Anybody here remember the EL/M-2052 AESA radar? The specs it was advertised with were mind-blowing. I vividly remember the line about being able to detect upto 64 targets. If it was really as good as it was claimed it’s a great shame no one bought it or developed it further.
Got this one from T-50 Facebook page..
If you ask me the bomb bay could be made larger by increasing the space between the air intakes/engines. Don’t the Flanker and Fullback have a wider ‘cavity’ in the centre?
In general the weapons bay needs more space to accommodate the wide range of Russian A2G missiles.
Thanks everyone. Cleared most of the doubts I had. One thing: What kind of IEP systems are there? The system on the Type 45 and the CVF simpy uses CODAG with the diesels and gas turbines linked to generators instead of propellor shafts. Is there a system that uses only generators, with no prime mover?
witcha, for all of Teer’s harsh comments, you do come across as quite ill informed on the subject and what’s worse, very opinionated. don’t take it otherwise, I do think you mean well but when divorced from ground reality that doesn’t mean much.
And in what sense is he aware of the ground realities? What does he know about me or what I know and don’t know? He pompously comes off displaying himself like some great expert lecturing his lessers when the only evidence he’s shown of knowing jack about aerospace is building RC planes. I have especial dislike for people who use that tone of argument.
take the GTRE funding comment for example, it doesn’t matter if it is large by Indian standards because what it tried to develop was not possible entirely with Indian subsystems, foreign systems had to be there, in large amounts as well and that doesn’t come at Indian prices.
ISRO has, is and will continue developing and building advanced rocket engines and other advanced items at a total budget that would put every other space agency in the world to shame irrespective of whether people like you and Teer regard it as impossible. Same for the people behind our missile programs. Same for LRDE, DARE, C-DAC and a dozen-off other institutions. By your logic they should have developed nothing with their budgets. But they succeeded, because an inescapable fact is that Indian labour and materials cost far less than in the West, and that we have many researchers who are capable of and have the will to stretch the buck. So arguing that GTRE needs the same funding as General Electric or Snecma isn’t going to get much sympathy from me, because all it would take is the right talent and ingenuity to do the same with less, which GTRE largely couldn’t.
No doubt the esteemed Teer will respond by re-posting variants of the same above general points I’ve read about a hundred times on a dozen forums accompanied by some more snark ‘Im Senior & superior, U know nothing’ comments designed to impress onlookers. Nor do I care to hear it.
The bulk of Teer’s reply was ‘You don’t know anything because I say so, everything you say is irrelevant.’ Whatever (vaguely) informative points he imparts are drowned out by the oozing condescention and ‘Hmph! Young whippersnapper! I’m an expert!’ attitude.
I’ll only answer this: if your argument against awarding the private sector any contracts is that they have never been awarded contracts before, it’s a broken argument. Some degree of charity is required in distributing this contracts if one wants to develop capabilities in competing organisations.
And this: subcontracting small components here and there isn’t going to do much to develop private expertise in developing and integrating full-fledged products.
Does anyone have a relative size comparison of the Su-34 versus the Flanker? Seeing the huge size of the cockpit one would think it at least twice as big, but they share the same airframe and engine family.
US COGAG cruisers have an embarrassingly short range compared to CODAG/CODLAG/IEP-equipped European designs. Again, are diesels quieter than gas turbines or is their only advantage fuel economy?
Yes. In fact, one of the most interesting recent propulsion ideas is the one proposed by DCNS for its FM400 frigates. It’s beautiful in its simplicity – 2 cheap slow speed commercial diesels each driving a shaft (up to 23kts), plus a waterjet driven either by a high speed military diesel (25kts) or a gas turbine (29kts). Maximal use of commercial components plus no complex reduction gear.
Interesting design. Is it CODAG or CODOG?
And HAL’s engine unit deserves more credit. By virtue of having built various engine designs over the decades they have accumulated design documentation and knowledge on their working. They rebuilt the RD-33 engines of the IAF MiG-29 fleet and developed a new fuel pump for the MiG-21’s R25 without any Russian assistance. They posess more designing skill than you think.
This cant get more idiotic !
Again, Gas Turbine engines for Fighter A/c are not exactly simple lego building blocks engineering, where in you hire a bunch of people who have no experience in this field, give them money and say that we want a “FLAT Rated Gas Turbine engine in the 80-85 kN class pronto” ..GTRE has the K9 prototype which will begin flight trials shortly on board an IL-76 , and once that is completed, its slated to be mated with Tejas PV-1 which would be great.
And looking at this Video, it doesnt seem that the Kaveri program is a failure as such .. !
“We never delivered before so you can’t expect us to deliver ever!” is a broken argument. Firstly when the Kaveri program started the GTRE wasn’t a bunch of fresh-faced amateurs scratching their heads and wondering ‘How does a jet engine work? We first need to learn ABC from textbooks.’ They already had experience with earlier-generation jet engines like the Orpheus(which they widely experimented upon and upgraded) along with documentation on various Soviet engines used in HAL-build MiGs. Even so they were given 20+ years and Rs.3000+ crores for developing the engine. And even so the result is unsatisfactory. BTW even after integration with Tejas it’ll still need thousands of hours of testing, and even after that the results still need to match the performance targets, which at this stage it won’t. Shiny static test videos don’t show anything.
For the time being, since the Kaveri program is delinked form the LCA, there IS no impact on the LCA-Tejas or on National security as the Tejas is flying and proceeding with the GE F404 interim measure ….
As the IAF accused some time back, even if it is officially ‘de-linked’ the GTRE won’t give up lobbying for acceptance even if it delays the LCA, which is what is happening with the failure to select a new engine for Mk.2 due to protests from the GTRE/Snecma entente.
And regarding a “JV” with a foreign partner, and the proposed GTRE-Snecma tie up, the IAF was quick to notice that the GTRE wont be absorbing CORE technology in that tie up as the French are proposing to use the M88 core.
It may come up with a useable engine for the LCA-mkII and/or the AMCA, however, the core will still be FOREIGN !
And what they want instead is a 100% foreign engine, because they realise expecting GTRE to deliver indigenous product within a reasonable timeframe is futile.
Once the Kaveri is done with matching LCAs specs, I say, only GTRE should be tasked with coming up with an Engine for Tejas MKII and AMCA.
Even if they take time and cannot meet the requirement for Tejas MKII, its okay since that can be fulfilled by the GE or Eurojet engine…
Right. Allow them to ‘take time’ and delay the mk.II by another five years, then choose the Eurojet, by which GTRE will partner up with Pratt & Whitney and offer an even better Kaveri!:rolleyes:
However, that will ensure that once its ready, India would have achieved true indigenisation in Gas turbine tech and then suitably equip its fighters …
As far as I and the IAF are concerned, the GTRE can take its sweet time achieving indigenisation in Gas Turbine tech so long as it remains far away from the LCA.
Gas = Excellent acceleration, compact
Diesel = Efficient for cruise (medium-high RPMs), simple intake/exhaust requirements
Electric = Silent, efficient at low RPMs
IEP = More damage resistant & more design freedom (can locate diesel/gas generators anywhere)These days diesel-electric is almost mandatory for ASW combatants and OPVs. Moreover gas is required for ASW (for sprints). AAW and GP combatants, as well as amphibs/logistics ships, are the only ones that can get away with diesel-only propulsion
I don’t know; the US, Russia, China and India, among others, seem to have no problem using CODAG/CODOG and COGAG for ASW vessels. About gas turbines, are they quieter than diesels or noisier?
Does China have any intention to develop a ‘true’ bomber in the vein of the Tu-22M and Tu-160 to replace their current fleet of H-6 Badgers?
2. Time to market from development to production to distribution is important in the success of any product. If we expect the private players to do indigenous development, I guess we may be asking too much. As a share holder of a company I may look for some quick bucks than waiting too long a term for return as competition would mean no guaranteed success. That is a huge risk considering the fact that their are few private sector companies with such deep pockets. So their route would be a JV with an established foreign firm as suggested by Matt which would lead to the fact that there is a level of dependency to a foreign firm. And now would it be acceptable?
Considering GTRE’s dependency on Snecma to fulfil the IAF’s needs, I’d say yes. As for private R & D, I agree there are few firms willing to put in that level of effort. But there are such firms. Tata, Mahindra, Wipro, L & T, and so on are heavily involved as subcontractors in various DRDO projects and are pretty eager to enter full-scale defence production. I should think they’re prepared for the R & D part with that level of enthusiasm. Kirloskar developed generators just for Indian Navy ships, I think they may be coaxed into jet turbine design if the government gave them incentive to do so.
3. There is a difference between scientist, engineer, and a production team[what would be the word for that:o]. I guess that would be the reason why HALs unit has not yet moved to engine development.
But having experience with materials and manufacturing processes is crucial to developing and testing engines. It would not be too difficult for the HAL engine unit to start up an R & D centre and hire scientists.
On a couple of the points
(iii)Lack of availability of test facilities in the country necessitating testing abroad.
When their budget was revised from Rs.300cr to Rs.2873cr shouldn’t they have asked for testing facilities? ISRO has advanced wind tunnel facilities so it can’t be difficult to build.
(iv)Lack of availability of critical equipment & materials and denial of technologies by the technologically advanced countries.
Can’t take this point very seriously. The sanctions that would block such ToT were only imposed in the late 90s, and that too only by the US & UK(Among jet engine manufacturers). They always had the option of going to Klimov/Salyut/NPO Saturn and Snecma. I have a feeling this point was added to gain sympathy from the perception of evil Western sanctions.
(v) Non availability of skilled/technically specialized manpower.
There was a bit on the BRF forums. Apparently GTRE failed to attract professionals skilled in engine/turbine design and had to make do with inexperienced staff. If so part of the blame lies with them for not using their vast research grants to contract the necessary expertise.
And you really CANT diss a whole organization if some person was guilty of corruption ! 😮
There have been cases of corruption in the IAF/IA/IN too .. I’m sure you wont advocate disbanding them … would you ? :confused:
I’m ‘dissing’ the GTRE based on their unacceptable 50-year record, along with the suspicion that corruption born from lack of accountability had a significant role to play in it.
If the only argument to let GTRE go on with their pet projects indefinitely is that there is no alternative, then it is a poor argument. Why can’t the government fund feasibility studies and start-ups from private engine-makers like Tata & Kirloskar? Why can’t HAL’s engine division graduate from license-building foreign engines to starting R & D on its own designs?
Yep … very much in the “behind” of history ! 😀
@Witcha : In view of your constant criticism of GTRE, i would like to remind you that there are NOT many countries who manufacture JET Engines !
If throwing loads of monies was all it took, every country in this world would be churning out engines !for GTRE to have come up with Kaveri which meets about ~90 % of LCAs requirement is itself a feat, coming from a country where we dont even have indigenous manufacturing of automotive engines !
There was a long and detailed discussion on the Kaveri engine specs and claims in Bharat Rakshak long ago. I don’t entirely remember or understand all the technical details that I read, but the gist of was that thrust alone doesn’t prove the engine’s performance. Among others, there are factors like angle-of-attack rates, fuel consumption figures and so on that will require a lot more testing to prove. BTW all versions of the engine together have only been tested for 1700-2000 hours so far when an engine should be tested for the duration of its operation life(3000 hrs in this case).
And keep in mind the current version of Kaveri has dumped the Kabini core and uses the Snecma M88 core intead. How much of this was GTRE’s effort? Pardon me if I’m leery of the GTRE’s sincerity after reading articles like this.
http://news.oneindia.in/2007/01/11/cbi-seizes-assets-and-cash-of-rs5818-lakhs-from-gtre-official-1168502950.html
This was a C-grade technical officer, a relatively low rank. If he could get away with looting this much research funding then imagine how much wealthier higher officials must be getting off the taxpayer. This is what happens when the government keeps writing blank cheques for every budget increase request instead of considering the progress made.