AHCA (Advanced Heavy Combat Aircraft) concept, 5/5.5/6gen? Su-30MKI replacement? TEDBF 2.0?

Our industry is not mature enough to have that many engines. Even the Chinese have just 1.

ADVENT started in 2007, but before that was another program that ran internally until 2007. Then came AETD and then AETP. So they keep closing programs after milestones are achieved and starting new ones with new objectives.

Our only future replacement program is MKI and its from 2055 onwards. The IAF is set until the mid to late 2040s with AMCA.

The thing is the IAF realized that they don't need a very big and heavy MKI-style jet for enemies at the border. They need Rafale/AMCA-sized jets because the main criteria is operational availability and turnaround time. So 100 AMCA will be superior to 270 MKIs in the main criterias.
> But that doesn't mean that every maker/country need to have same R&D procedure & timeline. This is an era of urgency for us & right time to absorb so many people into industry. Small countries sprung up after World Wars. This is the time to show industrial maturity.
> As every country as well qualified citizens in different domains, they also can question how their tax is utilized, they also know what they are saying, especially after multiple scams & delays. Not even in USA & Europe the qualified citizens always fully agree with DoD/MoD decisions. We even see protests on news. And that's why this kind of forums exist. There are even private Thinktanks & Study-institutes which qualified citizens join or contribute.
> 30 years is huuuuuuuuuge time for R&D. IAF is just the operator. We'll never get precise insight into who's fault is it, so collectively - GoI, MoD, DoD, ADA, NAL, DRDO, HAL, IAF, etc have made repeated mistakes ignoring R&D bcoz of which LCA, MWF, AMCA, UCAVs, everything has got delayed by decades. Like i said, the engine is deciding factor.
> It is not a thumb rule that big jets will have bigger turnaround time & lesser availability. It is a simple tech evolution & economics that certain size bigger jet per sortie can deliver more firepower with higher loitering time, sometimes in stealth mode. And the electricity required for avionics, equipments, DEW, etc will require much better engine. F-35 got hit by these points & now it is getting MLU/ECU, but we are not at par with them, hence our AMCA, Rafale, MWF will never satisfy the tech points mentioned. Just have a look at the table i created in 1st post. You may create your own table based on your opinion & vison & share with us.

I'm not talking about that being a naval requirement. The IN only needs an AMCA++ in the 2040s. So the industry will take it up after TEDBF.
Let them go ahead with TEDBF & AMCA as LSP, & in parallel work for common fuselage jet for IAF & IN. The easiest thing they can do is inflate AMCA with F110 or AL-41 engine.

But IAF will want its MKI replacement to be ramjet/scramjet capable in 2055.
What I'm saying is the next IAF jet ADA develops to replace MKI will not be NGAD, FCAS, GCAP class, it will be Mig-41++/SR-72++ class.
Any official statement, news, article, video?
Anyway, this is irrelevant to the discussion. My point is we will have ramjet/scramjet on an aircraft by 2030-35 as well, which can translate into a militarized engine for use on AHCA through the 2040s with introduction after 2050.


AMCA's engine will give us all that. AMCA and N-AMCA will require a turbofan, with or without VCE, whatever the forces want. This will serve our needs for 50+ years.

For AHCA, we will need turbofan/turbojet + ramjet/scramjet.

2055, not 2040s.

The next air superiority fighter will require stratospheric performance. You can quite literally say that MRFA and AMCA will deal with 18 km and below and AHCA will deal with 15 km to 80 km. Adding something between the AMCA and AHCA is just a waste of resources, we can instead just make an AMCA Mk2.

So my development goals for
IAF: LCA > AMCA > AHCA (stratospheric class)
IN: N-LCA > TEDBF > TEDBF 2.0 (NGAD, FCAS class)
ADA: LCA > TEDBF > AMCA > TEDBF 2.0 > AHCA

The IAF and IN will ultimately have 3 indigenous types, with only Rafale being common to both.

Of course, I'm not sure yet if LCA Mk1/A will see a direct replacement. It could all get subsumed into AHCA + drones.

Mig-41 should give us a clue in the future.
> Developing SCRamjet on missiles is much easier than on aircraft. I wonder why ISRO not helpign in Turbofan R&D with heat resistant materials, etc.
> Just like you're saying AMCA can do with or w/o VCE, similarly i'm saying AHCA can do with or w/o Ramjet/SCRamjet.
> If AHCA will need turbofan/turbojet + ramjet/scramjet then 4 engines setup automatically becomes Super-Heavy jet. It'll be ASHCA. I'm still imagining a 2 engine setup.
> So there is no need for AHCA to wait for SCRamjet to mature till 2055.
> Startospheric flight with SCRamjet will require afterburner which increases IRS, means huge amount of fuel, means Super-heavy weight. The turning radius will be huge. For example SR-71 at Mach 3 takes 80Kms for U-turn.
1724760805456.png


Such thing is better suited to different thread altogether.


> What you are refering to AMCA MK2 is an inevitable MLU, like EF-2000 has Tranche, Rafale has F#, USAF jets have Blocks. I'm talking about either simply inflate AMCA like LCA>MWF or a new project in parallel with AMCA as LSP.
> N-LCA is ok for research purpose but into production squads would be worst decision today & future of global Naval aviation. I'll never support my income tax after it.

In short our current opinions look like following table. Let me know corrections if any. I'm trying to arrive at values of empty weight, fuel weight, payload weight, thrust required, etc. It would be good if you share your guess of what you visualize.

1724767291965.png



I believe drones will be made to carry heavier weapons, while the fighters themselves will be more sensor and fuel-heavy with smaller weapons bays. 'Cause it's pretty cheap and fast to fly a drone and fire off standoff munitions.
Yes that's a possibility but we are not talking about old gen big weapons but customized ones with folding fins which are already being developed.

As per General Hostage, who was the commander of USAF's ACC, the F-35 has lower RCS than the F-22.
People are confused about it because they are comparing the F-22's achieved RCS to the F-35's goal. But the F-35 also surpassed its goal.
Armed forces personel of every country are oblidged to say all good about their worst product also bcoz there are always lagging nations to buy them.
Technology also depends on geopolitics. It is possible that USA's F-35 have better quality RAM & EW than export variant.

We are not doing anything fancy, our main goal is success. The Russians are far more experienced than India is, and they are bound to know more than we do right now, way more.
There is big list of global industrial blunders in every domain also, especially in developed & leading countries but media seldom talks about it.
Ultimately the RCS figure matters. The Quora analysis which you shared showed so many reasons. But Russia or any country wont ever tell exactly reasons for higher RCS.

AFAIK, the F-22's export ban wasn't because of stealth. It carries other unique technologies that they did not want to leak at the time.
So we have to think what unique tech at that time. Many of us know the basic category of components in a jet.
Few things which i can think of are airframe cooling system, Transpiration cooling for nozzles/plume, avionics computer, the F119 engine, RAM, etc. There are diagrams of many jets available on internet. People should ask what they don't understand. Following is F-22's diagram:
1724766912777.jpeg


As per the IAF, MKI is not underpowered.
As per mathematics & LIVE performance it is.
And remember that armed forces of all nations are oblidged to say all good diplomatically.
 
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I won't talk much about AMCA in this thread bcoz i launched this thread due to dissatisfaction with AMCA.😆
The size, shape, weight, structure of AHCA would depend on type & number of weapons it would carry.

LEARNING LESSONS FROM 5GEN JETS F-22, F-35, Su-57
New gen jets would require new gen weapons with modified shape & folding fins, perhaps a different attck profile, like F-22 & F-35 will get MAKO, AGM-88E AARGM-ER, Kh-58UShKE, etc.
For example it is not possible or feasible for Su-57 to carry Brahmos like big missile even if its tandem IWBs are joined.
View attachment 35792

We see that IWBs of both F-22 & Su-57 have some disadvantage.
Su-57 carries only 4 AAMs currently, may be 6 in future.
F-22 cannot carry weapon bigger than JDAM currently. MLU might add something.
View attachment 35790


Su-57 can carry cruise missle, Kh-58UShKE internally.
View attachment 35791

A bigger collage shows some current weapons fit, some don't.
View attachment 35793

A new jet can combine both capability by having multiple IWBs. the centerline IWB will carry customized CrM, AShM, ARM, etc.
And 2 parallel IWBs can carry 2 AAMs each, total 4.
If we imagine a modified diagram of Su-57 & F-22 then it would look like following:
NOTE - This is just preliminary & notional, otherwise the engines & internal components will obviously have to be adjusted.
View attachment 35797

The following is 1 of the many examples already created by CAD artist Rodrigo Avella in his vision of F/A-XX :
The IWB bottom edge would be wider than F-22.

View attachment 35794

AMCA is not supposed to carry heavy weapons, only small missiles and glide bombs for the A2G role. Its main role is air superiority. An extension of that is SEAD/DEAD via small bombs meant to destroy trucks and exposed radars. The F-22 has the same role.

The Russians merely combined the two requirements of AS and strike into one on the Su-57.

We have no need to internalize Brahmos-MA, its standoff range doesn't require a stealthy platform. And Brahmos on MKI will give us 800-1000 km range.
 
> But that doesn't mean that every maker/country need to have same R&D procedure & timeline. This is an era of urgency for us & right time to absorb so many people into industry. Small countries sprung up after World Wars. This is the time to show industrial maturity.
> As every country as well qualified citizens in different domains, they also can question how their tax is utilized, they also know what they are saying, especially after multiple scams & delays. Not even in USA & Europe the qualified citizens always fully agree with DoD/MoD decisions. We even see protests on news. And that's why this kind of forums exist. There are even private Thinktanks & Study-institutes which qualified citizens join or contribute.
> 30 years is huuuuuuuuuge time for R&D. IAF is just the operator. We'll never get precise insight into who's fault is it, so collectively - GoI, MoD, DoD, ADA, NAL, DRDO, HAL, IAF, etc have made repeated mistakes ignoring R&D bcoz of which LCA, MWF, AMCA, UCAVs, everything has got delayed by decades. Like i said, the engine is deciding factor.
> It is not a thumb rule that big jets will have bigger turnaround time & lesser availability. It is a simple tech evolution & economics that certain size bigger jet per sortie can deliver more firepower with higher loitering time, sometimes in stealth mode. And the electricity required for avionics, equipments, DEW, etc will require much better engine. F-35 got hit by these points & now it is getting MLU/ECU, but we are not at par with them, hence our AMCA, Rafale, MWF will never satisfy the tech points mentioned. Just have a look at the table i created in 1st post. You may create your own table based on your opinion & vison & share with us.

The reason why bigger jets are difficult to maintain is because they put as much latest tech and capability into it and that makes things expensive. For example, it's easier to maintain a 150 kg radar versus a 650 kg one.

As for India, right now, we only have 1 organization capable of designing and fielding an engine and that's DRDO. And because the DRDO Chief has a lot of power in the govt, other companies do not want to compete. Any attempt to design an engine can only be carried out in the private sector for civilian use first, which is why HAL is working on a civilian version for use on business jets. By the time multiple companies show up with such capabilities, we are talking 2060s-70s, not earlier than that.

The private sector is currently focusing on drone engines, small and medium-sized ones, from handheld to Predateor/Reaper sized ones. HAL is working on a business jet class engine. This will be followed by a militarized version for large drones like Triton. DRDO is developing everything above that; IUSAV, LCA, AMCA etc.

Let them go ahead with TEDBF & AMCA as LSP, & in parallel work for common fuselage jet for IAF & IN. The easiest thing they can do is inflate AMCA with F110 or AL-41 engine.

ADA says they won't be developing a common airframe for the IAF and IN. The orders are big enough for both and they do not want to compromise on the design trying to fit both their requirements. That's why there won't be an N-AMCA, any new naval design will be clean-sheet after TEDBF.

Any official statement, news, article, video?

It's an opinion.

AMCA is good enough all the way to the 2070s-80s, so there is no need to make a cousin. An AMCA Mk2 made by 2060 will take us all the way to 2100.

ADA can focus all their resources on a 6th gen TEDBF 2.0 and a 7th gen AHCA.

> Developing SCRamjet on missiles is much easier than on aircraft. I wonder why ISRO not helpign in Turbofan R&D with heat resistant materials, etc.
> Just like you're saying AMCA can do with or w/o VCE, similarly i'm saying AHCA can do with or w/o Ramjet/SCRamjet.
> If AHCA will need turbofan/turbojet + ramjet/scramjet then 4 engines setup automatically becomes Super-Heavy jet. It'll be ASHCA. I'm still imagining a 2 engine setup.
> So there is no need for AHCA to wait for SCRamjet to mature till 2055.
> Startospheric flight with SCRamjet will require afterburner which increases IRS, means huge amount of fuel, means Super-heavy weight. The turning radius will be huge. For example SR-71 at Mach 3 takes 80Kms for U-turn.
View attachment 35818

Mig-41 should tell us what size a jet of this class will be. I don't think we have to make AHCA bigger than it.

Btw, a turbojet-ramjet is one engine called "air turboramjet." It's a new class of hybrid engines.


So, for the hypersonic regime, we may need a turboramjet + scramjet. How this development will take place is yet to be seen. We could see it with SR-72 and our space shuttle. Maybe some Chinese design could show up before ours.

> What you are refering to AMCA MK2 is an inevitable MLU, like EF-2000 has Tranche, Rafale has F#, USAF jets have Blocks. I'm talking about either simply inflate AMCA like LCA>MWF or a new project in parallel with AMCA as LSP.
> N-LCA is ok for research purpose but into production squads would be worst decision today & future of global Naval aviation. I'll never support my income tax after it.

Same thing. I'm talking about AMCA undergoing an LCA Mk1 to Mk2 transition. Slightly bigger, more fuel, more powerful engines. Similar to the conversion from Hornet to Super Hornet.

In short our current opinions look like following table. Let me know corrections if any. I'm trying to arrive at values of empty weight, fuel weight, payload weight, thrust required, etc. It would be good if you share your guess of what you visualize.

View attachment 35834

Pretty much. Except that "Super-Heavy" will be relative to the technology of the time. For all we know it could end up being smaller and lighter than the MKI.

AMCA is like an MLU-ed F-22. AMCA has higher fuel fraction and almost the same internal carriage. ADA has made a version with sidebays and one without, dunno which one's been chosen.

Armed forces personel of every country are oblidged to say all good about their worst product also bcoz there are always lagging nations to buy them.
Technology also depends on geopolitics. It is possible that USA's F-35 have better quality RAM & EW than export variant.

US F-35s will have greater unlocked potential than export customers. They will simply restrict processing power to limit radar range for example. Or the EW system will manage lesser bands at any one time.

As per mathematics & LIVE performance it is.
And remember that armed forces of all nations are oblidged to say all good diplomatically.

Not in this case. The MKI's dogfighting capabilities should be compared to other jets on 25% fuel or equivalent fuel fraction, not a blanket half fuel. For example, LCA can only fly for less than an hour on full internal fuel, but MKI can do more than that at half tank. LCA enters a dogfight at half tank, but MKI does the same with quarter tank.

With quarter tank, the MKI has a fuel fraction of 0.12 whereas LCA is at 0.15, quite comparable. But TWR is 1.25 vs 1.1 resply.
Similarly, Typhoon at half tank is 0.17, and has a TWR of 1.24. So the MKI is not underpowered. In fact, with only quarter tank, the MKI will perform better than other aircraft with half tank. Plus TVC.

If any boost in thrust is necessary, the MKI can get the same out of a marginal rise to 132 KN, to compensate for any increase in weight during MLU. This is the reason why the IAF is not going for the 117S.
 
It's enough. It can carry AAMs, and small bombs (500 kg and below) and short range missiles. That's its main job.


As it's currently designed, the AMCA's IWB only has room for 2 BVRs and 2 SOW.

I know it won't operate alone but they should have made provision for a smaller bay to carry CCMs imo.

The good thing is that DRDO will now need to build a new class of small PGMs (like SAAW) and AAMs to fit the AMCA's bays, just as LM did with the F-35. Case in point: SDB series of bombs.

These weapons, when ready, will dramatically increase the load out of our other fighters.
 

As it's currently designed, the AMCA's IWB only has room for 2 BVRs and 2 SOW.

I know it won't operate alone but they should have made provision for a smaller bay to carry CCMs imo.

The good thing is that DRDO will now need to build a new class of small PGMs (like SAAW) and AAMs to fit the AMCA's bays, just as LM did with the F-35. Case in point: SDB series of bombs.

These weapons, when ready, will dramatically increase the load out of our other fighters.
Internal load of 6 BVRAAMs is necessary IMO for air superiority missions. Even F-35, a so called strike fighter is getting a sidekick in Block 4 to carry 6 AMRAAMs in its IWB. Having just 4 is not good at all.
 

As it's currently designed, the AMCA's IWB only has room for 2 BVRs and 2 SOW.

I know it won't operate alone but they should have made provision for a smaller bay to carry CCMs imo.

The good thing is that DRDO will now need to build a new class of small PGMs (like SAAW) and AAMs to fit the AMCA's bays, just as LM did with the F-35. Case in point: SDB series of bombs.

These weapons, when ready, will dramatically increase the load out of our other fighters.

2 missiles + 2 bombs is a pretty standard loadout for the MWB, same as the F-22.

If the missiles have both IR and RF seekers, then we won't need 2 additional WVR missiles for this mission.

The real goal will be to just make a VLO WVR missile for the wingtip. ASRAAM is already below 0.01m2, so getting a similar missile down to -40dBsm class wouldn't be difficult. The main point of a wingtip missile is to snapfire before disengagement. Weapons bays prevent that. The J-20 loses stealth to do the same with their contraption.
 
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Internal load of 6 BVRAAMs is necessary IMO for air superiority missions. Even F-35, a so called strike fighter is getting a sidekick in Block 4 to carry 6 AMRAAMs in its IWB. Having just 4 is not good at all.

That's a result of their failure to expand the size of the F-22 program. It's a half-as*ed measure.

Instead of 400-750 F-22s, they have to manage with just 125 or so, and have to compensate for the rest with 300 F-35As. Robert Gates killed the USAF singlehandedly.
 
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AMCA is not supposed to carry heavy weapons, only small missiles and glide bombs for the A2G role. Its main role is air superiority. An extension of that is SEAD/DEAD via small bombs meant to destroy trucks and exposed radars. The F-22 has the same role.
It's an opinion.
AMCA is good enough all the way to the 2070s-80s, so there is no need to make a cousin. An AMCA Mk2 made by 2060 will take us all the way to 2100.
Buddy, wrong reply to purely AHCA based post. And at least i'm not here to blindly agree with GoI/MoD/DoD & repeat their words. If they wan't to use MKI & other jets for next 100-150 years also, we can't do anything except hunger strikeo_O:ROFLMAO:, but i dont wanna talk about it here. You tag me in AMCA thread.
And reminder again - the idea is learn from limitations of every jet.

ADA can focus all their resources on a 6th gen TEDBF 2.0 and a 7th gen AHCA.
Perhaps you can create a 7gen thread & outline your vision about it, an ASHCA, not AHCA. And tag me in Hypesonic thread, we'll discuss SCRamjet, etc.

As for India, right now, we only have 1 organization capable of designing and fielding an engine and that's DRDO. And because the DRDO Chief has a lot of power in the govt, other companies do not want to compete. Any attempt to design an engine can only be carried out in the private sector for civilian use first, which is why HAL is working on a civilian version for use on business jets. By the time multiple companies show up with such capabilities, we are talking 2060s-70s, not earlier than that.

The private sector is currently focusing on drone engines, small and medium-sized ones, from handheld to Predateor/Reaper sized ones. HAL is working on a business jet class engine. This will be followed by a militarized version for large drones like Triton. DRDO is developing everything above that; IUSAV, LCA, AMCA etc.
Current actions are not good enough for most populous country in the world with unployment rising.
In engine tech as weall know there are 3 ways - import is shortest way, JV takes medium time, total self effort takes longest time. But like i said other nations, both small & big, developed a sense of urgency. It is luck & unpredictable thing if war will break out or not & when. Sometimes nations get dragged into others' conflicts. Sometimes a hostile nation preemtively strikes which our neighbors have done already few times. After that also we have not learned.
We are making LCA, MWF, AMCA only bcoz of lack of engine tech. If our GTRE or private firm could make any type of engine required then we would have made variety of fighters, bombers, etc & exported to world, plain simple.
But every country not having that industrial capability gives excuses - "we don't need this/that", "It is not supposed to do this/that", etc.
The next few decades are going to be unpredictible & delicate situation due to Chinese military buildup.
If future USA's regime becomes hostile or non-cooperative to us then we'll get a nice kick & sense of urgency.

The Russians merely combined the two requirements of AS and strike into one on the Su-57.
So that's a good learning they took. I hope if we take it too now, or never. We don't have to wait for rest of world to do something 1st.

We have no need to internalize Brahmos-MA, its standoff range doesn't require a stealthy platform. And Brahmos on MKI will give us 800-1000 km range.
> We have an urgent need actually to transition to new gen weapons with not just internal electronic improvements but also body design. Brahmos NG will be shorter. We just need to alter it little more. And more cutomized weapns are needed.
> Bcoz MKI is non-stealthy hence it needs huge standoff range weapons llike Brahmos. A stealth jet will be detected late at shorter ranges hence it can launch custom weapons from shorter ranges. You gave example of F-22 above, now it got the MAKO missile. I hope we will learn.

The reason why bigger jets are difficult to maintain is because they put as much latest tech and capability into it and that makes things expensive. For example, it's easier to maintain a 150 kg radar versus a 650 kg one.
Lots of things around us are actually costly like car compared to 2-wheeler w.r.t mileage, maintenance, etc. Military economics is different than civil. In era of every gen - 1st, 2nd, 3rd, 4th & now 5th things were costly initially. There were always some people who panicked in every gen's era o_O 🙀 🤦‍♂️:ROFLMAO:
Also things will be costly more in capitalist countries than communist & socialst mixed economies.
Nobody knew that subsonic P-51 Mustang will be replaced by supersonic F-22. It is merely natural tech evolution & requirement.
Difficulty doesn't stop Development.


1724930344099.png


ADA says they won't be developing a common airframe for the IAF and IN. The orders are big enough for both and they do not want to compromise on the design trying to fit both their requirements. That's why there won't be an N-AMCA, any new naval design will be clean-sheet after TEDBF.
Does that mean that Rafale was comproise by Dassault just bcoz a Naval jet needs stronger landing gear & lower speed stability. It is better to develop a common body jet 1st for Navy. N-AHCA =TEDBF 2.0 which can be a clean-sheet design, which can be used for AF too.

Mig-41 should tell us what size a jet of this class will be. I don't think we have to make AHCA bigger than it.
You wan't other nations to dictate our projects? Or you wan't our DoD to sit & wait for others to do things 1st & then beg for imports?
My last post showing F-22 & Su-57 diagrams was a step towards acertaining the size & weight of AHCA = Empty weight + fuel + internal payload. And regarding its engines, i won't be considering what GoI/GTRE BABUs will be doing at snail's pace but what is certainly doable in urgent mode.

Btw, a turbojet-ramjet is one engine called "air turboramjet." It's a new class of hybrid engines.

So, for the hypersonic regime, we may need a turboramjet + scramjet. How this development will take place is yet to be seen. We could see it with SR-72 and our space shuttle. Maybe some Chinese design could show up before ours.
Yes, i checked Turbo-ramjet on Wikipedia. It seems to use Hydrogen & Oxygen which would increase the size & weight of a practical aircraft a lot.
And apart from French Nord 1500 Griffon II there doesn't seem to be any other test aircraft.

1724931631372.png

Rest can be discussed in Hypersonic thread.

Same thing. I'm talking about AMCA undergoing an LCA Mk1 to Mk2 transition. Slightly bigger, more fuel, more powerful engines. Similar to the conversion from Hornet to Super Hornet.
Heavy jets like F-22, F-15, Su-57, Su-3X, J-20 are not just SLIGHTLY bigger & heavier than F-18 SH, MiG-29/35, Rafale, EF-2000.

Pretty much. Except that "Super-Heavy" will be relative to the technology of the time. For all we know it could end up being smaller and lighter than the MKI.
For that 1st you have to share your idea of realistic empty weight, fuel weight, internal payload weight. It is your vision of 7gen AHCA which will be much bigger & heavier than MKI.
But my idea is to technically come closer to NGAD, F/A-XX, GCAP, FCAS. If AHCA can be around MKI then it is very good.
As i highlighted some of the heavy jets above & the 6gen might be 30-50% heavier, & some custom AGMs carried internally & not just AAMs + DEW-CIWS, it is highly unlikely that their 6gen would be less voluminous & lighter than MKI.
But if we can package an AHCA jet near MKI, it is very good.

AMCA is like an MLU-ed F-22. AMCA has higher fuel fraction and almost the same internal carriage. ADA has made a version with sidebays and one without, dunno which one's been chosen.
Depends on what things are in MLU. Both will have today's standards of computing but total computing power of F-22 would be higher as USA is ahead in H/w & S/w R&D. Also, we have just begun optical sensors R&D while they got DAS & HMDS in 1990s.

Not in this case. The MKI's dogfighting capabilities should be compared to other jets on 25% fuel or equivalent fuel fraction, not a blanket half fuel. For example, LCA can only fly for less than an hour on full internal fuel, but MKI can do more than that at half tank. LCA enters a dogfight at half tank, but MKI does the same with quarter tank.
With quarter tank, the MKI has a fuel fraction of 0.12 whereas LCA is at 0.15, quite comparable. But TWR is 1.25 vs 1.1 resply.
Similarly, Typhoon at half tank is 0.17, and has a TWR of 1.24. So the MKI is not underpowered. In fact, with only quarter tank, the MKI will perform better than other aircraft with half tank. Plus TVC.
If any boost in thrust is necessary, the MKI can get the same out of a marginal rise to 132 KN, to compensate for any increase in weight during MLU. This is the reason why the IAF is not going for the 117S.
That way by reducing fuel & matching with light/medium jet you are intentionally degrading the design purpose of heavy jet. That way it would be wrong to make a heavy jet in the 1st place. You forgot that when design weight increases then the thrust of engines are also researched to maintain or increase the TWR.
The light/medium jets would run out of fuel quickly while heavy jets would still have a lot & their aerodynamics & aglity is designed with more fuel.
50% fuel is taken as an adhoc measure bcoz different jets have different empty weight, engine weight, # of engines, SFC, thrust, fuel capacity. The jets start, taxi, takeoff, climb, reach the conflict zone, engage in BVR combat, then dogight begins. So 50% fuel might have been consumed already. But the airframe TWR is the only mathematical measure left.
For example, F-35 has 8-9 tons fuel,
Su-3X have 11 tons fuel,
F-22 has 8.2 tons fuel.
But F-22's F119 engines have lowest SFC which if coupled with higher fuel capacity & airframe TWR would give TRIPLE advantage.
In a TVC maneuver if a jet comes to zero speed then it should be able to accelerate fast upwards where the net thrust is lowest.

1724946044036.png


2 missiles + 2 bombs is a pretty standard loadout for the MWB, same as the F-22.
Learning lesson for entire world. USA won't repeat that mistake with NGAD, F/A-XX.

If the missiles have both IR and RF seekers, then we won't need 2 additional WVR missiles for this mission.
The real goal will be to just make a VLO WVR missile for the wingtip. ASRAAM is already below 0.01m2, so getting a similar missile down to -40dBsm class wouldn't be difficult. The main point of a wingtip missile is to snapfire before disengagement. Weapons bays prevent that. The J-20 loses stealth to do the same with their contraption.
That's is exactly why 6gen has outlined DEW-CIWS to defeat multi-spectral AAMs. And that's why more attempts means more AAMs will be required.
Stealth missiles were tested but not materialized, IDK why.
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That's a result of their failure to expand the size of the F-22 program. It's a half-as*ed measure.

Instead of 400-750 F-22s, they have to manage with just 125 or so, and have to compensate for the rest with 300 F-35As. Robert Gates killed the USAF singlehandedly.
So you do think that F-22 should have got higher IWB capacity.
But you don't want our products to get over those limits & mistakes, WHY?
Just like you quote dual-band AAM to close gap b/w RF BVR-AAM & IR-CCM, similarly i'm projecting an idea of AHCA to improve the economics per sortie & at least narrow gap b/w AMCA, TEDBF & NGAD, F/A-XX. We can't afford to severely lag again by an entire gen for next 50 years. Again it would like "Can't swallow, can't spit" :sick:❌🤮❌ 🤣
IAF chief said they have roadmap to 6gen. What is it? :rolleyes::unsure:😃
 
Buddy, wrong reply to purely AHCA based post. And at least i'm not here to blindly agree with GoI/MoD/DoD & repeat their words. If they wan't to use MKI & other jets for next 100-150 years also, we can't do anything except hunger strikeo_O:ROFLMAO:, but i dont wanna talk about it here. You tag me in AMCA thread.
And reminder again - the idea is learn from limitations of every jet.


Perhaps you can create a 7gen thread & outline your vision about it, an ASHCA, not AHCA. And tag me in Hypesonic thread, we'll discuss SCRamjet, etc.


Current actions are not good enough for most populous country in the world with unployment rising.
In engine tech as weall know there are 3 ways - import is shortest way, JV takes medium time, total self effort takes longest time. But like i said other nations, both small & big, developed a sense of urgency. It is luck & unpredictable thing if war will break out or not & when. Sometimes nations get dragged into others' conflicts. Sometimes a hostile nation preemtively strikes which our neighbors have done already few times. After that also we have not learned.
We are making LCA, MWF, AMCA only bcoz of lack of engine tech. If our GTRE or private firm could make any type of engine required then we would have made variety of fighters, bombers, etc & exported to world, plain simple.
But every country not having that industrial capability gives excuses - "we don't need this/that", "It is not supposed to do this/that", etc.
The next few decades are going to be unpredictible & delicate situation due to Chinese military buildup.
If future USA's regime becomes hostile or non-cooperative to us then we'll get a nice kick & sense of urgency.

We need to go by our own timeframe, not others'. For example, the French completely skipped a stealth jet and Dassault claims the Rafale F5 is good enough until 2050, with a modernized Rafale taking over beyond that, which means they believe SCAF is unnecessary.

And now the USAF is doing a rethink on NGAD because they believe unmanned CCAs will surpass it by 2040. Which means our AMCA will be a better option than Rafale + modernized Rafale or F-22 + F-35 combo due to its relatively newer design.

With drones taking over the regular AS mission, the IAF is going to need a true next gen capability after AMCA, not just an NGAD equivalent. And remember, we are talking 2055, so that's gonna have to be us skipping a generation.

So that's a good learning they took. I hope if we take it too now, or never. We don't have to wait for rest of world to do something 1st.

Our plan is the same, we just want a much smaller jet because unlike their large territory which requires range and speed, we need higher endurance and turnaround. You don't get the latter two with a very large jet.

> We have an urgent need actually to transition to new gen weapons with not just internal electronic improvements but also body design. Brahmos NG will be shorter. We just need to alter it little more. And more cutomized weapns are needed.
> Bcoz MKI is non-stealthy hence it needs huge standoff range weapons llike Brahmos. A stealth jet will be detected late at shorter ranges hence it can launch custom weapons from shorter ranges. You gave example of F-22 above, now it got the MAKO missile. I hope we will learn.

Brahmos MA is being designed for 300 km range, perhaps 400 km. The MKIs will be able to use the 800+ km Brahmos-A variant in the near future.

Lots of things around us are actually costly like car compared to 2-wheeler w.r.t mileage, maintenance, etc. Military economics is different than civil. In era of every gen - 1st, 2nd, 3rd, 4th & now 5th things were costly initially. There were always some people who panicked in every gen's era o_O 🙀 🤦‍♂️:ROFLMAO:
Also things will be costly more in capitalist countries than communist & socialst mixed economies.
Nobody knew that subsonic P-51 Mustang will be replaced by supersonic F-22. It is merely natural tech evolution & requirement.
Difficulty doesn't stop Development.

It's supposed to be relative to the previous one, not spanning across generations. The budget impact only takes the previous one into account.

Does that mean that Rafale was comproise by Dassault just bcoz a Naval jet needs stronger landing gear & lower speed stability. It is better to develop a common body jet 1st for Navy. N-AHCA =TEDBF 2.0 which can be a clean-sheet design, which can be used for AF too.

ADA has officially decided they won't be doing that. They stated that AMCA will be IAF-only. TEDBF will be the interim IN aircraft followed by a 6th gen clean-sheet CATOBAR-capable design. And then Dassault is Dassault, they have the experience to pull off such things, we may not have the capability and we do not want to follow in their footsteps anyway.

Rafale comes with performance trade-offs.

You wan't other nations to dictate our projects? Or you wan't our DoD to sit & wait for others to do things 1st & then beg for imports?
My last post showing F-22 & Su-57 diagrams was a step towards acertaining the size & weight of AHCA = Empty weight + fuel + internal payload. And regarding its engines, i won't be considering what GoI/GTRE BABUs will be doing at snail's pace but what is certainly doable in urgent mode.

I am talking about you and me, not DRDO.

You claim AHCA will be a massive aircraft, I believe we don't have the answer, and Mig-41 will give us (you and me and other readers on this forum) a clue about the size required for stratospheric performance. And my claim is we will need a smaller aircraft than the Mig-41.

Remember, the timeframe is 2055. NGAD, GCAP timeframe is 2030-35 and SCAF timeframe is 2040-45, ours is almos 30 years away. We are most definitely not gonna go for an equivalent.

Heavy jets like F-22, F-15, Su-57, Su-3X, J-20 are not just SLIGHTLY bigger & heavier than F-18 SH, MiG-29/35, Rafale, EF-2000.

We don't need such a jet. We only need at best a 15% bigger jet than AMCA, an AMCA Mk2. It can have an MTOW of 30T.

For that 1st you have to share your idea of realistic empty weight, fuel weight, internal payload weight. It is your vision of 7gen AHCA which will be much bigger & heavier than MKI.
But my idea is to technically come closer to NGAD, F/A-XX, GCAP, FCAS. If AHCA can be around MKI then it is very good.
As i highlighted some of the heavy jets above & the 6gen might be 30-50% heavier, & some custom AGMs carried internally & not just AAMs + DEW-CIWS, it is highly unlikely that their 6gen would be less voluminous & lighter than MKI.
But if we can package an AHCA jet near MKI, it is very good.

Mig-41 will provide us the template. We can't guess it yet. Mig-31's MTOW is 46T.

Depends on what things are in MLU. Both will have today's standards of computing but total computing power of F-22 would be higher as USA is ahead in H/w & S/w R&D. Also, we have just begun optical sensors R&D while they got DAS & HMDS in 1990s.

Avionics is subjective. LCA has more processing power than the current F-22.

But the current AMCA design has 25% more fuel fraction than the F-22. 0.29 vs 0.35, that's quite close to the F-35A. So AMCA will comfortably outrange the F-22. Being smaller and lighter means easier maintenance and faster turnaround time. So it's an F-22++.

That way by reducing fuel & matching with light/medium jet you are intentionally degrading the design purpose of heavy jet. That way it would be wrong to make a heavy jet in the 1st place. You forgot that when design weight increases then the thrust of engines are also researched to maintain or increase the TWR.
The light/medium jets would run out of fuel quickly while heavy jets would still have a lot & their aerodynamics & aglity is designed with more fuel.
50% fuel is taken as an adhoc measure bcoz different jets have different empty weight, engine weight, # of engines, SFC, thrust, fuel capacity. The jets start, taxi, takeoff, climb, reach the conflict zone, engage in BVR combat, then dogight begins. So 50% fuel might have been consumed already. But the airframe TWR is the only mathematical measure left.
For example, F-35 has 8-9 tons fuel,
Su-3X have 11 tons fuel,
F-22 has 8.2 tons fuel.
But F-22's F119 engines have lowest SFC which if coupled with higher fuel capacity & airframe TWR would give TRIPLE advantage.
In a TVC maneuver if a jet comes to zero speed then it should be able to accelerate fast upwards where the net thrust is lowest.

View attachment 35874

Fuel is managed depending on the mission. CAP and certain AS missions are conducted at 50-75% fuel, so dog fight happens at 25% or less fuel. Air combat is where TWR is most important. The MKI's packed with fuel for strike missions, which is G limited.

Learning lesson for entire world. USA won't repeat that mistake with NGAD, F/A-XX.

The current NGAD may get canceled. They are probably planning to make a smaller jet than earlier. If they turn it into a drone, then they can carry more ammo.

F/A-XX needs more weapons by default, it's not being designed for air superiority. The USN has officially proclaimed that they will surrender the penetration mission to the USAF's NGAD.

That's is exactly why 6gen has outlined DEW-CIWS to defeat multi-spectral AAMs. And that's why more attempts means more AAMs will be required.
Stealth missiles were tested but not materialized, IDK why.
View attachment 35890
View attachment 35891

Dunno how that would work. If a laser is capable of destroying AAMs, then AAMs will become useless.

So you do think that F-22 should have got higher IWB capacity.
But you don't want our products to get over those limits & mistakes, WHY?
Just like you quote dual-band AAM to close gap b/w RF BVR-AAM & IR-CCM, similarly i'm projecting an idea of AHCA to improve the economics per sortie & at least narrow gap b/w AMCA, TEDBF & NGAD, F/A-XX. We can't afford to severely lag again by an entire gen for next 50 years. Again it would like "Can't swallow, can't spit" :sick:❌🤮❌ 🤣
IAF chief said they have roadmap to 6gen. What is it? :rolleyes::unsure:😃

The F-22's bays are fine for its mission. They had planned a strike version called FB-22 with bigger bays and weapons pods meant to replace the F-15E.

CCAs will carry weapons because deploying weapons is dangerous work. The primary fighter could cost $100-150M+, but a drone could cost $30M, so they will risk the drone for weapons deployment.

The IAF reference to 6th gen is unmanned drones. Any program activation for MKI replacement is well after AMCA is flying, so it can happen only after AMCA's achieved IOC/FOC. ADA has to work on CCAs in the meantime, apart from IUSAV and FUFA. So don't expect anything concrete to begin until 2035. So whatever technology you are thinking of the IAF will want will have to reflect the times.
 
We need to go by our own timeframe, not others'.
WHO/WHAT decides the timeframe? >>>>. Natural evolution with time. So there is noting like going by others' timeframe. 1 country invents something & becomes leader in it & others try to follow & close the gap a.s.a.p. SIMPLE.
History is evident that most powerful leader tries to become invader, dictator, destroyer. Our scams & failed results have proven that our timeframe is lazy, lousy & also loosing if war happens suddenly & this same concern is shared by Ex-officials from armed forces on YouTube.

For example, the French completely skipped a stealth jet and Dassault claims the Rafale F5 is good enough until 2050, with a modernized Rafale taking over beyond that, which means they believe SCAF is unnecessary.
And now the USAF is doing a rethink on NGAD because they believe unmanned CCAs will surpass it by 2040.
The current NGAD may get canceled. They are probably planning to make a smaller jet than earlier. If they turn it into a drone, then they can carry more ammo.
> If there is news of cancellation of FCAS, please do share. Like we all know, in every era the latest gen is supplemented by previous gen, there is an overlap. So Rafale F5 will supplement FCAS.
> Misinformation, confusion, diversion are part of military tactics & USA is good at it. USA is still testing its UCAVs & yet to demonstrate group flight, coordination otherwise they will accidentally ram into eachother. Yes, 1 day USAF will be UCAV-AF but that transition will take 1 gen of time for AI & ML to mature fully but in full safe control of humans. USAF wants to field 6gen soon which will be MUMT (Manned UnManned Teaming) with CCA+PCA=NGAD. They can't abruplty fire their pilots or stop recruiting or it'll impact them economically, socially, politically.
> A giant AF cannot have only 1 big jet even after all 4.5gen jets retire. If at all they are planning a smaller jet then it could be a follow-on to F-35, a supplementary jet & may be the next export product. They may not export the bigger NGAD.

Which means our AMCA will be a better option than Rafale + modernized Rafale or F-22 + F-35 combo due to its relatively newer design.
> PLEASE LET'S DISCUSS AMCA IN ITS OWN THREAD. THIS THREAD WILL FOCUS ON SURPASSING AMCA IN CAPACITY.
> In general, every 5/5.5gen is supposed to defeat every 4.5gen jet most of the times. It is supposd to have 50-50 chance with any other 5gen jet including F-22, F-35, Su-57, J-20, J-31/35.
> But USA, Russia, China have operated 1 heavy & 1 medium category jet - F-15+F-16, Su-27/3X+MiG-29, F-22+F-35, Su-57+Su-75(very late unfortunately), J-20+J-31/35. We also operated MKI+MiG-29+others. Now we are going to make AMCA but leaving a hole in the heavy category, glorifying MKI & overconfidently depending on it & AMCA.
> You are simply not keeping patience to understand the limitations of smaller airframe & engines & why heavy jets with heavy engines have been created in the 1st place. Not just F-22, Su-57, J-20 but also previous gen Su-27/3X, F-15.
> AMCA airframe & its F414 engines are not sufficient - fuel, payload, electricity. Hence AHCA is the answer
> Let me repeat - We are making LCA, MWF, AMCA only bcoz we can't arrange a better engine by self/JV/import. If our GTRE or private sector could make engine like F119, F110, etc then we would also have a strong IAF with those big jets + global export market.

With drones taking over the regular AS mission, the IAF is going to need a true next gen capability after AMCA, not just an NGAD equivalent. And remember, we are talking 2055, so that's gonna have to be us skipping a generation.
> 1st let the drones/UCAVs be fielded & demonstrate practical success together in group, long time remaining for that.
> BUT you are the one who is thinking 2055+, i'm talking 2040s. You are leaving everything on AMCA for next 30-40yrs.
> You are talking about AFTER AMCA, i'm talking about parallel to AMCA with it being LSP.
> You spoke about 7gen, SCRamjet, that's NEXT TO NEXT GEN, while this thread's title/idea has 5.5/6gen. Anybody can peek way ahead into future & say that eventually we will need 8gen, 9gen, 10gen tech.
If you create a new appropriate thread on your vision, we all will discuss there.

Our plan is the same, we just want a much smaller jet because unlike their large territory which requires range and speed, we need higher endurance and turnaround. You don't get the latter two with a very large jet.
No, in your words, our plan is not same, bcoz your statements are self-contradictory. Larger territory also needs more fuel & higher endurance also needs more fuel. Our country is also sub-continental. Su-57 & Su-3X have similar internal fuel. Russia has MiG-31 fast interceptor for their continental country. Smaller jets means less fuel, less range, less endurance unless you can explain exactly the opposite. Using EFT means precious hard-point lost, bad for economics per sortie.
Also, please let's know your metric of light/medium/heavy jet so that we can understand eachother better.

Brahmos MA is being designed for 300 km range, perhaps 400 km. The MKIs will be able to use the 800+ km Brahmos-A variant in the near future.
Please don't go in circles. I already answered, again repeating - 4.5gen jets have higher RCS hence they require higher standoff range. Stealthy jet with stealthy weapons, less range required.

It's supposed to be relative to the previous one, not spanning across generations. The budget impact only takes the previous one into account.
A sedan will be costlier than hatchback in same segment with common features. You are deadly against big jets stating costly to maintaiin but supporting Su-30MKI. So that's another contradiction. Then we made mistake getting MKI also.

ADA has officially decided they won't be doing that. They stated that AMCA will be IAF-only. TEDBF will be the interim IN aircraft followed by a 6th gen clean-sheet CATOBAR-capable design. And then Dassault is Dassault, they have the experience to pull off such things, we may not have the capability and we do not want to follow in their footsteps anyway.

Rafale comes with performance trade-offs.
> Team discussions happens in all offices but we don't know who exactly makes the final verdict & based on what. But ADA/NAL has made bad decision bcoz enemy won't give discount to Navy with less capable SAMs & AAMs. If IN faces battle before they get stealth jet then there will be more losses than IAF. It is not personal opinion but the physics, chemistry, maths of technology, ask any tech grad student. ADA/NAL made another bad decision by using AL-31 for SU-30MKI & glorifying it but not for AHCA R&D. So the IAF will also suffer in that category.
> If we don't have the capability then we are destined to suffer.
> When we are not tech leader/inventor the we have to follow footsteps of technology evolution, not of any country.
> Naval jet will always have little bit trade-offs compared to AF jet, but that doesn't/shouldn't stop R&D. NGAD will progress doesn't mean F/A-XX won't. If Russia, Europe, etc can't field Naval jet corresponding to AF jet w.r.t. prevailing technologies then their Navy will also suffer.

I am talking about you and me, not DRDO.

You claim AHCA will be a massive aircraft, I believe we don't have the answer, and Mig-41 will give us (you and me and other readers on this forum) a clue about the size required for stratospheric performance. And my claim is we will need a smaller aircraft than the Mig-41.

Remember, the timeframe is 2055. NGAD, GCAP timeframe is 2030-35 and SCAF timeframe is 2040-45, ours is almos 30 years away. We are most definitely not gonna go for an equivalent.
Mig-41 will provide us the template. We can't guess it yet. Mig-31's MTOW is 46T.
> You are talking like Russian citizen or close ally. You wan't to wait for MiG-41 & learn from it but not NGAD, F/A-XX, FCAS, GCAP.
> You wan't ADA/NAL/HA/DRDO to wait for 5/10/15yrs or whenever Russia will disclose, develop & fly the MiG-41 & be dependent on them. But again a contradiction as you said we should foucs on our timeline. IDK if MiG-41 will be naval or not bcoz it is a Mig-31 follow-on, a long range fast interceptor, but my idea has to be naval. For a quick preliminary idea, just imagine a stealthy Naval Flanker with more IWB capacity. MTOW of Su-33 is 33 tons, Su-57 is 35 tons, add 3 more tons for more IWB capacity = 38 tons, same as for MKI.
> Hence I gave indication that my vision is inspired by Su-33 & global tech R&D, meaning F/A-XX actually. I also showed notional diagram of F-22 & Su-57 with more IWBs. So you can get the idea about rough size of AHCA. There is no need to wait for MiG-41. And you only said we should focus on our timeline, so that adds to more contradictions on your part.
> Like i said earlier, you are thinking about MiG-41, Stratospheric flight, 2055+ time, NOT ME. I'm not against your vision but it doesn't match this thread, it needs another thread category. How many times should i repeat? I sincerely request you to open a thread with title something like "Post AMCA capability 7gen concept - Stratospheric flight, SCRamjet, 2055+ timeline"

We don't need such a jet. We only need at best a 15% bigger jet than AMCA, an AMCA Mk2. It can have an MTOW of 30T.
> Some of us are saying that to hide our incapability to have a better engine.
>
That's what many people said since P-51 Mustang days in era of 1/2/3/4gen aircrafts. But makers didn't listen to them.
> By your logic it can also be said that we don't need 7gen stratospheric SCRamjet fighter needing huge fuel & money.
> MTOW 30T is basically trying to match J-35 & F-35. If N-AMCA is designed, it will need bigger wings & stronger LGs, meaning say 2 tons more. Its IWB has to be adjusted to carry custom AShMs, ARMs like West is designing. So its IWB capacty might increase from 1.5 to 2.5 tons. So your 30 tons gets consumed. But the internal fuel remains same & bcoz engines will remain same so the TWR will go down which may impact takeoff, landing, range, endurance.
My idea is little more ambitious by improving all aspects in ratio, that's all. You can disagree, no problem. But IDK if technology enables us to do something better then why would someone be adamant to oppose it desperately.

Avionics is subjective. LCA has more processing power than the current F-22.
My college senior worked on LCA & he indicated to us that LCA got redundant computers but more or less same as that of similar jet like Mirage-2000. While F-22's computer was equivalent to an average Cray Supercomputer.
A light 4gen jet simply doesn't have the components & hence requirements to have a Supercomputer or more processing power than world's costliest 5gen jet.

But the current AMCA design has 25% more fuel fraction than the F-22. 0.29 vs 0.35, that's quite close to the F-35A. So AMCA will comfortably outrange the F-22. Being smaller and lighter means easier maintenance and faster turnaround time. So it's an F-22++.
> PLEASE LET'S DISCUSS AMCA IN ITS OWN THREAD. THIS THREAD WILL FOCUS ON SURPASSING AMCA IN CAPACITY.
> Why are you mixing fuel fraction, range with H/w, S/w, avionics & going astray? Combination of many things like fuel consumption/SFC, quantity, aerodynamics, altitude, payload decide range, this is again the physics, chemistry, maths of technology, so fraction is merely a design aspect calculation which alone cannot decide range.
> Features & capacity are 2 different things. LCA, Gripen, Hurjet, Yak-130, JL-10, KAI FA-50, etc, all these light fighters also can be equiped with full glass cockpit, HMDS, even virtual cockpit, DAS, EOTS, SPJ if their engine can produce enough electricity but their payload, range, endurance is severly limited.
> BTW there should be only Tata Nano & selected hatch-backs from Maruti-Suzuki, on the roads, less purchase cost, less maintenance, cheap spare parts, easy to park & turn around. All Sedans, Station-wagos, SUVs, etc should be banned. Same thing with phones, TVs, clothes, watches, etc also. Same thing with military also - only light machine guns, light tanks, light artillery, light ships, light submarines, etc.
😵😵‍💫🤐:LOL:🤣


Fuel is managed depending on the mission. CAP and certain AS missions are conducted at 50-75% fuel, so dog fight happens at 25% or less fuel. Air combat is where TWR is most important. The MKI's packed with fuel for strike missions, which is G limited.
> Airframe design has evolved also, considering, economics, ergonomics, etc. Fossil fuel is precious even for the military. The fuel tanks are spread all over the airframe. Like you guys said they try to put fuel into rudders, CFTs, wherever they can.

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> In war time there are many scenarios which can be strategic/pre-planned or dynamic/tactical.
> Often the multiple task forces are loitering to create false attack impressions, diversions & then suddenly 1 of them do the actual attack. So at least 1/3rd fuel is gone there only.
> In another scenario, a jet fighter can be launched from forward airbases near border in offense/retaliation/strike or defence.
> If a 5gen jet has successfully used half of internal weapons AAMs/AGMs it might be ordered to loiter or re-engage somewhere means optimal use of fuel capacity.
> Either ways, to escape from SAMs, AAMs it can be expected to change orientation any time. And with enemy stealth fighter a BVR evasion maneuver or dogfight can begin anytime. So if a 5gen jet fighter cannot take off with full fuel & perform then its design & performance are compromised.
> Today's & few more decades of manned dogfight would be using HMDS & LOAL AAMs which reduces using afterburner maneuver to get into AAM seeker FoV to lock.
> So far we have referred EFTs as DROP tanks, means take off with them but get rid of them after using fuel 1st from them. But 5gen onwards focusses on carrying hat fuel internally. That's what i put it in my 1st intro post but you don't want to understand that.

1725780480228.png


> Hence taking off with full fuel is important.
> Moreover, fuel is continiously re-distributed evenly across airframe to maintain the CoG (Center of Gravity) so that a 5gen jet fighter can perform any time.

F/A-XX needs more weapons by default, it's not being designed for air superiority. The USN has officially proclaimed that they will surrender the penetration mission to the USAF's NGAD.
> It doesn't mean the world will follow same doctrine & industrial decisions. And you also said we should not follow footsteps of other countries.
> Moreover USA has bases globally to participate in any war anytime. It can be flexible with its doctrine. It can send B-2, B-21 then F/A-XX but when you say it needs more weapons also means it can have versatile roles in stealth & non-stealth configs.

Dunno how that would work. If a laser is capable of destroying AAMs, then AAMs will become useless.
The only way forward to defeat missile is to disrupt or destroy. Disrupting will also suffice.
The DEW R&D started in 1980s i think in era of STAR WARS, not the movie, i mean SDI or Strategic Defence Initiative. It is still progressing. Mobile platforms have been tested on ships, trucks, helicopters, etc. Our DRDO also seems to be working on it.

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The F-22's bays are fine for its mission. They had planned a strike version called FB-22 with bigger bays and weapons pods meant to replace the F-15E.
> If any jet was FINE then it wouldn't require MLU or next gen airframe, SIMPLE. In my understanding they didn't make the FB-22 bcoz of following reasons :
> Engine tech was not at VCE stage in 1980s/90s with higher thrust for TWR.
> Hence FB-22 would not be able to dogfight well. Astonishingly F-22 didn't field certain things like HMDS, EOTS, IRST which might come now in its MLU.
> But they can't MLU the IWB, an airframe limit, hence next gen leap with NGAD.
> Private firms can burn cash & push ahead of time but technology fails also if pushed ahead of time. But BUSINESS CONTINUITY is required to employ 1000s, may be 10,000s of people in supply chain. So USA will push only that much as per capability of rest of the world to stay just 1 step/gen ahead.
> In 1980s they planned YF-22, YF-23 with upto 8 internal AAMs when nobody across planet thought or confident about it.
Today they are planning to increase internal payload by compacting other components, but also realizing that to maintain TWR better engines are required, hence R&D on XA-100/101/102/103 which will be bigger & heavier than F119 & F135 engines.
Now they can create FB-22 in form of NGAD, F/A-XX to be multi-role. Below is combo of 2 pics edited to show notional size comparison.

1725810938470.png


CCAs will carry weapons because deploying weapons is dangerous work. The primary fighter could cost $100-150M+, but a drone could cost $30M, so they will risk the drone for weapons deployment.
IDK how a UCAV Wingman can cost just 20-25% of manned fighter unless you or someone can precisely explain.
> The UCAV also needs radar, sensors, cooling systems, comms, auxilliary equipments. The only thing less will be cockpit with its OBOGS, HVAC, ejection seat for pilot. But some people say it can be optionally manned, then it has to fly with empty cockpit.
> The UCAV will have to do the dashing, intercepting, dogfighting.
> I already said - If manned fighter is devoid of weapons then it becomes a stealth ISTAR jet. Why to develop high thrust VCE with reduced SFC for manned jet? Instead, pass instriction to UCAVs via sat-com or AEW&C jet with high BPR engines with high SFC. The manned jet needs something for self-protection for sneaking enemy.
> Hence, in order for a UCAV to qualify as Wingman, it needs to fly with manned jet when & where required.

All above points means UCAV Wingman should have same foundation aspects of endurance, speed, fuel capacity, avionics of a 5.5/6gen manned jet. And hence it canot cost 20-25% less than the manned jet.

The IAF reference to 6th gen is unmanned drones. Any program activation for MKI replacement is well after AMCA is flying, so it can happen only after AMCA's achieved IOC/FOC. ADA has to work on CCAs in the meantime, apart from IUSAV and FUFA. So don't expect anything concrete to begin until 2035. So whatever technology you are thinking of the IAF will want will have to reflect the times.
> DRDO/ADA/NAL progress on UCAV is very slow. But that's just the unmanned part. The manned part of the puzzle is missing. That's 1 of the points i noticed while making this thread.
> If citizens like me should not expect & express then all forum websites should be banned in our country. Just chill & watch news, pray to god that war should not happen till we field AMCA, FUFA, PAPA, MAMA, etc🤦‍♂️:ROFLMAO: in good numbers. The GoI/MoD/DoD, not willing to expand human resource & facilities, will operate in TOTALITARIAN mode rather than DEMOCRATIC, which will be SUICIDAL for entire country.
> Anyways, 6gen will be MUMT, so if people can glorify MKI then they can certainly tolerate a much better stealth jet with AL-31 engines if we can't get F110 or AL-41 w/o ToT.