Actionjackson said The surface angles of the yf-23’s side surfaces were significantly more canted than the f-22’s.
The angle of the f-22’s side surfaces are 55 degrees from horizontal, the yf-23 was around 35 degrees. This accounts for the difference in allround RCS.
The PAK fa has some surfaces canted at 65 degrees like the f-35 and j-20, however it also has surfaces at 75 and 85 degrees like non-stealth fighters have (this has not changed at all with the new prototypes with the new engine cowling either) so from a stealth shaping perspective the t-50 is more analogous to a clean rafale or
Another thing you’ll notice on the actual VLO aircraft is sharpened (blade-like) leading edges and meticulous attention to reducing surface discontinuity reflections, neither of which have been addressed in the latest PAK fa examples.
Are you just eye balling the jets and coming up with the angles ? Nobody knows what the angles look like on the computer or on the test platform. We dont have the RCS’s of both jets to compare. What we do know is that they are taking their time to build a stealth 5th gen jet. We can be arm chair RCS testers all day but we really have no idea.
The surface angles of the yf-23’s side surfaces were significantly more canted than the f-22’s.
The angle of the f-22’s side surfaces are 55 degrees from horizontal, the yf-23 was around 35 degrees. This accounts for the difference in allround RCS.
The PAK fa has some surfaces canted at 65 degrees like the f-35 and j-20, however it also has surfaces at 75 and 85 degrees like non-stealth fighters have (this has not changed at all with the new prototypes with the new engine cowling either) so from a stealth shaping perspective the t-50 is more analogous to a clean rafale. Both have frontal RCS reduction measures with some side RCS reduction. Neither have any rear RCS reduction.
Another thing you’ll notice on the actual VLO aircraft is sharpened (blade-like) leading edges and meticulous attention to reducing surface discontinuity reflections, neither of which have been addressed in the latest PAK fa examples.
will reply in Pak Fa thread
FSB said
No it doesn’t, look on underside of Pak-Fa inlet. If u want to respond, move it over to appropriate thread.
Its 2 totally different designs. The Pak Fa is basically an under engine design with each engine separated with levcons on top. The air is free to go around each engine. The F 22 has a blended fuselage/intake design. And in that design, there is more potential for dead air where the intake separates from the fuselage.
It seems that “Falcon 21” was a family of GD´s designs, something like “Falcon 21” being the simplest (big wing plus an upgrade of avionics and engine) and the “Falcon 21++” (new wing, new airframe, F-119, etc) being the most advanced.
Bit more information here:
https://www.flightglobal.com/pdfarchive/view/1991/1991%20-%203220.html
Interesting stuff.
He’s talking about the boundary layer spill ducts. Look on top of the F-22 near intake.
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Looks like a mess compared to the Pak Fa. Any air that doesn’t go through the engine on the Pak Fa, has a straight path right out to the back of the jet.
Is it so outside the boble to say the F-22 has a better detailed signal management?
Hell just take another example, those air spill doors from airduct on top of F-22 and then look at the ones on bottom of PakFa(Flanker) air-intakes.I’m sorry if it upsets people. It is what it is.
I like the PakFa over F-22 Design for several reasons, stealth finesse is not one of them.I would say the F-22 is more boxy vs F-35 considering the F-35 has only one(huge) engine. And every airframe design is build around its engine/engines.
Is it so outside the boble to say the F-22 has a better detailed signal management?
That’s not the argument. There is a tactical costs to having this detail. Im sorry to say, that you have to explain how this tactical cost outweighs the advantages that the Pak Fa has.
Hell just take another example, those air spill doors from airduct on top of F-22 and then look at the ones on bottom of PakFa(Flanker) air-intakes.
Any pics ? I have no idea what this is about
Sigh..
Let me try again. Being slim as the YF-23 and PakFa does not mean it has a lower RCS vs F-22.
It only means it has a slimmer side profile, but LARGER top/under Profil.
It a design choice.
From ground or above the PakFa has a larger fotprint.
Oh and the same when PakFA turns over from a peer point of view.Yes i’m sure Sukhoi want to cut some corners on cost, but that does not take away anything from the F-22 Design.
It may be the most expensive fighter, but its a very advanced product. I’d say that matter.If the PakFa design advocates any advantage, i’d say it utilizing its internal volume a tad better vs F-22 more boxy airframe with the air-intakes inside vs under the airframe.
PakFa also produce more lift from the blended wing/body layout.
Let me try again. Being slim as the YF-23 and PakFa does not mean it has a lower RCS vs F-22.
It only means it has a slimmer side profile, but LARGER top/under Profil.
It a design choice.
You are implying that the ratio’s are the exact same and that the Raptor is taller in the exact number that the Pak Fa has a bigger top down profile. And then you are implying that the top down footprint is more important than the incoming profile. The YF 23 is shaped more like the Pak Fa and it got better all around stealth than the Raptor.
Yes i’m sure Sukhoi want to cut some corners on cost, but that does not take away anything from the F-22 Design.
OMG… I said OPPORTUNITY COST. Not production cost. Meaning, they deemed the advantages of the slimmed down option did not outweigh the advantages of the protrusions.
It may be the most expensive fighter, but its a very advanced product. I’d say that matter.
Again. I was talking about opportunity cost. Which has exactly nothing to do with the value cost of the jet.
Well being slim doesn’t really make it Stealthy on it self.
The details on F-22 is still the best out there. Not a singel protruding probe or antenna.Perhaps redone nozzles.. Still waiting on PakFa on that department..
Btw, where does PakFa discard all the Shells from its gun?
To say that size doesn’t matter is just so fundamentally ironic and ignorant. How could size not matter ? And unlike everything else you mentioned, you can’t change size.
The details on F-22 is still the best out there. Not a singel protruding probe or antenna.
And you think that this is some scientific breakthrough ? Its not. Obviously the Pak Fa engineers believe that the opportunity cost for having no protrusions does not outweigh the benefits of the protrusions. But you are one of those stealth absolutists. How did stealth absolutism work in Serbia ?
Perhaps redone nozzles.. Still waiting on PakFa on that department..
You mean the flat nozzles ? Where are they in the F 35 ? But its just another opportunity cost calculation. Or are you talking about the saw tooth edges ? ooh tough.
Btw, where does PakFa discard all the Shells from its gun?
More stealth absolutism.
The Raptor has to change the big ugly horizontal stabilizers, the big boxy intakes and the general size of the airframe to get anywhere near the Pak Fa. The Pak Fa could get an inch of RAM painted over the whole thing and it would still be lower profile than the Raptor.
The only thing that comes close to the short stabilizers, moduled engines and general low profile is the YF 23
looking at the rather conventional approach to stealth in T-50 it may seem that during 80’/90′ they simply underestimated its importance.
Honestly what the hell is that supposed to mean ? What is conventional about the T 50 ? The T 50 is the lowest profile jet. It looks the most like 6th gen concepts as anything with the smallest horizontal stabilizers. Sure smaller than the Raptor. The only other super low profile 6th gen looking comparable is the YF 23.

It is sad that the 1.42 did not reach operational status as I would think that it would have been stealthier than the current Sukhoi PAK-FA looking at both designs.
?? Just the opposite.
It is a bulky configuration. Intakes, canards ect.
Out of all the 5th gen designs, nothing comes close to the slim profile of the Pak Fa except maybe the YF 23.
U.S. Air Force Official: F-35 Could Beat Russia’s Stealth PAK-FA or China’s J-31 in a Fight
That’s a low information article made to read by the general public. Not hardcore enthusiasts
To quote Andraxxuss
http://forum.keypublishing.com/showthread.php?135460-test-pilot-quot-F-35-can-t-dogfight-quot/page34
It makes me wonder why they didn’t just take the F 16 and do what it took to stealth it, internalize fuel and weapons and put the fancy computers in it.
@KGB, how would you choose which 2 roles and how would you justify the extra $30-40 Billion in dev combined with the higher cost to produce?
I mean they should improvise. Like keep using the A10 instead of retiring it.
Maximum speed of the Su-47 is less than M = 2, since the air intakes are not regulated 😉
ЛЛ-УВ(ПС) – flat nozzle bomber “product 54C.” By the fifth generation fighter is irrelevant.
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what a big ugly awkward looking POS that is. Glad they stayed with the roundies.
Generally it is said the X-32 failed to convince people of its approach to vstol.
What if say, the Navy, Marine, and Air Force decided separately to choose their own variant rather than the “one decision for all” approach that was use.
would the X-35 would’ve still won over the X-32 in all three branches?
The x 32 was just too ugly and unconventional to ever get produced.
Evidently 2 entirely different aircraft should have been produced though. Because the F 35 is a jack of all trades but a master of none.