That is the point, they have not Expanded flight envelope, contrary to your varying combinations hypothesis.
The above can be rephrased as HAL has broadened the flight envelop, but is yet to progress it further.
What were the 400 flights were? Joy rides!!! or as the Air Marshel puts it :
The retired Marshall (not connected to Tejas programme at any time), is quoting generally only. The media report directly doesn’t say that Tejas has performed many tests. It inserted his general statement to imply an incorrect fact.
In other words, note that neither the report nor the respected Air Marshall directly say, “The Tejas has been only taking off and landing since 400 tests”.
Now, as mentioned by the Air Force officer quoted in the 2005 news report, the first 400 tests tested vibration issues, and radio communication. The tests before visiting dignitaries and air-shows since 2001 amount to only 3-4 (you may refer to official website of ADA, which records date, time, duration and Tejas unit number of each test).
How did they progressed to Serial production without completing the flight parameters in Technical Demonstrator???
Technical Demonstrator Vehicles are only TD-1 and TD-2. The PV vehicles, or Prototype vehicles PV-1, PV-2 and PV-3 are also tested. The LSP-1 (Limited Serial Production) is tested in tandem with all 5 earlier models. All vehicles after TD series have progressively superior airframes and improved avionics.
The LSP series of 8 units do not include the initial IAF order of 20 units of Tejas. These are the only ones being manufactured for IAF’s evaluation purposes.
Regarding testing, as of now tests are concentrated towards asymmetrical drop-tank testing, more missile firings, trials in Himalayas and Rajasthan desert after the sea-level trials, and most importantly sensor trials like HUD and HMDS system, besides others. Till now, all on-board systems have exceeded expectations.
References :-
Again you are repeating the same thing over and over again.
When did the LCA project started??
- Is it when the government of the sanctioned by releasing funds-1983?
[*]When the DRDO/NAL/Whoever conducted the feasability studies with user requirement, techinical studies culminating in submitting the report -1978?
[*]When Project defination phase was completed 1989??
[*]When FSED was sanctioned 1993?
See, as these questions have been answered to vikasrehman, you can refer to previous posts (like difference between “metal-cutting” and paper design, or 1993 vs. 1989 etc.) Also, I repeat that there was no requirement in 1978 in particular; in the late seventies, a question for Tejas-type plane was unofficially suggested. The organization that developed Tejas, ADA was formed in 1983.
You did not ans me, How much is the flight envelope expanded exactly from 2005 till now:
As of Feb 2008, one news report reported the same flight envelop. However, the expansion of the flight envelop may have been in the various combinations, of varying degrees of the top speed-altitude-g number achieved so far with new loads.
Since 2005 Tejas has flown with 2 drop-tanks, targeting pod, fired an air-to-air missile and undergone trials at sea-level atmosphere at Arakkonam.
Note that since 2005, PV-2, PV-3 and LSP-1 have flown progressively reducing weight starting from 800 kgs lost since PV-1. They have used more composites, and more modular avionics.
The flight times and endurance limits have also been increased. All maneuvers of a non-TVC plane have been throughly tested.
Thus, this may be a transient stage, similar to the temperature remaining the same as the state of ice changes to water.
While the above does make sense, the statement from the article saying that “design and development” of Tejas began in 1992″ does not appear to be the most accurate one (on its own). From what I know, to someone in the west, designing the layout, building & testing wind tunnel models etc would form part of regular design and development phase. But if this was not the case and initiation of design and development was to be considered from cutting of metal, I wonder how LCA would compare with other 4th gen fighters.
vikasrehman, as rayrubik said earlier (and quoted by you), design process concludes with CFD tests, wind tunnels and also small scale models after PD is released : a phase which Tejas completed by 1990. Some authors practically regard 1993 as start date of FSED (as pointed out by rayrubik) or Full Scale Engineering & Design.
Note that the first Tejas rolled out in Nov. 1995, but was grounded for 5 years till its first flight on 4 Jan. 2001. This was due to lack of FBW, for which software was designed, tested on F-16 Vista sims and integrated on it. Hence, this was part of design process also. Also note that since the first flight in Jan 2001, subsequent Tejas prototypes have steadily lost weight as they increased percentage of composites (PV-1 lost 800 kgs weight). In PV-2, fully modular avionics were introduced, unlike older ones on the prior versions of Tejas.
Hence, all this is evolving design, and cannot be substituted by only the PD documentation and scale modeling done upto 1990.
Buraidiah, the article quoted by you is outdated currently. Note that even as of that writing, the Tejas had a capability to carry 5.85 tonnes including engine weight and radar weight. It is still unlikely however, that Tejas is 1 tonne overweight than the stipulated 5.5 tonnes, as larger planes (with lesser composites) like the all-metal JF-17, Gripen and T-50 weigh quite lesser than or equal to 6.5 tonnes.
I think India’s contribution of the PAK-FA program is not just about the technology transfer or designing the aircraft together.I think we should look this topic from the political side.If Russia would develop this aircraft it’s ownselves,they could maybe sell it to the India’s enemies.And in my opinion this is more imporant than the money or getting the stealth design secrets.
medal64, actually it is confirmed that in the earlier part of this decade, China had refused to partner/fund Russia’s FGFA programme (not particularly the PAK-fa), because it was pursuing its own J-XX programme.
So the fee is for IPRs for local manufacture by HAL, and not merely the assembly of kits?
Yes as per media reports that is correct.
Actually, these IPRs are often misinterpreted to being exclusive (i.e. they won’t be passed on to a third party like China). However, nothing in the news reports so far suggests that India will have exclusive rights to IPR; it is clear that the PAK-FA programme is modelled exactly on the lines of the Su-30 MKI programme and there appears to be no exclusivity clause that prevents Russia from selling IPRs to a third party.
At the most, as in the Brahmos project, India’s consent may be taken because it is a 50% financier to it.
I think you are blaming the IAF here, for not raising objections before:eek: . How do you know they did not raise it before? here it is refresh your memory
http://www.hindu.com/2007/08/25/stories/2007082563300400.htm
I think these objections, along with the ones raised a only few months back here should have been raised by the IAF a few years back, and not after over 800 flight tests have taken place.
Oh Abhimnayu as I told you before ……..LCA is good at specs only, But the specs are just that, not reality. This NEWS is just in, today………for you onleee
http://www.hindu.com/2008/03/23/stories/2008032354971000.htmBut the GTRE’s task has also been complicated by the fact that with the Tejas overweighing by well over a tonne, a Kaveri engine developed as per specifications originally spelt out (when the Tejas was within its design weight) will not be capable of providing a heavier aircraft with the thrust that can satisfy the Air Force’s ASR
The above quote has clearly been phrased improperly because it implies that there was some time when Tejas was within weight limits, but later became overweight. Tejas unit PV-1 reduced its weight by 800 kgs since the first flight of unit TD-1 in 2001. From unit PV-2 onwards, the empty weight of Tejas has been lowered further to 5,500 kgs, and subsequent units PV-3 and LSP-1 have been fixed at that weight.
In my view, the IAF should have come up with these objections much earlier, so that latter “derailments” like this could have been avoided.
That’s obviously isn’t it. I think it was clear from the beginning, that the Indian PAK FA would differ in terms of avionics only and that India wouldn’t be able to contribute anything else, as Sukhois development efforts are to advanced.
Scorpion82, I agree with your views. As per this news report of Aug 2006, the Indian defence ministry had objected to Sukhoi, of India not being in the design decision-making from ‘scratch’.
However, nothing came of this objection, as Sukhoi proceeded with finalizing the design, avionics and weapon systems and has now begun the production also. What maybe unclear is why the Indian defence ministry and IAF change their earlier position.
It may have been clear to those who could read-between-the-lines, but to their respective publics it was being spun as -at best a new project (esp. in India) and at worst a PAK-FA spin-off.
Even on Russian forums last month the query was why were Indian MoD/AF/HAL officials being shown PAK-FA assembly at YG KnAAPO if that ‘jv’ was another project.
Anyways, PAK-FA MKI sounds cool to me. Any word on what the hefty $8 billion Indian ‘contribution’ will be spent on? Does it include aircraft batches?
Otaku, the $8 billion ‘contribution’ from India may practically only be the licence manufacturing fee, in the “disguise” of contribution. Mikhail Pogosyan is on record saying to Russia’s Nezavisimaya Gazeta, that India’s role will purely be that of a financier. After the production of the plane, India can later customize it. As per Reuters, the so-termed ‘joint development’ is in fact only the rights India will purchase to have the PAK-FA modified or customized to local requirements.
From Nezavisimaya Gazeta, 17-10-06 :-
[b]There is a directly connection between the Russian T-50 and the joint Russo-Indian PAK FA. The Sukhoy management, who several years ago won the tender for the creation of the fifth generation fighter, understood such work would take huge financial expenditures and proposed the Indians take part in it.[/b]
References :-
1) Russian Aviation News :-
http://www.royfc.com/acft_news_old_oct3.html
1) Reuters news report :
http://in.reuters.com/article/topNews/idINIndia-30053120071018
News on Indo-Russian FGFA:
Hi Otaku. From the news report you posted, the following excerpt :
The Indo-Russian fifth generation fighter aircraft (FGFA) will be developed based on Sukhoi’s PAKFA platform and would incorporate specific requirements of the air forces of the two nations.
Currently the two sides are finalising the specific requirements and technological inputs identified by the Indian Air Force, which differ from the Russian requirements. “Every customer has nuances. This is true also in the case of fifth generation fighter: there will be a common basic platform, but every customer will have its own specific requirements,” an unnamed official of Sukhoi was quoted as saying by ITAR-TASS.
He gave a typical example, when Malaysia ordered Su-30MKI fighters developed for India, but insisted to replace the Israeli avionics with French. “This is just the same aircraft, but it required certain efforts for adapting different avionics,” the spokesperson added.
I think it maybe the first time that an Indian news report acknowledges that the design of PAK-FA would be based on Sukhoi’s platform only. The official from Sukhoi quoted, gave an example of avionics change of the Su-30 of the Malaysian airforce, to highlight the fact that the customization efforts of IAF in the PAK-FA would only be limited to avionics modifications.
The max. weapon payload of the following planes (some in IAF service) are as follows :-
MiG-29 :- 4,000 kgs.
MiG-27 :- 4,000 kgs.
Tejas :- >4,000 kgs.
T-50 :- 3,000 kgs.
JF-17 :- 3,600 kgs.
From the above, it is clear that as Tejas has superior payload specs., it is superior than the IAF’s existing MiG-29 and MiG-27 planes and is not merely a MiG-21 replacement, as is often incorrectly mentioned by the media (note its max. range also matches that of the above mentioned jets).
You are missing the plot here, I linked the article to show you how recent the Litening acquisation is 2007!!!! The 1995 report seeking Israel help was for LEVI Tech knowhow. Refer the link in previous post.
That was for latter 20 production planes only. Note that the Tejas PV-2 flew with the Litening LDP in Dec. 2007.
Though the news report is unavailable, the Litening LDP was selected for Tejas in the 1990s itself, just like for Su-30 MKI.
Lets not go there…:D
See, I specifically mentioned payload specifications of JF-17 are inferior to Tejas, despite weighing 800 kgs more than Tejas and being the size of F-16. Yet, 2 airforces regard it as a multi-role fighter (not trainer) and plan to induct 200 units of it, each.
Thus, from the same ‘yardstick’, Tejas qualifies as a multi-role fighter.
Well they do emphisised that LCA is also contemporary of F-22 …..Didn’t thay:confused:
The above context is discussed. Anyway, those 2 authors did not mention the quote you are referring to (that was Mr. Hormuz’s article). The Tejas is indeed capable of being an MRCA contender.
Abhimanyu you may want to have a look here
http://www.india-defence.com/reports/3273
Rafael has been selected to supply its Litening targeting pod to equip the Indian air force’s Aeronautical Development Agency-built Tejas light combat aircraft.The order – of undisclosed value – covers the production of Litening systems for the service’s initial batch of 20 production aircraft
The above order is for production run of 20 planes only. That the Tejas would have Israeli designator pods has been known since many years, as the same were contracted for the Su-30 MKIs since late 1990s.
Is it not obivous to you, that they are made in different eras??
See, Mr. Hormuz also mentioned that the current MiG-29s are also no superior than the Tejas in weapon-load capacity. Only MiG-35 is known to carry 1,600 kgs more armament than Tejas.
LCA has same Engine F-404, Same form of help from Dassault like LM for T-50.
Hell even the flight performance till today is same Mach 1.4, 6G, and 48,000 Feet altitude.
Again note that Tejas weighs 1,000 kgs lighter, and has a smaller wingspan and height than T-50.
Although not to be brought into discussion, the JF-17 also has inferior payload specifications as the Tejas, despite weighing 1,000 kgs more than it, and being almost the same size as an F-16 (check length, height and span).
Even the celebrated authors of “LCA comparable to F-22” Parthasarthy and Raman Puri concede that LCA will better suit as trainer.
The above two authors twice emphasize in their article, that the Tejas can also compete as an MRCA contender, as its technologies are second to none.
Don’t kid youself Abhimanyu, the litening pod and Radar acquisation is 2005/6 development and am pointing you to 1995 agreement of using LEVI:dev2: Knowhow
The above is incorrect. The Litening pod was contracted for in the 1990s only.
Do you intend of referring the “LCA comparable to F-22” authors for everything? Guess what, Mirage III was also capable of 4000Kg payload.
Note that Mirage-III weighs 1,500 kgs more than Tejas. Authors have pointed out that Tejas can carry loads of much larger planes than itself, like MiG-29 and MiG-27. Aircrafts of Tejas’ size and weight are classified as trainers, like the S. Korean T-50 (which too weighs 1,000 kgs more than Tejas).
Ok, its all become so confusing.
If ‘The actual design and development work of LCA commenced in 1992’, (im particularly refering to design here) then why do we have an article in Flight in 1989 claiming that LCA’s ‘design has been frozen’???
Now from what I understand (and please correct me if Im worng) a lot of design work needs to be done before you can actually freeze a fighter design??? So either the design work started before 1989 for the design to be frozen in 1989 or the person making this claim was not telling the full truth???
Also if the construction of a 1/7 model model started in 1989, what was that model design based upon? Im sure ir wouldn’t have been the result of a simple meeting about what sort of model we should make, and then we’ll refine the design afterwards.
As we discussed earlier, the 1/7 scale model was based on the PD document, which was formalized between Sept. 1987 to 1988. The design was frozen based on that.
The authors in this article mention “design and development” of Tejas began in 1992″, possibly referring to the beginning of the production (or “metal-cutting”) of the full-scale unit. If freezing the paper design, or drawing board design is considered, then that would be the finalization of the PD in 1988.
But most authors usually take the 1993 date i.e. when the full-scale model begun development, as the start date for design. This is because only the on-paper PD may not be sufficient enough to formally end of design stage.
And they were given $100 Million just to finalize configuration?? That is 1980s $100 Million, irrespective of the claims that ADA did all the work here is the snippet….
The conclusion that it was a design of Dassault and not ADA is incorrect, as Dassault was chosen as the contender (amongst 3 others) to assist in finalization of the Project Definition draft. Its formation took place between Sept. 1988 to 1989.
As mentioned by FlightGlobal’s archives itself, this assistance included the usage of Dassault’s software tools and their design research to arrive at our own design. As we have discussed earlier, the Tejas’ outward compounded-cranked delta configuration is unique globally.
and then Israelis did join the party….:dev2:
http://www.flightglobal.com/PDFArchive/View/1995/1995%20-%200626.html
INDIA HAS turned to Israel in an attempt to rescue its faltering Light Combat Aircraft (LCA) programme. Talks between the two sides are under way about the Israelis providing electronic systems and know-how. The discussions are taking place between Israel Aircraft Industries (IAI) and India’s stateowned
Aeronautical DevelopmentAgency (ADA), thmanagement organisation for the
LCA programme. According to sources, India is asking for help in terms of “hardware and know-how.” The two sides are also believed to be discussing
Israeli involvement in the flight-test programme.
The above led to the usage of Israeli Litening Target pod, and assistence in development of the pulse-doppler multi-mode radar.
IAF requirement was MIG-21 class fighter, that needed to be inducted in 1990s. If you are expecting that IAF mandate Mirage 2000 CLASS aircraft from ADA, then you are in delusion. IAF wanted something better than Mig-21 and expected nowhere near Mirage 2000, hence chosen Mirage III design and seeked Dassault as design consultant.
The above is inaccurate. The IAF never in its ASR specified that Tejas must be a MiG-21 class fighter. As per the authors Mr. Raman Puri and Ashok Parthasarthy quoted earlier, the final ASRs of the IAF were practically that for a Mirage-2000 class fighter. The Tejas can carry the weapon-load of a twin-engined MiG-29 and MiG-27 bomber despite weighing much lesser than the two.
Well you have to ask Kota babu, why he was making false promises to the devotee…don’t you think. He should have known better that without the FSED, how the hell he ordered engines in ’86 and make tall claims of inducting in 1995:eek:
Again, I reiterate that it was the IAF’s delay that led to the production work to begin only in late 1993. The original roll-out of Tejas that was scheduled in 1992, actually happened in 1995.