its software.
- Canards add to the radar cross-section
- F-16 does not have canards so its is doable to dispense with canards for LCA.

Maybe the aerodynamic shape parameters/dimensions for LCA does not lend itself to control by software only in this aspect.
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Re: LCA Tejas: News and Discussions

Post by Indranil »

This has been discussed in great detail. Go here for all the technical details. What followed was a few pages of studying the papers from ADA/NAL. Nileshjr can tell you more.

@Nilesh, let's get that document going again. Can you please post the link to that online document again.
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Re: LCA Tejas: News and Discussions

Post by ramana »

OK. The compound delta wing and possibly software negates the canard need in LCA.

I'll ask in different way.

Wind tunnel and CFD will show the flow around the aerodynamic shape. We see that from the papers and explanation given by Nileshjr.

However actual control is shown only in flight as the FCS is a hidden variable?
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Re: LCA Tejas: News and Discussions

Post by Vayutuvan »

If you mean by FCS flight control software, then yes the simulations can be carried out with various positions of the control surfaces too. CFD simulations will reveal aerodynamics.
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Re: LCA Tejas: News and Discussions

Post by vsunder »

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Re: LCA Tejas: News and Discussions

Post by Bhaskar_T »

Saurav Jha ‏@SJha1618 - The Tejas Mk 1.5 will be called the Mk 1A.

Is Mk1.5 officially recognised btw? Mk1.0 IOC-2 is flying, MK1.0 FOC is likely to fly before Q1 2016 and Mk2.0 steel should be cut some time this year. Where this Mk1.5 comes from - ADA, HAL, IAF?
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Re: LCA Tejas: News and Discussions

Post by rohitvats »

Well, HAL cannot resist to get a hand in the pie...it proposed Israeli AESA radar and some other stuff on LCA Mk1 to 'overcome' some of the performance issues. Seems to have found a buyer in IAF.

All good if it gets order for 40 more LCA Mk1.5 and keeps the line humming till Mk2 comes on line by 2022.
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Re: LCA Tejas: News and Discussions

Post by Kartik »

So it does appear that the AESA equipped Tejas Mk1 variant will see light of day..as a Mk1A..that is indeed good news if it means that the IAF will place enough orders to continue production till the Mk2 variant enters production. And perhaps at a later stage the MMR/Elta 2032 will get retrofitted with the Elta 2052 to have a common radar baseline for the Mk1 and Mk1A variants.

internal SPJ, AESA and perhaps more maintenance friendly features that may not have found their way on the IOC-2 standard Tejas Mk1. OBOGS too perhaps? Since it was supposed to be ready for fitment on a prototype for testing.

One question for those who may know- is the Tarang RWR on the Mk1 a digital RWR or analog?

And one thing we haven't heard much about, but may perhaps be a feature on the Mk2- sensor fusion..taking inputs from the radar and RWR to paint a single composite picture of the battlefield.
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Re: LCA Tejas: News and Discussions

Post by Indranil »

ramana wrote: However actual control is shown only in flight as the FCS is a hidden variable?
FCS does not add to the maneuverability or agility of a fighter. It lets you fly a fighter which is inherently unstable. The FCS of LCA is fairly simple when compared to Su-30 etc., and quite robust. I have never read or heard of any problems.
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Re: LCA Tejas: News and Discussions

Post by fanne »

True that. Also the canard (pun intended) about canard adding to RCS is nandi dropping. Theoretically yes, but how would drdo know unless it made one and flew it against a group of radars. Theoretical calculations are just that theory. Moreover, to lessen detection by half, one has to decrease RCS by the power of 4 (1/16 th). A loaded LCA with ammunition with or without canard would have marginal RCS difference, irrelevant to war fighting.
If you read between the lines, IAF has been quite critical of the lack of it and attributes shotfall in STR and ITR to this while ADA has been emphatic that that is not the case based on 'theory' and wind tunnel. As Shivji pointed, the only way to know that would have been making one and flying. In day of drones, maybe a scaled down drone can accomplish the same.
Also to be completed for LCA (as science project, different than opertions and FOC)- The spin test has not been done. They have restricted the FCS that LCA does not go that stage at all (same strategy followed by Tornado), the trade off is that LCA may have pushed the flight envelope a little bit more, but it is more conservative now. God forbid, if it gets into spin for any reason, only resort will then be to bail out. Moreover learning there will also help IJT. That trainer will not stall or spin (good for all planes but trainers).
Moreover LCA has same FCS operating on 4 channels with same hardware. It has worked fine, but other planes use different FCS with different hardware and the computer always poll and take the action recommended by the most FCS. This is something that should be worked to make this thing more robust.
Last edited by fanne on 08 Jul 2015 21:40, edited 1 time in total.
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Re: LCA Tejas: News and Discussions

Post by ramana »

fanne, After reading the links by nileshjr and discussion with indranilroy, the LCA compound delta with the FCS makes the canards redundant. I am sure of that now. Problem was the empty weight is higher than the current engine thrust. Hence the the higher thrust engine for Mk2.


I too had read cursory stuff about need for canards as control surfaces etc. After reading those aero papers ADA put in lot of effort early on that concept.


The bugbear is the empty weight for which the engine is being changed.
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Re: LCA Tejas: News and Discussions

Post by fanne »

Well at this point in time, it is a moot point. Even if LCA with canard is better, it does nothing. We needed LCA day before yesterday and right now even a bad LCA (and it is a big IF, most likely LCA is very capable) is better than the 15 squadron of planes that we do not have. LCA mk2 is nothing but LCA MK1 with uttam and internal EW suite, something that LCA should be able to do without any design changes.
AESA needs high power, where would that come from for a supposedly under powered LCA? The weight should not be an issue, as 120kg of dead weight is carried by LCA in the nose.
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Re: LCA Tejas: News and Discussions

Post by ramana »

They could have allocated some of it to the engine we won't be here!!!!
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Re: LCA Tejas: News and Discussions

Post by Indranil »

Please rest the worry in your heads about LCA not having enough STR for want of a canard. Canards are not a one stop shop. NLCA has a Levcon. On paper, in model and on a real airplane. Yet, they are not going with a Levcon on the IAF Mk2 even after a lot of detailed studies. They are not even adding a passive strake like that on the Mirage 2000s/EFs. So lets not worry about things which are not a problem.
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Re: LCA Tejas: News and Discussions

Post by srai »

indranilroy wrote:Please rest the worry in your heads about LCA not having enough STR for want of a canard. Canards are not a one stop shop. NLCA has a Levcon. On paper, in model and on a real airplane. Yet, they are not going with a Levcon on the IAF Mk2 even after a lot of detailed studies. They are not even adding a passive strake like that on the Mirage 2000s/EFs. So lets not worry about things which are not a problem.
Great point! If STR/ITR/AoA were so bad, we would have seen quite a few drastic changes on the airframe, but that hasn't happened. So we can conclude (without knowing real figures) those flight characteristics as demanded by the users have been adequately met with the current airframe design.
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Re: LCA Tejas: News and Discussions

Post by srai »

Anyone seen supersonic external tanks?

These three have been mentioned recently.

Image
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Re: LCA Tejas: News and Discussions

Post by chetak »

fanne wrote:True that. Also the canard (pun intended) about canard adding to RCS is nandi dropping. Theoretically yes, but how would drdo know unless it made one and flew it against a group of radars. Theoretical calculations are just that theory. Moreover, to lessen detection by half, one has to decrease RCS by the power of 4 (1/16 th). A loaded LCA with ammunition with or without canard would have marginal RCS difference, irrelevant to war fighting.
If you read between the lines, IAF has been quite critical of the lack of it and attributes shotfall in STR and ITR to this while ADA has been emphatic that that is not the case based on 'theory' and wind tunnel. As Shivji pointed, the only way to know that would have been making one and flying. In day of drones, maybe a scaled down drone can accomplish the same.
Also to be completed for LCA (as science project, different than opertions and FOC)- The spin test has not been done. They have restricted the FCS that LCA does not go that stage at all (same strategy followed by Tornado), the trade off is that LCA may have pushed the flight envelope a little bit more, but it is more conservative now. God forbid, if it gets into spin for any reason, only resort will then be to bail out. Moreover learning there will also help IJT. That trainer will not stall or spin (good for all planes but trainers).
Moreover LCA has same FCS operating on 4 channels with same hardware. It has worked fine, but other planes use different FCS with different hardware and the computer always poll and take the action recommended by the most FCS. This is something that should be worked to make this thing more robust.
This may become a major issue going forward. It's best to separate channels by incorporating different hardware and software.
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Re: LCA Tejas: News and Discussions

Post by chetak »

ramana wrote:Why don't we map the IAF personnel assigned to LCA from TD phase onwards?


We can clearly identify Cdre. Balaji from IN.

BTW Cdre. is higher than Group Captain but lower than Air Vice Marshal.

In US its equivalent is Rear Admiral Lower Half.

I bet even Squadron Leader ranks from Engineering section (let alone Flying section) were not assigned.
The issue may also be partly connected to the DRDO's unilateral "mapping" of Service ranks with their own hierarchy. This has caused friction on occasion.
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Re: LCA Tejas: News and Discussions

Post by ramana »

India's principal threat in the forth coming years is TSP.


IAF has many types of aircraft to combat the Fizzle ya in air to air mode.
Mirages, Mig-21 Bison upgrades.

The advent of HMDS and advanced WVR have made plane on plane advantage to the first plane that sights the opponent.
So here the plane with minimal front cross section will make it difficult to spot.
However modern turbofan engines have huge inlets compared to turbojets makes them more easier to spot. So one measure of difficulty in spotting would be the frontal cross section of the fuselage (visual/IRST spotting) and including the wings for radar.
Similarly AESA and BVR have made the A2A into a spotting game.
But handicap is once you turn on the plane radar you make your presence known. RWR helps there.
Further for survival in A2A you have IR chaff dispensers for infra red homing missiles and jammers for radar homing.

LCA seems to have all features which will make it hold its own in A2A mode once the Uttam is ready.

Another point from a study of the many A2A combats from WWII to modern days is strength lies in numbers. So need to get as many of the LCAs as soon as possible.

Factors from studies are:
- First bogey spotter. 80% of all combat shot downs were where the fighter never got to use all its fancy capability.
- Out number the opposition with numbers. A larger, maintainable air force (more sorties in air) can withstand attrition, losses and so on to prevail in the end
- Outmaneuver the opponent to gain position. Pilot ability and training. Even IAF Gnats took on all sorts of fancy planes. (Here STR and ITR come into play)
- Once above are achieved reliably shoot down the opponent: guns don't jam, shells have enough oomph to shoot-down the opponent, AAM warheads go off and damage the opposing planes. i.e. have high kill probability.

Top speed is nice but most combat is in the LCA speed regime.

Seeing all this am waiting for Cobham radome and Derby integration.
Gun trials are useful for LRU qualifications.
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Re: LCA Tejas: News and Discussions

Post by ramana »

chetak wrote:
.....
The issue may also be partly connected to the DRDO's unilateral "mapping" of Service ranks with their own hierarchy. This has caused friction on occasion.

Chetak, That is why important to second Engineering duty officers (EDO) for weapon development. They will have rapport with the technical team and can refocus on military needs. And the EDO usually can assess the technical merits of the civilian arguments.
Its when combat personnel are seconded that issues arise.
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Re: LCA Tejas: News and Discussions

Post by ramana »

srai, Why do they have 725 liters and 800 liters tanks? Any special need?

Looks like IAF needs to order quite a few of those drop tanks for LCA for future service use.
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Re: LCA Tejas: News and Discussions

Post by chetak »

ramana wrote:
chetak wrote:
.....
The issue may also be partly connected to the DRDO's unilateral "mapping" of Service ranks with their own hierarchy. This has caused friction on occasion.

Chetak, That is why important to second Engineering duty officers (EDO) for weapon development. They will have rapport with the technical team and can refocus on military needs. And the EDO usually can assess the technical merits of the civilian arguments.
Its when combat personnel are seconded that issues arise.

With the same IIT MTech background, military engg folks may not be happy to report to their juniors in age, experience and domain knowledge.

Combat arms folks are easy. You piss them off only once and that too at your peril. Where do you draw the line?? All IN folks are combatants, bar none. A war ship does not sail into battle with "non combatants".
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Re: LCA Tejas: News and Discussions

Post by ramana »

Chetak is this a new thing? The IN MTech folks in my time were very eager to learn and interacted with us on even keel even though we were younger.
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Re: LCA Tejas: News and Discussions

Post by chetak »

ramana wrote:Chetak is this a new thing? The IN MTech folks in my time were very eager to learn and interacted with us on even keel even though we were younger.
This is not a new thing at all. It has existed right from the beginning and even during Dr Paulraj's days. Interaction is one thing. One can interact even with a hand cart puller. Reporting is another thing all together and who writes the ACR is important. Don't make anything more out of this than what is being stated.

This is applicable across all services and not just any one service or "combat arm". Hierarchy is important in Govt service. After the debacle and the babu perfidy in the pay commissions, this has become embarrassing and many organisations have taken undue advantage of it.
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Re: LCA Tejas: News and Discussions

Post by deejay »

^^^ + 100 to that. Services have drawn the short end of stick.
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Re: LCA Tejas: News and Discussions

Post by chetak »

deejay wrote:^^^ + 100 to that. Services have drawn the short end of stick.
various services have pushed back in their own ways. Not seconding folks may just be one part of it.
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Re: LCA Tejas: News and Discussions

Post by ramana »

Ok. Understood.
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Re: LCA Tejas: News and Discussions

Post by Indranil »

fanne wrote: Also to be completed for LCA (as science project, different than opertions and FOC)- The spin test has not been done. They have restricted the FCS that LCA does not go that stage at all (same strategy followed by Tornado), the trade off is that LCA may have pushed the flight envelope a little bit more, but it is more conservative now. God forbid, if it gets into spin for any reason, only resort will then be to bail out. Moreover learning there will also help IJT. That trainer will not stall or spin (good for all planes but trainers).
Unfortunately, you have got your facts mixed up and ended up confused. I am replying only to clear away the misconception that you have spread.

1. ADA had determined that after LCA departs, it is very unlikely that a human can retrieve the plane. Also, there are big financial costs involved to finish that kind of testing. Therefore, they decided that the FCS should be designed to limit LCA from entering an unrecoverable state. This is nothing new. The majority of FCS are coded this way to limit risk and cost. All such FCS factor in a safety margin.

2. The ITR of lightly loaded delta wing fighters is never in question. So, LCA will not have a problem with that. At 26 degree AoA, a light plane like LCA with a huge wing will be turning really fast. The problem is not that at all. Turning that fast comes at the cost of energy, and soon LCA would have to lower its nose and settle into a sustained turn. Unfortunately, in this region, LCA is not doing as well as one had hoped for. This is because the drag is too much for the 84 kN engine to overcome. Adding a canard, or changing the FCS does not affect this condition. In fact adding a canard would worsen the situation (add weight and wet area). They have to lower the drag, and increase the thrust. You can see that is exactly what they are doing.

3. You assumed that spin test are not done. Not true. They had planned to go for high AoA tests with a spin-chute, i.e. if LCA did depart, and entered a flat spin, then the plane can be recovered using the chute. Now, it has been published many times that the high AoA tests have been completed, without the chutes. This means that the pilots had sufficient confidence in the plane to approach this tests without a spin-chute.

4. IJT and LCA are completely different. IJT is a statically stable plane. Its spin problems are very different in nature from an statically unstable plane like LCA. Therefore lessons from one cannot be applied to another.
deejay
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Re: LCA Tejas: News and Discussions

Post by deejay »

^^^ Is there any Delta design which has been spun successfully.? (sorry for OT)
Abhibhushan
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Re: LCA Tejas: News and Discussions

Post by Abhibhushan »

Is there any Delta design which has been spun successfully.? (sorry for OT)
Yes Deejay, The MiG21 specially the earlier models like type74, type 66, type77 could be intentionally spun, though the were not cleared for doing so by the average pilot. However, the exercise was straightforward. Loss of height in the process was substantial. Some of us demonstrated a spin to young MiG 21 pilots but did not ask them to practice it on their own.
ramana
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Re: LCA Tejas: News and Discussions

Post by ramana »

Abhibhushan, As you know the Mig-21 had horizontal stabilizers that helped.
The LCA is tailless delta.
So different animal.

I guess you are IAF fighter stream?
fanne
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Re: LCA Tejas: News and Discussions

Post by fanne »

Indranil, point 1 is same as what I am saying. For point 2, a stable delta like mirage 3 will will get into a turn with nose down and Musharraf up, where by killing lift (apart from any draggy design or low engine power). The whole point of static instability of Lca or mirage 2000 was that they go in turn with nose up ( watch all the videos). But the other point stands, due to g limitation speed comes down, lift gets killed, draggy design does not help and Lower thrust engine further kills it. Mk 2 addresses these. Increases in length is to decrease that drag (there is a graph that shows sudden increase in drag vs l).
On point 3, I have not reAd or interpreted the way you have. My take was that the general push for turning angle was done (without spin coming into picture). There could be news, if you have read that explicitly states that. Point 4 is well taken, but a better understanding of claw around spin will help here.
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