ACM believes the same too. Wonder if his beliefs are wrong.
if ACM was beleiving like you he would not be inducting 2 squadrons of LCA mark 1 which he beleives is a Mig 21++ and which it was to replace.
That's nothing. We just added equipment to existing ports. When you buy a new graphics card and attach it to your motherboard, do you call that
integration? I am talking about designing and developing the entire architecture of the motherboard and then attaching equipment to it. Huge difference.
that is because you are ignorant of how the darin upgrade happened. it was not just adding hardware to the motherboard. it was done on the MIL 1553B databus
- a first on Jaguar anywhere in the world and which was later adopted by others!!
go thro' this from the man who led the DARIN team himself -
It was our recommendation that we would build a system with an open architecture connected by a Mil-Std 1553B Bus with redundancy.
Some eyebrows were raised by our choice of Mil-Std 1553B as the Bus as the protocol was a brand new protocol and no aircraft in the whole world had
attempted to work a system on it.
It needs to be emphasized that the Indian jaguar was the first weapon system in the whole world to adopt the MIL-STD-1553B data bus protocol. It was
also one of the first weapon systems to adopt a truly open architecture where not only the computers and displays but also the sensors and control panels all
communicated with each other through a data bus. One could whip in or out any sensor or display or computer or control panel on the system. As long as
the format of data interchange was maintained there would be no problem.
He asked me whether it was a fact that no aircraft in the world had so far used the MIL-STD-1553B bus. I affirmed. He then asked whether it was true
that the continuation of the Jaguar production line was dependent on the successful timely completion of the integration task. I said yes. He then asked
me whether it was true that no one in India had ever undertaken a task similar to what I had just undertaken. I said probably yes. He then asked me
whether it was true that all the varied vendors we had selected had never worked together before. I said yes. The he asked his last question. You
still want to do this job all by yourself? He said. Yes, I said and we shall do it too. All the best of luck Air Commodore, he said. I thanked him and
closed the meeting. I certainly needed a lot of luck.
As soon as the vendor contracts were signed, the tempo of IIO's work became higher. We concentrated on a few specific segments.
Creation of a mock-up for physical integration
Creation of a static and then a dynamic rig to put the system together.
Creation of an exhaustive flight instrumentation requirement, setting pass / fail targets for component level acceptance, setting pass / fail targets for
system level acceptance.
Making sure that an instrumented air range would be available in good time for the flight trials (which were many months into the future at that time).
Ensuring that system design authority remained firmly in our hands.
Hammering out detailed procedures to ensure that there were no conflicts of legal nature or of safety in structural nature in sharing designing authority
between BAe, HAL and IIO
Creation of an infrastructure that allowed us to monitor the day to day progress on the development of each component reliably.
Organizing a system where the certification / documentation / verification of the INAS related work could be handled through the CRE / CRI reps.
Keeping an eye on the budget
Creation of operations manuals and technical manuals for the system.
http://tkstales.wordpress.com/2010/03/07/the-darin-story/
huge difference!! unlike your worthless comment denigrating any indian effort.
In 2010 IAF claimed a 50% obsolescence in IAF(only MKI, M-2000, Bison, Mig-29 and upgraded Jags being certifiable). By 2015 IAF claims 20%
obsolescence, LCA adds to the figures even after the above aircraft are nearly phased out. Only Jaguars and LCAs will be our obsolete aircraft by 2018. Even
Jaguars will start being phased out by then.
After 2025, LCA will be our only obsolete aircraft with the other aircraft being FGFA, MKI, MMRCA and AMCA. Early retirement anyone.
advise the ACM about it ASAP.
If IAF inducts aircraft, the number of engines imported is usually twice the number. With 230 MKIs it was 920 engines and 600 Honeywell engines for
Jags. So 200 F-414s for LCA sounds just about right for 100 Mk2 or 83 in service aircraft and X number of test prototypes.
hello??
for the Mig 29 (60+) upgrade the contract signed for RD 33 S3 is for 20 off the shelf and 120 HAL licence manufacture!! where is it double or trible that you
are trying to imply??
http://www.domain-b.com/defence/def_prod/20090822_rd-33_series-3_engines_2.html
going by your logic C-17 should be getting 40 or 80 extra engines!!! but do you know it is only 5?? that is how it is. normally 10-15% is the reserve.
That's why the Mk1 production was capped at 40 aircraft. IAF wants 83 Mk2 and even that will reduce as time passes.
nothing confirmed. 123 anyway is not small. equals MMRCA.
According to the plan, LCA was supposed to fly for the first time in 1990, 1996, 1999 and finally 2001. Don't you see what's wrong?
plans can be anything. FSE funding only happened in apr 1993. you can't expect it to fly in 1990/96. 1999 was possible but for the FBW story!!
A triplex channel sends 3 signals from source to destination. A Quadruplex channel takes the average voltage of a triplex channel and then sends it
along with the other 3 channels.
A Quadruplex channel is also a Triplex channel at the source but ends with 4 channels at the destination just to increase redundancy.
correct but the point is as you said "increase redundancy". safety.
The Gripen's FBW would be more advanced in coding and quality even if we have a more pretty sounding FBW system. Let's not forget the amount of
modifications it has gone through.
did you do the coding for the SAAB?? lol. hillarious.
Haha! We did not develop it from scratch. We only integrated it by ourselves. BaE and then LM helped develop it. It means the senior scientists at LM
and BaE explain how everything needs to be done and then help design the architecture. Then they gave their equipment to simulate it and then gave us a
helping hand in developing it fully. Once done we tested nukes and got kicked out. Only integration work left, we took 3 years and voila.
when your modules are confiscated and you are thrown out what else does it mean other than doing it from the top?? and it is obvious ADE guys could do it
because of their experience with BAE but the fact that we now have FBW tech independantly without any interference from the outside is fact of life.
Even if we do half of what they did, it would be awesome. Heck they achieved supercruise with a clean load on a Technology Demonstrator.
whether we do it or not is moot. you did not answer my question wrt super duper NG SUPERCRUISE!!! better answer it instead of moving off in a tangent.
i am used to this 'chant' for 16 days now!!! make it your signature on your profile instead of repeating it again. saves both ours time.
Huh! Overall specs push the Gripen forward simply because it is indeed better than LCA Mk1.
again used to this now.
You are confused. Link 16(ODL) and net centricity is one and the same. We don't have ODL to finish IACCS. We will get deliveries of an ODL as capable
as Link 22 from Israel only a year from now. What we did with fibre optics only recently, PAF did some 4 or 5 years ago.
Their new F-16s are already connected to their AWACS. Their JF-17 will also have Link 16 and their AWACS are already connected to their ground radars using
ODL.
everybody knows that. i asked you specifically when did PAF network their assets - both ground and airborne - for their IACCS to be functional??
JF 17 has at present chinese systems on board. they have to be compatible for the link 16 - i don't think they are.
As of today even our MKIs need voice commands from our Phalcons because our ODL is still not operational.
they have datalinks but are crappy. hopefully indian ODLs will take their place.
The USAF know everything about El/M 8222 and their own Jammers are ancient. Heck ours is a more advanced version of their legacy Jammers. The jamming
environment is too much for LCA to compete in.
irrspective of who has the superior jammers, i don't expect them to use them to full potential in an 'exercise' for obvious reasons. the results of cope
india was the case WVR and tactics employed around it.
The scenario I posted is one of the many scenarios played out during CI-2004. It was a WVR scenario where the M-2000 and Su-30 were already merged
while Bison took pot shots from a range of 15 to 20 km using R-77s.
which is why i said it shows badly on the US insistence on BVR. the importance of WVR is still there and tactics have to be evolved around it while the BVR
missiles mature for the future to make BVR combat more significant.
besides IAF had numbers on their side.
AWACS is not guaranteed to be present always. USAF pilots do exercises in difficult conditions even without AWACS support.
just to learn and evolve tactics for the same. this is exactly the reason for the exercises.
Their second best was equal or better than our best at the time. We employed the Mkk.
ofcourse.
The LCA is obsolete already. They will only employ existing Bison tactics.
you should advise the ACM immediately.
If you exceed the time limit of your ability to fight in WVR then you cannot run away. A bigger aircraft can enter and leave a fight at whim. If it
can keep the LCA occupied for some time and then merge the LCA will not be able to run away with its speed.
In conditions where the LCA's presence is very important, eg if the LCA is protecting a base. Then the bigger aircraft only has to wait for the LCA to
exhaust its fuel supply before engaging it. So, the enemy has a kill as well as bombs the base.
same applies to any similar fighter. how does a Mig 21 Bison has an advantage in this considering it has even less loiter time and a crappy engine with high
SFC and a crappy load?? speed alone does not dictate terms.. tactics are!!! every aircraft being a compromise due to their design - tactics are evolved for
the role they play.
You are still hung up on specs.
because i beleive in facts rather than fiction.
The MKI has enough fuel to last 30 minutes in a dog fight. The LCA has only 5 minutes to make a kill or get away. This was great in 1996. Now it's
just a waste of time.
if PAKFA has more time than SU 30MKI. so?? different aircrafts built for different purpose. which is why i say compare to a similar ones. will Gripen C will
have more time?? will Mig 21Bison will have more time??
i think next you will compare LCA to B-2!!
grow up.
Super Hornet can spit out nearly 80KW for avionics. MKI gives out nearly a 100KW. LCA will be lucky to give out 10KW.
how much SH or MKI spit out is moot. i repeat what reserve power they have. besides your figures are wrong.
EA 18G is the very example.
EA-18G is a bigger aircraft. SH and EA-18G are the same except for avionics and payload.
EA 18G is for electronic attack. IOW most of it's power is dedicated for jammers and other sensors. while SH is like any other fighter.
You can't have that on LCA. 85KN is too less. Heck F-35 spits out 191KN which is almost the same as a SH. So, it can spit out more power.
The MKI and F-15, which are bigger aircraft can spit out even more power than SH or F-35. Obvious.
The Mig-29 being a bigger aircraft can also pit out more power than the LCA.
again you are missing the point. small is not the issue. LCA's empty weight is less, it carries less load and less internal fuel unlike the bigger aircrfats
- meaning it does not need the same power as the bigger fighters. the power optimisation is done accordingly.
Flankers were always a delta. But with bigger tails instead of a single fin.
take a good look at it. does it look like a delta to you??
No. You are confusing the terms. Payload is different from Loaded weight. Loaded means weight coming from fuel and weapons, let's not forget the
weight of the pilot as well. Payload is the amount of load you can carry externally. This is also called the Useful Load.
The useful load on the Rafale is 9.5 tons, Flanker is 8 tons, GripenC/D is 5 tons, Ef-2000 is 6.5 tons, SH is 8 tons and LCA Mk1(IOC) is 2 tons. LCA Mk1(FOC)
= unknown but on paper its 4 tons.
your nitpick aside, the larger point was about the engine power supporting an aircraft and the mission.
PAKFA is a trapezoidal design similar to F-22. Not a delta.
PAKFA's useful weight is 8 tons and fuel load is 11 tons. At 19 tons, the plane would achieve MTOW. With half the figures it would be called Combat load. Get
the terminologies right.
Payload is stuff you carry on the hardpoints.
ok my bad on the "trapezoidal".
as to the rest i don't know why are you saying the obvious. my answer was simply wrt your point - PAKFA being smaller than the MKI has a higher range. my
answer was PAKFA has more internal fuel. that's all.
and before i get my 'terminlogies' right tell me what is "useful weight"??
Only A2A equipped fighters with jammers will engage the LCA on our territory. So, all what you said is not affected.
irrespective of the territory, i think that would be the better option.
You just lose a point and then start nitpicking.
If I am the aggressor I will send out a lot of aircraft which are capable of both A2A as well as A2G. I will make sure my A2A will be the one engaging your
LCA. My A2A aircraft are, say, Mig-29smt against your LCA Mk1. My aircraft is bigger and carries a bigger jammer while LCA will only attempt to engage the
A2G fighters since shooting them down will end the mission.
My A2G aircraft are not in the engagement zone for obvious reasons while my Migs are fast approaching your LCA. Wonder who wins?
ok. you are speaking of the jammer advantage.
LCA has MTOW of 13500kg (some feel it is 14500kg now) - 2500kg (internal fuel) - 100kg (pilot weight) - 6500kg (empty weight) gives me a useful load of
4400kg. now i won't be putting that for obvious reasons.
this is what it would be -
R-77s - 4x175kg = 700kg and R-73 - 2x105 = 210. total = 910kg!!
that would be the A2A config for the LCA mark 1 if it takes on Mig 29 or any other fighter. so just as the Mig 29, LCA too would have the reserve power for
the jammer!!! meaning equal advantage. however LCA because of it's delta design would not get into WVR. it would engage only in the BVR regime as per the
tactic.only in WVR Mig-29s will get the advantage which is why LCA will not get in to that.
TACTICS.
however i agree LCA mark 1 needs a higher thrust engine.
Get the terminologies right. The F-22 is 2 or 3 times bigger than LCA and still has a RCS significantly smaller. The B-2 is massive and I bet even
it's RCS is smaller. Stealth has nothing to do with size it is all to do with design. Get that right first.
tell me if an F22 is built in LCA dimensions it's RCS will be less than a normal F22 or same??
You are getting OEM noises stuck in your head. Just because LCA is small does not mean LO. Even wooden gliders can be picked up on radar.
i repeat LO/VLO are terms associated with Radar Reflections. normally since 5th gen fighters are specifically designed for LO/VLO people associate the terms
to 5th gen. IMO that is not true.
That's why LCA Mk2 is a more viable option compared to the obsolete LCA Mk1. This is why I am claiming LCA Mk1's second squadron was forced on them.
If given an option I am sure IAF will cancel the Mk1 induction all together.
no doubt LCA mark 2 would be a lot more capable but Mark 1 is still better than the existing Mig 21Bisons. they can replace them.
This Light and Medium difference is not defined any more. It's probably just to shut the media up.
whether one defines them as such or not, they are there. also the lighter ones are more cost friendly and their turn around times are much less besides you
don't need a heavier ones where a lighter one can do the job.
good.
That's why the terms LO and VLO are associated with 5th gen aircraft. Did you not notice the way I pulled you down just now.
i explained it earlier.
I gave you specs suggesting smaller aircraft like Surya Kirans with clean loads were picked up by LCA's radar from 100km. You were very happy with
that info, claiming "it's Great." So, what makes you think LCA, a bigger aircraft is suddenly LO?
a fighter aircraft needs to carry a decent enough load to be of any use in combat. LCA sort of fighters are the minimum one could ask for - unless you want
only the cannons to be on.
LO is a relative term. wrt an aircraft with an RCS of 5m2 an aircraft with an RCS of '3m2/1m2' is LO relative to 'those two fighters'.
F-15s, MKIs, F-16s and J-10s will be eating aircraft like LCA for breakfast in a mano a mano.
you were bragging about Mig 21 KILLS in the cope india exercise??
It does not compare to any aircraft and that's why it shouldn't be inducted at all.
but it is being inducted!!
Knirti SAP 14. It's the Russian equivalent of the American Al/Q 99E. Also the Knitri SAP-518 jammer. Both are massive and was first displayed attached
to the Su-30MKI model at MAKS 2009.
SAP 14 is carried on the centreline while SAP-518 are on wingtips.
ohhhh!! there was one photo on one SU 30M ages back. does not mean we get them. even FGFA is supposed to have indian EW.
russians are behind in electronics. i doubt it.
any specs for these???
Doubt that's happening. Did you not see our ACM?
The plan was 7 squadrons of Mk1. Later the plan became 2 squadrons of Mk1 and 5 squadrons of Mk2. Numbers have been reduced from 100 to 83. The more the
delay the smaller the numbers.
there is only a livefist article. true or not nobody knows. lets wait and see.
It is official. ADA announced it during IOC function. IAF wants 83 and those are the last figures from IAF.
i did not see this at all when i saw the IOC function on tv. neither have i seen any other report other than the livefist. infact if the LCA mark 2
supposedly is a different aircraft with bigger wings/more internal fuel/more hard points/aesa/high thrust engine - then we may see MMRCA capped at 126 and
more LCA mark 2 ordered!!!
we need to wait.
It's not always. But I gave it as an example. An aircraft that claimed 140:0 kill ratio just got shot in the azz with a radar lock. It's a HUGE deal,
the Growler achieved radar lock on Raptor.
it is good no doubt. the whole purpose of the american simulated exercises is to find weaknesses in F 22 and fix it. i don't see it happeneing often.
Huh! What's that go to do with the fact that Gripen surpassed Mirage-2000?
the question was about sustained AOA of Gripen. not what surpassed what!! besides still you have not proven that gripen C surpassed Mirage 2000. all you have
been saying is "it surpassed".
It's not a one off incident. Pilots always do that for unpredictability. Turning off FBW is done by experienced pilots.
experienced or not there is something called human endurance.
it is one off incident because a normal pilot can't take more than 11g beyond which they will lose consciousness. but few pilots like the one satish
mentioned can take more momentarily and during that moment he may have managed that kill.
IAF does not need Mk1 anymore. Even Mk2 could end up getting the short stick in 3 or 4 years. But we don't know that. But we can be sure the Mk1 got
the short stick.
but mark 1 even in its present avatar can easily replace Mig 21s including the Bisons. ofcourse IAF wants high thrust engine on the LCA. let's wait on LCA
mark 2.
Nothing to twist. You asked for fact based analysis. Here's an interesting one. Go to A-11 on the first day or the second day and go to Saab. Ask him
how would the LCA fare against GripenC/D? Then come back and give me a "link" about what you learned from him. I won't believe you unless you provide a link.
If you go after the business days then its no use.
i have neither the time nor do i stay in B'lore.
Ok. Then the only alternative to my statement is we are better than Western OEMs.
i never claimed that but that would be correct wrt Gripen C.
Stopping spares supply for 4 weeks is no big deal. It takes that long for us to get it anyway.
you are justifying somebody screwing us in a war!!!
Can you give me detail on war reserves saying IAF aircraft will be badly affected as soon as OEM stops supply within the first week? This was your
assertion so back it up.
as if you have backed up any of your assertions!!!
i said may be Ray sir/Kunal sir can throw more light on this. IIRC i read long back, can't reacall where, which spoke of this war reserve to be about 1 - 2
months. if i get that link i would be happy to give you.
My contradiction is LCA is a fail. ACM said on National Television that LCA is a fail. Best of luck.
fine. keep to your beleif.
If we fix a more powerful engine on a small aircraft without changing fuel load, the aircraft will be an even bigger fail than the first model.
not in the case of LCA mark 1. even if you stick a higher thrust engine of say 100-110kn the point you are making does not happen. there is a lot of scope.
You are short sighted if you believe an airframe enhancing part is useless when it pitches up. Now you will ask me to back this statement up and then
you will say I am providing only fictional rhetoric. For the above "brilliant" statement I am ending this discussion simply because you don't know **** about
aerodynamics.
oh mr. aerodynamics, heard of "form drag??". i guess you have not - looking at your silly answer.
let me illustrate. take a plywood sheet in your hand
1. hold it horizontally relative to the earth and slice it thro' the air in one forward motion. (that was smooth i guess)
2. now incline the sheet at 30degrees and repeat the action. (it may not have been as smooth..)
3. now incline it at 60degrees and repeat. (worse than last time??)
4. now incline to 90degress and repeat. (ouch.. this was the worst)
now get it?? btw in all 4 situations the drag was there but you felt more as you moved from 1 to 4.
so why a canard?? because the advantage of a canard wrt to maneurability is a bigger gain than the drag factor. an aircraft - by any design - is a
compromise. it is not perfect for all situations and hence you compromise on some parameters for a bigger gain on some other parameters. as long as it suits
one's requirement it does not matter. simple.
any external element to an aircraft brings in the drag factor!!! period. even pylons have to be designed for low form drag and so are the external pods. in
AOA even the wings are a big drag factor. this is even more felt in delta wings. canard is no different. they are but small wings!!!
Read up a bit more, learn more about terminologies and how each aerodynamic aspect affects the other and then come back. By then you won't be asking
such stupid questions.
who is being stupid??
You will never be happy with anybody who goes against your view points.
as if you are any different.
atleast i am sticking to facts while all you have been doing is passing off your fiction as fact.
..........
Did you not see the post where I asked for the full video of the speech as well as the interview?
Anyway in the link I provided, ACM compares LCA Mk2 with Gripen NG saying Gripen will be better.
Do you have the Mig-21++ video as well?
Or anything that puts the actual comment in quote?
Perhaps a video which sees him quoting this"This means first in endurance, second in performance, third in load carrying, fourth is the number of weapons it
can deliver. Fifth is the weight with which it can navigate with and the vintage of the aircraft or avionics and sixth is radar."
Let's not forget Mk1 will still not clear ASR and production has been capped to 2 squadrons.
i told you earlier beleive what you want to. makes no difference to me.