I may be wrong,but that hexagone in the nose is probably the IRST room??
Since i don’t see it, neither seems to be dissambled, i mean, the IRST room that flew in the first flight did have other location, i don’t see any kind of instalation on that place
Those hexagonal shapes are visible in the T-50 prototype that flew as well, so I would guess no. Plus it leaves very little room for the radar if thats the case.
Or.. The Russians know something we dont. For example they may know/assume that a new line of airborne sensors soon will render the current stealth technology (Raptor, JSF, T-50 etc) not obsolete, but significantely less of the seemingly invincible game changer it is today.
Ah yes…the typical answer. If the Russians didn’t do it, it must be because they know something else nobody knows yet. If they think stealth will be irrelevant, why take the effort to build the T-50 in the first place.
compare that to the careful LO shaping observed on forward fuselage wing ,engine intake S Duct,wings and upper fuselage.
Ah here we go with the “s-ducts” thing again…even though every piece of evidence suggests there are no such things in the T-50. Now someone mentioned something about Russians not being able to change physics…well thats the same case here…there’s just no room in there for something of the sort. The frontal LO shaping isn’t all that extensive for some very important reasons…first of all the lack of total hiding for the engine face and the fact that from even most frontal angles you will get a good view of that conventional underside.
So lets just slap a B-1B intake into it 🙂
Fact of the matter still remains that no one can yet produce a possible means they achieved total concealment of the engine face with those engine nacelles.
The Russian’s thinking with this is to take the Eurocanard concept a step further…ie focus on signature reduction under certain parameters and rely on EW. Its not the same approach as the F-22, or even F-35. Not that this is necessarily a bad approach.
Yes, the EU is very large, but in practical termes is bankrupted, just like USA, printing endless columns of painted paper to try to control the crisis that they unleashed.
Love these tid bits of educated comments based on youtube videos. Very entertaining. Of course…they’ve been saying the US economy was bankrupt since the 70s. 😉 The US economy is very far from serious trouble the way Russia’s economy is…all it needs is for Barack to be a one-term president. But I digress.
Anyway…
…Anyone wondering that if there is export of western aircraft to Ukraine (like Grippen), there is an almost guaranteed chance of technology leakage to the Russians? I don’t know if the US will allow the sale of any aircraft carrying AIM-120s or other sensitive components to a nation like Ukraine.
Kapedani, thanks for the constructive criticism. I disagree for what it’s worth. I think that the photos clearly indicate that the landing gear retracts into the side of the intake area not upwards into the wing root.
It shows nothing of the sort.
S-bend in my sketch is intended to show as both upwards and laterally,
You tried to fit a curvature that is neither possible nor functional. You can try and fit it anyway you want…it just won’t fit into the T-50
Are you nuts?
On a 9+g fighter, you are seriously trying to suggest they would have a wheel well at the wing root instead of structure?
It retracts as the drawing suggests. It retracts as is clearly visible from the underside image of the T-50 (you see clearly the space for the main wheel to retract parallel with the wing)

Bingo 🙂 Which is what I have been saying all along and which is the only possible arrangement in this plane. The main wheel retracts into the WING ROOT…and the air intake has to go UNDERNEATH the main undercarriage to the engine. Its pretty obvious…from every picture…
And of course as I’v been pointing out all along…there is no way to fully shield that engine face with that intake.
So yes, there’s probably a radar blocker on that engine face. The issue remains, that none of the aircraft that have such a thing achieve the same level of stealth as the arrangement on the F-22.

This is a completely wrong arrangement for some very fundamental reasons.
First of all in order to achieve that geometry inside the air intake, the air intake has to protrude INTO the area of the weapons bay…which the external shape of the engine nacelles doesn’t suggest at all. Second, to do so it will need to narrow extremely at that point…hardly something achievable. You’ve tried very hard to fit it into an area and into a configuration it can’t possibly fit.
You can use movable LERX to improve aerodynamics and stealth.
This isn’t completely mutually exclusive and you might need to sacrifice some stealth in that process, indeed.
Which is what I was trying to get at.
I don’t think any poor ******* has ever won a war by having more economical aircraft than the enemy
Then you better recheck your history, namely WW2.
In my next sentence I said precisely that 😉 Other than WW2…but thats a whole other animal.
PAKFA doesn’t need to fly as fast, doesn’t need to be as stealthy and doesn’t need to have sensors as good as F22, if there’s 2.5 times more of them.
It would be even better if there were 4 times more of them…and less capabilities too 🙂 But thats not a very convincing argument. (besides as was pointed out, this aircraft will not cost 2.5 times less than F-22…and its unlikely there will be anywhere near more of them in 20 years time). But I realize these are all hypothetical scenarios.
The real issue is…this isn’t an aircraft that can directly be compared to the F-22…
More notions…F22’s superior stealth, sensors, cruising…
You don’t know PAKFA’s stealth, sensors, cruising, so how can you draw a conclusion of which is superior and to a what degree?
As I recall you said the T-50 will be “just as good” as the F-22 but at a lower price 🙂 (due to hypothetically being able to be build in larger numbers (how Russia will do this…remains a puzzle)). I made no such claims.
But we can infer of its stealth capabilities from the pictures we’re seeing. We can infer of its sensors capabilities by observing the capabilities of the Russian industry at this level…Now I know there will be a multitude of fanboys jumping up and down at this…
Well, I took Mig25’s example to prove a point of the necessity to superimpose one’s way of fighting.
Which the Coalition did quite well. Taking one exception to the overarching rule…

Now what we see here is a very conventional intake with variable geometry…which indeed poses a very serious concern. (which is what I’ve been trying to say the whole time).
(and nobody has yet to answer my question as to what implication on stealth does a variable geometry intake have?)
The problem is, the radar energy does not behave like air. It is not of intrest how much did enter the inlet, but how much of that will leave it to give a signal from that. As long there is a direct line of “sight” some problems are still alive.
It may not matter too much, when some higher peaks are created in other areas of the Su-50. The first impression does show, the Su-50 is a semi-stealth design for cost and flying performance reasons.
Exactly.
The problem is that we don’t know enough about this intake, there are at least 2 pictures showing interesting structures on it, something is going on, but we don’t know yet what is exactly.
The “interesting structures” you see are the variable geometry intake. Looking at the external shape of those engine nacelles…the only conclusion that can be reached are the above drawings showing the internals of the intake…and these show a relatively conventional intake because there’s little other shape you can fit in there.
AFAIK, insetting elements (like wheel doors f.e.) can be EM sealed, so I don’t think this is a problem.
The trouble with canards is that they’re in front of the wing in comparison to elevators and reflect when elevators wouldn’t, being in wing’s EM shadow.
PAKFA’s edge over the intake is exposed anyway (no resemblance to canards), so why not add extra ability to improve flying characteristics, or deflect it to reduce RCS at certain angles?
Ok I get this. But the issue remains that in order to use this for improving aerodynamic conditions…you might end up sacrificing some towards stealth in those circumstances (well yes you say you can deflect it to particular angles to reduce RCS…but you’re either using it to optimize RCS or you’re using it to improve flight characteristics. Besides…how do you know which angle to set thing thing in case you’re trying to reduce RCS at certain angles without knowing where the viewing radar is first?)
Maybe it’s because F22 was designed in the times when SSSR was fielding SAMs by the thousands, on a relatively small space of German border.
Fighting in those conditions would give F22 operational autonomy to try to perform quick attacks against SSSR’s high value targets (AWACS, Heavy transporters, etc…).
So stealth.
UCAVs are something else.
They don’t have neither performance nor a pilot to assess the situation properly, so are much more reliant on passive defenses like LO.
So one would say the US move hasn’t been anywhere the same as the Russians (in their brochures)…not focused on aerodynamics and manuvrability for air-show tricks…but rather towards more stealth, smarter weapons, smarter sensors…that negate the need for extreme aerodynamic performances. Anyway not that important…I was just trying to poke at you.
In the aspect that gets forgotten most of the time, but is the determining factor in fighting the war…cost/effectiveness performance.
I don’t think any poor ******* has ever won a war by having more economical aircraft than the enemy 🙂
Unless we’re talking an all-out fight to the death WW2 style war with no end in sight till someone dies…the determining factor of victory in the air is the guy who has the best toys, the best pilots and the best systems to support it…even if outnumbered.
Which is why I disagree with your notion that since this T-50 may…might…hypothetically…fly better than the F-22, that it is worth the effort because it is “cheaper”.
So, if Sukhoi manages to make a plane doing M1.5 SC with comparable range and similar weapon load, but at a 2.5 times less price that’s more than enough to offset any advantages F22 might have in terms of pure performance.
I’ll have to absolutely completely disagree on that one. If you spend 2.5 times less then me to fly faster, to fly further, to carry more…but still manage to not see me…then you haven’t done much.
That’s true, but…
That difference appears to be too small by comparison to other aircraft and corresponding numbers in the field.
Many ppl here compare planes 1 on 1.
It doesn’t work that way and this is why the wars are fought by armies, not individuals.
In some distant times, warlords would have go 1 on 1, to determine the winner and spare the soldiers of slaughter.
Undoubtedly. In that case I don’t think any F-35 operator in the future will have much to worry about the T-50 to begin with (all the 2 nations that will possibly ever field this plane 20 years from now).
As for raw performance, I can think of at least 3 aircraft that do key things better than F22.
F22 possibly covers most aspects of air combat in the most balanced way, but that doesn’t mean it’s the best in each and every category and mostly isn’t.
Except for stealth and sensors (and cruising)…ie it can see better then anyone out there, and can’t be seen by anyone out there. I don’t know of a more important aspect of air combat than that.
The thing is Mig25 killed F18 in GW, in spite the fact that most ppl would say Mig29 will do that and that one haven’t scored a single hit, let alone kill.
So, the victor is the one that manages to superimpose the way of fighting that suits him best, at his opponent.
I’m sorry but thats not very sound. The second sentence is very sound…the first one though means very little. Yes a MiG-25 scored a kill. It also lost more than a few 😉 There’s few better examples of imposing the way of fighting that suits one best on the opponent then GW1.
USAF will continue win (or loose?) aerial battles, mostly due it’s “logistic” assets and F22 contribution here is much lower than popularly presented (mainly to justify enormous expenses).
🙂 Now you just said “The T-50 will do what the F-22 does at a cheaper price” 🙂 The F-22 provides the spear tip to an immensely extensive US battle system…and does so like no other aircraft in the world…thanks to its stealth and sensors.
What exactly does the T-50 do similarly?? It can super-cruise faster and further (in a hypothetical scenario…about an engine that doesn’t exist…on an aircraft whose performance is unknown)? Does it represent any similar capability as the F-22? Unlikely. Does it represent a game-changer in such a scenario? Unlikely.
What does it represent? A cheaper (though not necessarily better) alternative to a Eurocanard for nations that can’t afford one or aren’t allowed one.
So as I said earlier…when is the point that we want to admit to ourselves…that that is NOT the target being aimed at? Because we can’t reach that target 😉
The flyaway price of the lasts F 22 delivered was around 140 mil $. I doubt that the PAK FA could cost ~ 60 mil. Today advanced version of Su 30/35 cost more.
Yep. As I said…what is the performance level improvement (purely hypothetical) that I need to achieve in order to say that the trade-off in stealth and sensors was “worth the price”?
From here on in, do not quote me or refer to me in any way, shape or form.
Clearly, we are not from the same planet. Our worlds should never meet.
Thankyou.
You can rest assured that every time I do so…I do so with great distress 🙂
I think both.
EF claims to deflect canards to mitigate RCS and “slab” verticals (haven’t seen one since A-5), are most certainly put on PAKFA with that purpose in mind, as well.
To mitigate RCS for the purposes of the aerodynamic use of the movable lerx. That still doesn’t tell us…if this movable lerx…despite its…hypothetical…optimization for RCS reduction doesn’t actually add to the problem of stealth as opposed to not having one. ie…not having canards is better for stealth than having them, but since you’re going to have them you can optimize them a little better…
Or am I just misunderstanding this entirely? Either way I’m sure this just adds complexity to its stealth characteristics…
Why do you think F35 doesn’t (and EF and others, for that matter) hide it’s canopy-jetpipe ridge (engine cowling)?
Because normally the only angle it can be seen is generally higher and perpendicular, meaning F35 is already beam riding the radar, so no need to further stealthify that part.
Well the F-35 wasn’t designed for all-around stealth. Neither the EF. Neither seems to be the T-50. But then there are always magnitudes…even though not optimized for all around stealth, some are just better then others.
Then the question becomes…why the much greater care for the F-22? (furthermore my impression is that the care taken in the F-35 or the eurocanards in that regards still seems much greater than the standard Su-27 engine nacelles or underside of the T-50)
I don’t know. That’s why I said hypothetical.
I know. I’m not expecting an answer. I’m just trying to get some perspective going on here (for the thread overall) instead of just letting typical fanboy euphoria go unchecked.
you’re the only one replying though and I appreciate that 🙂
Well US most certainly don’t insist on lower and lower RCS, as is seen from F22 < F35 RCS relationship.
Or one could say it is represented in the even higher stealth of UCAV designs 😉 (which are really the follow-ons to the F-22) F-35 is the cheap version to be used on day 2 of the war when there ain’t nobody else left to fight.
So, I think Russians made a better choice (true, they had the time to study F22 flaws) in terms of LO/performance trade off and should be able to achieve F22’s performance at lower price tag.
In what respect in performance do you assume the T-50 exceeds the F-22…in order to justify what is undoubtedly a much lower level of stealth? (when you say…”F-22 performance”…are you referring simply to flight characteristics or to actual war fighting capabilities? Because the first one I might accept…but the second one…ehh…being a function of the plane’s flight characteristics, stealth characteristics, sensor suite, weapons suite, pilot etc etc…I highly doubt that)
I’m no expert but I don’t see in the F-22 an aircraft lacking in performance. And of course a huge piece of the equation here will be capabilities of the sensors of the two aircraft. Now one can go on hypothesizing quite a bit on the mock-ups and brochures the Russians distribute at air shows…but thats another story.
In the end…the aircraft that sees the other guy first, locks on first and fires first…has the advantage. Now what sort of “performance edge” would I want to have over the F-22…in order to say with a straight face that my tradeoff in terms of stealth is worth it? (of course the level of hypothesizing here gets exponentially bigger when talking about an aircraft where the engines or the radar or any sensors are yet to exist)
In that case…an even heavier investment in ECM technology and load-out…put into a super-flanker…would make more sense since it trades nothing in performance, and hopefully takes away the F-22s advantage in seeing me first and killing me first.
Or do I just want to admit to myself…that maybe that isn’t my real target? 😉
In terms of pure interception, Mig31 and B-1R are most certainly better performers than F22, but lack fighter (maneuverability) component.
F22 represents one “school” of combat and will be victorious, only as long as it manages to superimpose the way the “school” that made it, fights.
In terms of pure flight performance…yes. In terms of seeing and being seen…hmm…
In my mind thats just a fancy way of saying that I’m bigger and faster and stronger then you…but I just can’t see you.
Anyway now we’re really getting off into the realm of pure assumptions and theories.
Pssst…Guys just say he’s right and maybe he’ll go away (forever).
OH MY GOD!!!!! HOW THE HELL DID THAT GUY GET HOLD OF PAK-FA’S BLUE-PRINTS……HOW COULD I HAVE BEEN SOOOOO WRONG!!!!!!DAMN YOU TO HELL HIGH-RES DIGITAL SLR…….HOW THE GODS MOCK ME!!!!!!
Its quite amazing how suiting that picture next to your name is…or how you haven’t been banned long ago.
To Kapedani
http://www.aviapedia.com/files/fight…A/PAK-FA-2.jpg
That’s the kind of picture I was looking for wrt the inlet/air-duct/engine issue.
Maybe I’m wrong but the way I see it in this pic, the air-duct needs to make a really significant turn (horizontal plain) in order to get to the engine. Especially if you enlarge it.
Generally speaking, it seems highly implausible, virtually impossible, at least to me, that the designers wouldn’t take care of this issue. In terms of achieving stealth, it’s just too basic of a problem for them not to take a good care of.
FW
Looking at that picture one gets no impression of what is going on.
This gives you a good representation of what is going on:
http://i46.tinypic.com/2mrfj4n.jpg
Hey haavarla, (Re: pic below see those elongated yellow panels in line with the engines, centre-fuselage? do they look directly in-line with the intakes to you? that’s the ‘roof’ of the S-duct
Again…look above.
In any case, that pic from Quadro and Otaku clearly shows intake work done by the russians to hide the blades.
Clearly they show nothing of the sort as the picture only shows the entrance to the duct…and shows nothing to indicate any curvature inside the duct (and the external shape of the duct leaves little room for anything of the sort)
it seems highly implausible, virtually impossible, at least to me, that the designers wouldn’t take care of this issue. In terms of achieving stealth, it’s just too basic of a problem for them not to take a good care of.
Undoubtedly there are measures taken such as RAM coating (which the Russians have experimented with) inside for example or some partial shielding (as the intake has to go…UNDER (Otaku!)…the main gear). But the question remains as to the actual… effectiveness…of such a measure as compared to the F-22.
Again, there are half a dozen aircraft which also take such measures…but one can argue that none of them achieve the same effectiveness as a true VLO design like the F-22.
It is a question of…magnitude of the effectiveness. If the Sukhoi designers were willing to sacrifice stealth from most angles below the centerline (with that conventional underside), in exchange for flight performance, then the question can legitimately be asked…”what else did they sacrifice inside those intakes for performance?”. Then you’re building something along the Euro-canard mentality of “reduce RCS as much as possible till we can theoretically cover it with EW, without sacrificing flight performance”. I don’t know how much that qualifies as “5th generation”.
Once you are maneuvering that hard there’s a good chance the leading edge flaps will start to move as well, not to mention you’re probably close enough to your opponent that you can cease to worry about stealth.
Agreed…if it comes down to maneuvering you’re already too close. My specific question is for using a movable lerx for controlling airflow to the intake…which might require it to be in different positions even while in non-maneuvering flight
In case of a hypothetical war, the winner of the air battle will be the one who will destroy the oponent’s stealth aircraft on the ground. The aircraft that has the advantage is not the one that is slightly stealthier than the other, but the one that has longer legs.
And if the quoted range (to be confirmed) of the T-50 at 5500km is correct, then it will be operating from airfields that are out of range of the Raptor.
Checkmate (Russian style).
Hmm…that is completely false.
If the Americans could do that 20 years ago, then they should be able to deploy an even better IRST now….and screw the heavy, expensive and self-exposing radars.
But wait….on their Raptor, they installed a radar but no IRST
Thats because an IRST isn’t a replacement for a radar by a long shot.
Regarding the T-50’s inlet, how many here know whether or not it has a fan blocker?
That’s what I thought.
Don’t get me wrong, watching you guys argue over how much you don’t know about this aircraft is entertaining. But I would be willing to bet the PAK-FA will come close to, if not meet, it’s design requirements. Since that includes a low frontal RCS, you can bet the fan won’t be detectable from the forward aspect, regardless of how it’s achieved.
Its interesting how many “bets” T-50 fans out there want to make.
Either way, you don’t seem to understand what I’m trying to argue here. Yes in all likelihood it will have some sort of RAM blocker or other sort of treatment. That STILL doesn’t say much of anything…in terms of how effective these measures are…as compared to the measures taken on the F-22 for example (there’s half a dozen aircraft out there who employ some forms of blockers and some forms of curvature to hide partially the engine face…but there’s little doubt that none are as effective as the measures on the F-22).
Its a question of how much…not if.
1) and 2), are most probably the same…a !!conditionally!! called variable geometry intake.
However, it doesn’t impede RCS as such and is variable (most probably) due the necessity to reposition edge according to EW/RWS/FCS command to mitigate RCS, against specific angle of inbound beam and to increase fuselage lift and effectively reduce alpha, at large angles.
Ok but we can see these things moving in the video…and I’d assume not in response to the need to align to any inbound beams. My concern is whether these things are going to be fluttering around on a regular basis during flight…or whether if they are used as variable geometry inlets then they will not necessarily be aligned to the best angle for stealth.
3) I’d agree and such layout will certainly increase RCS from side/below.
In head-on situation it’s irrelevant though and so, the RCS increase is noticeable from lower/ground and side positioned radars, only.
On the other hand, PAKFA gained a load of body lift and enhanced directional stability, which in turn allowed smaller vertical stabilizers.
This should enable some very slow speed flying with half wing stalled, which will happen quite often with such sharp sweep angle.
Certainly it has implication to flight characteristics…but also saying that it limits RCS reduction only to completely straight viewing angles and above…but any viewing angles below that are compromised.
In my opinion thats a big detractor.
4) You don’t know if engines are exposed and the intake pipe can be constructed as an anechoic chamber, to actually attenuate signal when sheathed with RAM coating and of particular dimensions, for predefined frequency and inbound angles range.
So, theoretically one could have engine’s fan fully exposed and yet has the most of the signal dampened within the intake volume.
On the other hand, PAKFA gained significant “tailboat” drag reduction in comparison to F22, which will eventually enable the same performance with smaller thrust (smaller engines), which will further translate into longer range, simpler maintenance, etc…
Yep aerodynamic advantages aside…my question is whether these…”hypothetical”…anechoing alignments will be as effective or effective enough….ie…what is “most” in a “marble size” argument? (yes I know the marble size is much more complicated than that…but you know what I mean)
) From RCS point of view, a drawback. From sensor’s, immense help, particularly if radar readings are unreliable, due ECM or LO opposition.
Not questioning the usefulness of an IRST…just the particular choice of layout.
Yes I know someone will say “they will change it”. So why did they put it in in the first place? Bad move by any measure.
Now, the choice of aerodynamic/stealth features the Sukhoi’s designers made is interesting and points toward the frontal RCS reduction mainly.
Yes its obvious it is mainly frontal RCS reduction. The question still remains…how much?
Furthermore…if the aim here was to create an aircraft with good aerodynamics and performance (which I don’t know if anyone can claim the F-22 doesn’t have)…and not have stealth limit this (meaning can’t make a true 5-th generation aircraft)…then what exactly is the point of such an exercise? Or more correctly…why haven’t the American’s figured this out but insist on smaller and smaller RCS (if as according to you this Russian approach was well thought out. In my opinion…it was the best they could do…and possibly a rush job at that). This then becomes Eurocanards thinking.
This points toward different prioritization of design and clearly shows Sukhoi’s confidence for an ECM system to substitute for any LO gaps.
I would not want to take that gamble with the F-22 🙂
I’ve taken your advice and did some reading and this is what I came up with: The Russians built an one-of-a-kind MiG-21 technology demonstrator that has a RCS of 0.25 sq m.
A clean MiG-21 has an RCS in the range of 1m^2. This represents a 4x reduction…What does that translate to in terms of range reduction? I don’t stand by these numbers…but I recall reading somewhere that one needed a 16x reduction in RCS to half the detection range from the same radar. If thats the case…this Russian experiment doesn’t seem to impress anyone.
Originally Posted by Kapedani
Now besides the intake…can someone please explain to me the implications for stealth of the following features:1) Movable lerx
Not that great I’d guess, similar to a leading edge flap on the wing as opposed to a fixed leading edge – something both the F-35 and F-22 have.
I don’t know much about this…but how often during the flight envelope of the F-22 do they use leading edge flaps…as opposed to how often would this movable lerx be used? I don’t know if I’m thinking about this right…but a movable lerx used to adjust intake into the engine or for maneuvering purposes…might be a liability in terms of stealth.
Originally Posted by Kapedani
2) Variable intake
Might be the same thing as the movable LERX – are we certain that it has variable intake ramps in the same sense as the Su-27? Keep in mind, IIRC this claim originates from an unofficial comment translated into English before the first pictures were released, it may well be that the movable LERX was considered to be part of the inlet system by the source.
I don’t know…I assumed it had them judging from the pictures and what was said about it.
In any case…lets assume for a moment it does. What are the implications for stealth here (as opposed to every other VLO design which didn’t have them)
Originally Posted by Kapedani
4) cylindrical engine nacelles and unsheathed engines
The nozzles may not be the final design, is it even confirmed that the engine is not an interim type? As for the round nacelles, their impact can’t be all that huge, otherwise where would that leave the F-35?
The engine may change…but long cylindrical nacelles running along most of the side length…will require a much deeper design change. And I don’t think the F-35 compares (though it itself had to tradeoff some side and rear RCS…but in the T-50 it seems as if no care was taken whatsoever other than grafting an Su-27 design in there)
I don’t think it needs to have a similar RCS to the F-22 in oder to be considered a VLO aircraft. Is the F-35 not a VLO design? Because I think a production version is going to be *a lot* closer to that than to the Super Hornet or an Eurocanard.
Well the chasm between the F-35 and the Eurocanards…may be very large. Saying it will be closer to one or the other…may in the end not be saying much at all.
What are you basing your belief about the Dutch Frigate detecting the F-22 at 150km being accurate on? I’m pretty skeptical of any story about an F-22 being used to strafe a naval vessel, much less a figure given for detection ranges, without info on the F-22(i.e. did it have RCS enhancers, EFTs, etc…).
I’m not sure but there is something fishy about F-22s flying even with NATO allies without some sort of masking for their real stealth capabilities…or practice strafing frigates for that matter.I’m not passing judgement…just wondering with how much salt one should take this story?
and in the hi res pics its visible the engines arent on intake plan
Look at underside picture to really understand 😉
(I’ll apologize before hand because I’ll probably quote a lot of things in this post…I haven’t seen this thread in some days)
omething to do with the “Blind Swordsman” tactics.
If two stealth fighters meet in combat at BVR range, most likely both of them will stop radar emission to avoid detection from each other. The fighter with the IRST can still “see” though, giving him a distinct advantage over the one lacking it. Besides 2nd generation IRST(based on QWIP technology) would probably extend detection range out to 70 nm. If anything, next update of F-22 may include IRST.
I’m not arguing the usefulness of the IRST (although your argument works only if both stealth aircraft have similar levels of stealth and detection capability…;) ) The question was concerning the design Sukhoi chose to put on this prototype (whether they change it or not latter is another issue). Clearly the way it is now…it is a liability for stealth.

That is the B-1s intake arrangement. First of all such an arrangement wouldn’t work on the T-50 (to see why not one only has to try and fit those shapes inside the T-50’s intake 😉 ) and secondly…the question still remains as to HOW effective it is in comparison to the F-22’s approach.
What is the probability of two fighter going against each other to be EXACTLY on a straight line facing each other ? The turbine blades are so deep inside intake cavity that a few degrees off the straight line into sideways and they are invisible. But by that distance you already have other detection mechanisms operating such as OLS etc. At long distances IR signals are weak because of lower energy.
Sure. There’s still a big problem because there’s a pretty wide frontal angle from where the engine blades can be seen.
So, if a poster has some doubts about a prototype, of a new design, in a a totally new field for the Russians (stealth), that just made 40 min first flight, try to answer him with facts; maybe he just doesn’t share your excitement, that’s all.
Blasphemy! Shame on you 😉
In a short while PAK-FA will be moved to LII, Zhukovskii, and when someone (like ‘Airwolf’) produces clear pictures of the MLG retracting into the intake cavity (including that sizeable wheel) his entire rabidly retarded argument will fall apart.
Yet another beautiful example of the level of discourse we’re limiting ourselves to. Good job Otaku.
Have you actually looked at the DAS installation on the F-35? You might want to before suggesting it’s the same as Sukhoi’s giant ball.
My point exactly
Hardly important unless we have series version of the T-50. X-35 didn’t have any IRST, right?
Agreed. So the question then becomes…why put a mock-up of an IRST ball on this thing when you have no intention of using that configuration to begin with?
PS. Kapedani ironically the aircraft you have shown doesnt have any new revolutionary technology on it as someone already pointed out it is mixture of old technologies.
🙂 I put that as a joke (or maybe not)…to keep things in perspective. It is amazing how underestimated keeping things in perspective is 😉
can someone please explain to me the implications for stealth of the following features:
1)flaps
2)slats
3)rudders
4)airelons?
Cute.
Now besides the intake…can someone please explain to me the implications for stealth of the following features:
1) Movable lerx
2) Variable intake
3) The Su-27 style underside (a big detractor in my opinion)
4) cylindrical engine nacelles and unsheathed engines
5) IRST ball on front ( maybe in future generations that will go)
As it is laid out so far, this aircraft clearly cannot have the stealth characteristics approaching the F-22 by a long shot. (yes I know I know…there’ll be lots of personal pointless comments).
Just looking at that underside and at that engine arrangement…
It has fairly beaten both F-22(air-superiority) & F-35(bomb truck) in their own two respective roles as PAK-FA have combined the two into one single airframe, without compromising on either! Brilliant!
Quite a bold statement there, given that the F-22s air superiority role and the F-35s “bomb truck” role depend heavily on their stealth characteristics and even more on the electronics of those aircraft. (forgetting for a moment that those definitions of their roles aren’t true…or the weapons)
It is Sukhoi’s answer to capture the light/medium & heavy fighter market with a single aircraft!
How does it capture the “light and medium” market? This thing will be more expensive then any Flanker derivative.
Its not a “stealth” a/c like F-22 or F-35, but just a “LO” a/c thats meant for combat….
Perhaps the most sensible thing said so far here.