Sukhoi Su-57 / T-50 / PAK FA - flight testing and development Part II [2012-current]

But you see this?
I see. And i read it as PASSIVe and active. And again, KNIRTI is not a developer of radars for PAK FA, NIIP is.

i was wrong either way because Igor stated the functions of a fundamentally new radar for the pafka, not the existing EW system. You know the front, sides and behind view quote? I dont even care anymore it gets other users here worked on what the su-57 has or will not have. The Voltaire quote,"I disapprove of what you say,but I will defend your right to the death to say it." Doesnt apply here. I will drop the subject.
 
View: https://twitter.com/i/status/1390535336539852802


 
is it me or do they sound reminiscent of dive bombers like the Stutka
 
At what point does the Radar Blockers being the cause of the noise become common knowledge? It's been known they make that noise now for a while.

It's truly both amusing and infuriating how uninformed people truly are about the Felon.
 
At what point does the Radar Blockers being the cause of the noise become common knowledge? It's been known they make that noise now for a while.

It's truly both amusing and infuriating how uninformed people truly are about the Felon.

At least it got people to click hahahaha.
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Anyway, something for fun. So yeah I did a little bit of experiment. I made myself a model of an inlet. With a simple Radar blocker and a compressor face with its respective Guide vanes.

Inlet and blockers.png

The radar blocker is just loosely based on the one in Su-57 patent. treatments that i did was to the leading edge of the Blocker where it would have ogival shaped edge to reduce contribution of RCS from the edge. The RAM Is the one from the "Radar Cross Section 2nd Edition" the Magnetic RAM Sintered-Zinc-Nickel-Ferrite.
The inlet Body is not treated and left as PEC, so does the engine face. The solution being used is SBR+ Which allows cavity RCS to be computed

The frequency being used here is L-band (1 GHz) because it's fast and can still enter the duct. Polarization is horizontal, and 3 conditions were taken as follows and the result in 2D contour projection :

No Radar BlockerBoth radar blocker and engine face are made out of
PEC (Perfect Electric Conductor)
Blocker is treated with Radar absorber
No Blocker.png Inlet and blockers.png Inlet and blockers.png
NoBlocker.png Inlet-blocker both PEC.png With Blocker.png
Remarks :
Relatively strong and broad reflections from the blades and guide vanes.
Remarks :
Blocker and Inlet are basically compounding each other, produces strong reflections at the middle of the engine face.​
Remarks :
The radar blocker appears to be able to suppress the reflection of the blades behind it, "flare spots" appears to be reduced.

The above projection are views from the front of the engine. Basically from this :

Face1-With Blocker.png

Numerical wise this is the Median of the inlet's RCS :
Blocker3 coloumns.png

There is about 5-6 dB or 3-4 times of RCS reduction from above model. Doesnt sound like alot but still reduction. Plus i have no idea on how actually a radar blocker is designed. I wonder what kind of reduction a purposely designed and optimized radar blocker can have.

The subject of the design of radar blocker however appears to be rare in open literature so far. There are patents, but research papers are somewhat nonexistent. There are instead many on S-duct. Even the idea of ogival leading edge treatment for my simple radar blocker there came from paper dealing with S-duct (Attached):
 

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Sweet is that a test result from a anechoic chamber or another guestimate like the south Korean 5th gen thread?
 
Sweet is that a test result from a anechoic chamber or another guestimate like the south Korean 5th gen thread?
Obviously Guesstimate with ANSYS.

note that the inlet, blockers are just loosely based. Not gonna claim that would be the real signature. As i said above i have no idea how the blocker was actually designed.
 
Obviously Guesstimate with ANSYS.

note that the inlet, blockers are just loosely based. Not gonna claim that would be the real signature. As i said above i have no idea how the blocker was actually designed.

main-qimg-85d7e99aaa000ff779069c4f010c2dc9.jpg
main-qimg-17167430ee43c9cdc8bc609e57fdeea3.jpg
Got source from LMFS https://findpatent.ru/img_show/12839574.html

  • There were partial S-ducts demonstrated on the patent itself. Meaning the fan blades are not completely exposed but partially.
  • RAM is applied in the inlet.
  • Patent and image shows radar blockers to reflect radio waves away from radar source and covering fan blades
  • There is an anti-radar grading installed inside the air channel.
  • Fan blades are made of composite materials
  • Image of inlet vanes along with patent which are behind the blades are seen as being designed a particular way to lower RCS on bottom image.
If you saw this patent before or not I don't know, just wondering if the above statements were taken into account of the model you made of the inlet? (I no you cant take in account the absorption properties of their RAM)
 
Sounds a bit like a howling F-104. Also, distinctive sounds make any weapon more badass!
 
Obviously Guesstimate with ANSYS.

note that the inlet, blockers are just loosely based. Not gonna claim that would be the real signature. As i said above i have no idea how the blocker was actually designed.




If you saw this patent before or not I don't know, just wondering if the above statements were taken into account of the model you made of the inlet? (I no you cant take in account the absorption properties of their RAM)

Well you should be able to see what i took into account in my post.


The only thing demonstrated from my observation above are that the blocker works. But it also opens up many question like how to optimize the shape. basically things you dont get from just the patent images. Or like why it shaped the way it is.
 
Anyway, something for fun. So yeah I did a little bit of experiment. I made myself a model of an inlet. With a simple Radar blocker and a compressor face with its respective Guide vanes.

Interesting! Some suggestions if I may:

1) Your inlet shape seems to be square with right angles in frontal projection, this is not accurate. The real inlet is a rhomboid which will probably affect the location of spikes.

2) Your blocker & engine face appear to be too close to the intake opening, which will probably impact things as well (especially in connection with #3).

3) It would be nice to see what coating the interior walls of the intake duct ahead of the blocker with RAM changes.
 
doesn't the Super Hornet also use a similar blocker? and if so does it make a similar sound to the 57?
Only problem with other aircrafts carrying blockers (besides the Su-57) I cant find patents for or what physical features they carry in shape if they compare to the su-57.
 
Saw this on another forum. It's from the parade that happened recently. It's obviously CG and it could just be added by the company mistakenly or even maybe some intentional disinformation. Still interesting it was even added. Horizontal louvres in the intake. What do you guys think?
 

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@TMA1 : Good screenshot.
I think you are right: they are probably trying to offer a quick answer to those trying to understand from where the witheling noise comes from (I can't see how such error would have been left unnoticed by Mil officials).
Honestly, it's a good explanation since those kind of louvres will certainly produce such witheling noise in the airstream.

But then, according to our knowledge so far, they are not part of the real Su-57.
 
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The Russians won't be the first to build a hypersonic plane. This requires enormous expenses not only for the creation of such an aircraft, but even more for its operation.
Let the Americans, if they can, or the Chinese, first step into this "puddle"
 
I am a little confused here, so this question is more like a survey. The F-35, NGAD and Russia's 6th gen I am assuming are heading for a 3 stream cycle engine design, correct? Is the FCAS really going for SABRE and Tempest going for reaction engines for near hypersonic speeds or will they just settle down for a 3 stream cycle engine design? I see more promise with a 6th gen interceptor Mig-41 getting detonation engines https://tass.ru/ekonomika/11103513 https://www.militarynews.ru/story.asp?lang=RU&nid=516338&rid= for a near hypersonic design than I do of the other two in my own opinion.

No more dreaming about pulse-detonation technology for PAK DP.
1. Wont change the fact that lyulka developed the detonation engine. 2. The co-development 6th gen project that mikoyan and sukhoi are developing is separate to the 6th gen project mikoyan is developing for a interceptor.

@GARGEAN

darn that sucks https://www.defensenews.com/global/...cialist-reaction-engines-with-new-investment/
 
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MOSCOW, May 30. /TASS/. The defense-industrial complex is preparing for a new stage of modernization of the Russian fifth-generation Su-57 fighter. This was stated by the Minister of Industry and Trade denis Manturov on the air of the TV channel "Russia-1" in an interview for the program "Moscow. kremlin. Putin."

"The Su-57 has just entered service, only supplied, and we are already thinking and preparing for a new stage of modernization. This is an ongoing process," Manturov said, answering questions from journalist Pavel Sarubin.
 
Its like the F-35 Block upgrade path. Expecting it be sensors and software driven.

Edit: About new engines, i think they will get installed as soon as they are ready, it doesn't really hinge on any block upgrade here.
 
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I assume Manturov refers to the Megapolis project to change the engines, actuators and cockpit, probably they will integrate also new weapons that have been in development for a while.
 
I assume Manturov refers to the Megapolis project to change the engines, actuators and cockpit, probably they will integrate also new weapons that have been in development for a while.
are you referring to Izdeliye 30? or are they planning another engine further down the line?
 

The KLA previously reported that the "Okhotnik" will hit air and ground targets as part of the network-centric interaction with the fighter

MOSCOW, June 1. / TASS /. The pilot of the fifth generation Su-57 fighter will simultaneously coordinate the actions of four newest Hunter heavy attack unmanned aerial vehicles (UAVs). This was reported to TASS by a source in the aircraft industry.

"Now the possibilities of controlling several attack drones from the cockpit of the Su-57 are being worked out. It is assumed that the fighter will carry from two to four Hunters with it," he said.
 
When talking about the future of the Russian Navy he mentioned an aircraft based on Su-57:

- You said about a promising deck fighter. If it's not a Mig-29K or a Su-33, what?
- That's what aviation specialists should tell us. The Su-57 can be taken as a base, but the designers will have to count everything as the base of the aircraft on the ship. First of all, it is a folding wing, elements related to brake devices, because a conventional aircraft will not be able to perceive the dynamic loads associated with the hook when landing behind the hook.


 
First of all, it is a folding wing, elements related to brake devices, because a conventional aircraft will not be able to perceive the dynamic loads associated with the hook when landing behind the hook.
Does he mean it will be a Variable-Geometry design?
 
I've recently received Piotr Butowski's Su-57 book, and there are some rather interesting pieces of program history that I wasn't aware of. In no particular order I'll list a few of them off below, although it's by no means exhaustive.

During the now-defunct Indo-Russian FGFA saga, it seemed like the Indians from the beginning preferred the smaller Mikoyan E-721 design over the Sukhoi T-50; when the partnership was forming in 2005, Sukhoi's design was largely finalized, and India would rather pursue a less "mature" design like the E-721 where they can have more input into the design. Whether the FGFA cooperation was doomed to failure from the start is unknown, but there was definitely friction from the very beginning between India and Russia.

Unlike previous Sukhoi fighters, integration of mission systems and other onboard systems was performed by Sukhoi itself, rather than the traditional RPKB of Ramenskoye.

It appears that the AL-41F1 (izdeliye 117) is not quite as "interim" as many have believed; while I think there was always a longer term goal of equipping the aircraft with new engines, it appears that the plan has always been for the PAK FA to enter production and serve in combat units with the AL-41F1, and this was decided as far back as 2004. In fact, it appears that Sukhoi's T-50 submission for the PAK FA had the AL-41F1 from the very beginning. This is an interesting contrast with the Su-27, where the T-10 prototypes used the AL-21, but the revised T-10S and the production aircraft were equipped with the AL-31 from the beginning.

Apparently, weapon firing from internal bays didn't occur until March 2016.

The Su-57 has certainly suffered from weight creep compared to what was originally planned. I recalled the original goal was for an aircraft to be somewhere between the MiG-29 and Su-27 in size, in an effort to rein in cost. Certainly the Su-57 that's in production today is much closer to the Su-27 in terms of size, and especially after the "second stage" structural rework.
 
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Also, Sukhoi's approach to the PAK FA competition at the program level was fundamentally different from Mikoyan's. Mikoyan had planned for a more collaborative consortium-like approach between the design bureaus, while Sukhoi believed that it can win the competition by itself and directly contacted avionics and propulsion suppliers as well as research facilities to create a "complete system" from a program perspective.

Envelope expansion by February 2014 was up to Mach 1.7, 1,000 km/h IAS, 14,000 m ceiling, and 6 g. There was a lull in testing around that time, especially state trials at Akhtubinsk, due to the need for structurally reinforced airframes.

The second phase of state trials, GSI-2, would actually qualify the aircraft as a weapons system, and was supposed to end in 2019, but I’m not sure if that had actually occurred. Entry into service was delayed by the crash of the first production aircraft in December 2019.

Also, the capital U in the title of that book annoys me to no end. It is Su-57 goddamit. It is always Su.

To be fair, the book's title is in all capital letters, so it's merely a stylistic choice.
 
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The Su-57 has certainly suffered from weight creep compared to what was originally planned. I recalled the original goal was for an aircraft to be somewhere between the MiG-29 and Su-27 in size, in an effort to rein in cost. Certainly the Su-57 that's in production today is much closer to the Su-27 in terms of size, and especially after the "second stage" structural rework.

Empty weight wise ?
 
The Su-57 has certainly suffered from weight creep compared to what was originally planned. I recalled the original goal was for an aircraft to be somewhere between the MiG-29 and Su-27 in size, in an effort to rein in cost. Certainly the Su-57 that's in production today is much closer to the Su-27 in terms of size, and especially after the "second stage" structural rework.

Empty weight wise ?
Almost certainly. Originally, the target normal takeoff weight (presumably air-to-air load and a certain percentage of internal fuel) was 22-23 metric tons, whereas now it's 25 metric tons by most accounts. The book also stated that the "second stage" structural rework has also increased weight somewhat.

Incidentally, there was also a chart in the KNAAZ factory showing the distribution of materials in the PAK-FA/Su-57. By mass, the airplane is 40.5-44.5% aluminum alloys, 22-26% composites, 18.6% titanium alloys, 10.7% steel. Composites do make up about 70% of the outer surface.
 
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