Cain Marko wrote: ↑03 Jan 2025 03:37
BenG wrote: ↑02 Jan 2025 12:47
<snip>useless rant<snip>
75% commonality between mk1a and mk1, I'll believe that. Between mk1a and MK2, I'll believe that with a pinch of salt and olive oil (only if it is extra and virgin). Between MK2 and AMCA, I'll go tell you to keep the salt and whatever snake oil you're trying to sell with it.
I notice that
the ADA/drdo is some kind of sacred cow on this forum. Sorry, I'm not buying it. Thank you for posting some hard and provocative questions here.
Cain Marko-ji you fell for the troll isn't it?
Last time, this genius
was trying to sell the idea of F414 on Mk1A platforms, just because, some random-google search told him, the F414/Kaveri have the same mass-flow and F404 and F414 have the same dimensions (which is incorrect by the way)?
So get F414 for Mk1As etc ...
Now he's surfaced again with another ingenious idea of HAL's paper-proposal trainer to be replacing the on-the-verge-of-a-rollout, of true-blue MWF, the Mk2. With ample dollops of make-believe narrative of IAF not asking for MK2, and it's somehow forced upon them etc etc etc.
On the top of it, he sure has an axe to grind against the top (now ex) scientists who has dedicated their lifetime nurturing indigenous programs (Mk1 -> Mk2 -> AMCA) to their current successes. I wonder what the motivation would be ...
But since in the current new-and-improved BRF, it is now the norm to allow such blabberings, under benign gaze of the mods - then so be it, I guess!!
But you sir, who has been with (and contributed +vely) the forum for so long, falling for such trolls, is really surprising ...
I mean, it's ok to have opposing/contrarian view-point wrt Indian Def R&D, PSUs etc. A forum remains vibrant/lively because of a variety (so some would be opposing as well) of viewpoints, which allows the debate to be taken forward etc - but does that have to be based on such clueless narrative-building nonsense utterings!!
The least you could have done is, ask/analyse,
1) What has a
program like F-35 got to do with MK1/MK1A, Mk2 or AMCA?
(unless in some pure-google-search-induced-narrative building, the search keyword "stealth" throws up for both F-35 and AMCA, which incidentally this troll specializes in)
2) How is the part count at a platform level,
linked to various surface structure as it has been pointed out of A/B/C variants (of F-35)?
(or was the intent to highlight the specific portion of the platforms)
3) How about trying to figure out the
part-commonality between these A/B/C variants wrt,
i) DFCC and the attended FBW systems (incl FC laws)
ii) Avionics subsystems like AN/APG-85, EoDAS/EoTAS, EW Suite, MADL, Various Radio Systems etc etc.
iii) CFC based structural design and fabrication technology (IIRC they are now all UHM based) - just because the shapes may be slightly different, the "parts" must be different right?
iv) DAI Intakes, Hydraulic and Pneumatic system architecture (Reservoir, Pumps, Valves, Actuators, Pressure Regulators etc)
v) Various Cockpit Displays/HMDS, Radio Altimeter, ILS/TACAN/VOR etc
vi) Other subsystems like HOTAS, OBOGS etc
... etc etc etc.
That should have provided clues about this whole part-commonality etc between these variants - however, this being "Bharat" Rakshak forum, there's no point in trying to list out such stuff (and analyze them) of a videshi platform.
Now coming back to the AMCA-via-Mk2 saga, I know for a fact that you, of all people, needn't to be told/lectured about the following:
1)
IAF lead design-changes (necessitated by 4-5 iterations of requirements change) that saw
the MTOW go from 15000T to a whopping 17500T (with 45% and 25% increment of payload and Int uel respectively) full-blown MWF.
After all why did the
QRs took full 9 years (2009 - 2018) to be finalized - who led the whole iterative Initial Req->design->Rev Req->Redesign-> ... ->Frozen Design initiatives?
So, where's the question of Mk2 being "imposed" or something on the IAF?
2) The
difference between Unkil MiC and our desi MiC, and how the approach of capability dev has to be completely different:
Unlike Unkil, in our case, we have a "developing" MIC and supply chain partners, mostly via MSMEs - with whom we can't expect them have substantial in-house R&D and capability-building investments.
So we'll need to
incrementally build technological capability in them via
continuous and uninterrupted "on-the-job" platform series production - so that when your 5th Gen series Mfg capability is needed, it's just about there.
Also the volume of platforms that Unkil's MiC is supposed to support is large enough, to have dedicated industrial units, with ample parallel and alternate programs to supply to and sustain themselves - same for our desi MiC, is it?
Quick example, without naming names (but should be quite easy to search and find out though):
Do you expect the relevant MSME to somehow directly graduate to producing GaN TR modules for AMCA radars - without producing the GaAs TR modules (for Mk2) first.
After not only investing in relevant GaN foundries, but also developing the relevant expertise amongst it workforce, ab initio.
(PS: This is an deliberately chosen this example - after all, Trolls need opportunities to parade their ignorance, will wait eagerly)
So the question remains, without
building for Mk2, how will this MSME-based MIC, directly graduate to producing/building AMCA - ADA/DRDO et all will hold hands, no doubt, but capability building, require certain base technical capability, to build upon - where will that come from.
3) And as per the "part-commonality" between Mk2 and AMCA is concerned ... let's consider the system/subsystem list for F135 A/B/C above (pt 3), and try to
map the diff wrt them, between what is envisaged for AMCA vis-a-vis those going to be in MK2.
I'll start with a few:
i) Why would CSIR-NAL
develop various algorithms for multi-target tracking/fusion using onboard sensors such as IRST,MAWS, Radar, & RWR for
BOTH LCA Mk 2 & AMCA ... why not only for AMCA? Is it that they want real-world usage data in MK2 before fine-tuning it for AMCA?
ii) Which IAF platform uses
co-cured co-bonded hybrid composites technology (as opposed to composite skins riveted etc) for air intake-duct assembly?
(anxiously waiting for the troll to start blabbering about cocured cobonded tech of Mk1/Mk1A tailfin)
iii) Structurally, where will the
CF2 grade CFCs (designed by NAL) be used, before going into almost entire structure of AMCA?
iv) Which IAF platform has/will have
internal/integral DRFM based ASPJ + DRWR (produced indigenously), which can then miniaturized and modified to be able to integrated in a 5th Gen planform (of AMCA)?
Something like
INTERNAL within the wingtips, wing trailing edges, horizontal stabilisers and either side of aircraft's exhaust.
Will the capability wrt external ASPJ of Mk1A suffice to be able to miniaturise it sufficiently? Isn't the first step to distribute the subsystems to a hump below the tailfin and other parts of the fuselage etc?
v) Which IAF platform
will have a LAD - something that will be used directly on AMCA? Or is it that a LAD is the same technological capability wrt 6in x 8in MFDs?
vi) Any IAF platform
with indigenous MAWS - which can then be miniaturized and distributed for an integral implementation in AMCA? Without having an implemented integral MAWS, how can that system be miniaturised and then distributed across the AMCA platform?
vii) What
about IRST? If AMCA is envisaged to have EOTS, should atleast a 3rd Gen IRST be first developed and used somewhere, to be able to morph into a EOTS later?
...
...
I'll stop here, but I hope you'll take it from here and do the required research to understand the Mk2-AMCA part commonality etc ...
No, you don't have to agree with the 75% part commonality figure (or 74.9999% figure) etc - all these are approximations from whatever little gets published via tenders and public utterings/announcements anyway.
But such a research will certainly help understand the
extent of this part-commonality between Mk2 and AMCA and
why Mk2 is considered as an mandatory pre-requisite for the AMCA program.
Assorted Trolls and import-pasand shills not withstanding ...
