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There's a video on this twitter post;
View: https://x.com/clashreport/status/2022327801475367055?s=20
View: https://x.com/clashreport/status/2022327801475367055?s=20
That was the GTU-0/P0 Tech Demo/Ground Test Article, whereas the newer ones are designated as P1 & P2(?); though one of them in the photo is said to be for the Iron Bird tests, whereas the P2 is supposed to be one of the flying prototypes.Nothing personal to P1, but P2 is BY FAAAR more attractive.
One of them is the Iron Bird, the other is P1. That must be the reason for the differences.
I vaguely recall that P1, P2, and P3 were being built at the same time, with P3 supposedly designated for Iron Bird tests?I see so, just P0 and P1 plus the Iron Bird for static tests. No P2 present just yet.
(i still hope they'd replace upper irst with something else, for aesthetics only)
come to think of it, it ain't quite as bad as it was on graphics.
That should be the case. Tolga Özbek confused it with P2, but TAI doesn't give Iron Birds "P" designation. I mean, look at Hürjet or Gökbey. The Iron Birds were built before the second prototypes and didn't receive a "P" designation.I see so, just P0 and P1 plus the Iron Bird for static tests. No P2 present just yet.
Indeed.. However this is the static test airframe. Iron bird is a totally different test rig all together, has nothing to do with what is shown here.One of them is the Iron Bird, the other is P1. That must be the reason for the differences.
View: https://x.com/KaraKulak__/status/2022325470054826229?s=20Turkish Aerospace GM:
"The 10 engines we have are sufficient for the prototypes.
We are awaiting engines from the USA, and we are currently in the final stage of the approval process.
We will likely receive approval for the first batch of blocks 10 and 20 this month, or perhaps next month
more internal space?Guys.. The main landing gears are now side-mounted.
Static Prototype (left)
View attachment 801906
VS
GTU-0/P0
View attachment 801907
This would also require a fairly substantial internal redesign...
The gears are the same. But yeah, when I first noticed it, I was like, “How the heck did we miss this detail?”View attachment 801908
@snne Good catch. Lol, such an obvious change, but we didn't notice it. The gears are also much beefier. Also, no more double chin.
Initial tests only, not the full engine assembly.Fascinating development. Really.
Does the start date for the TF35000 prototype tests remain this year?
Is there a higher-resolution image available? Devil's in the details and the new prototype is so detail-rich that such low-resolution comparisons do not do justice to how much more advanced it is...Quick comparisonView attachment 802039
Is there a higher-resolution image available? Devil's in the details and the new prototype is so detail-rich that such low-resolution comparisons do not do justice to how much more advanced it is...
To make room for the side radars.They moved the EOTS forward.
Aerodynamic optimization to increase body lift. Kaan P1 looks like it will generate more lift from the body vs P0. Approaches Su-57 level body lift. Much better than the Raptor.View attachment 802064
Why is this surface not curved? could this be a preparation for some sort of flat nozzle?
Looks that way, but the canopy and the rest of the cockpit section are the same; it's just the camera perspective making the dimensions appear different.Is it just an appearance, or is the canopy really higher?
Indeed, the wings are small compared to other 4th/5th gen heavy-lifters (even with its 3 pylon slots). In a non-stealth A-G configuration, I’d imagine cruise missiles would take up a significant portion of the available underwing real estate, given how short the span is from the wing root to the tip.Aerodynamic optimization to increase body lift. Kaan P1 looks like it will generate more lift from the body vs P0. Approaches Su-57 level body lift. Much better than the Raptor.
CEO of TAI had an interview a couple days ago:Initial tests only, not the full engine assembly.
It’s currently in CDR. They’re following a strategy similar to the Kaan fuselage development approach, i.e. producing and testing components while the Critical Design Review phase is still ongoing. Single engine integration on a prototype in 2028 still seems possible, albeit on a somewhat tight timeline.
Now, Kaan's engine, as you know, is being developed in collaboration with TEI and TR Motor. Yes. The PDR phase was completed last week. We moved on to the CDR. This was an important phase. In other words, the design has emerged. What will it be like? What will be there? What will be placed where? What interfaces will affect the interior design of the aircraft, its weight, power, etc. These are now frozen as a concept. One of them has been chosen, and this is the stage where the final design details are started. This takes approximately 1 to 1.5 years. In the meantime, sometimes risks are taken, and parts and systems that will take a long time to procure are worked on beforehand, and quickly, I think, we plan to start the first prototype tests in the 2028-29 range. So we will put it on the aircraft in the 2029-30 range. It's progressing fast right now, but we need to speed up even more.
we plan to start the first prototype tests in the 2028-29 range. So we will put it on the aircraft in the 2029-30 range.
2032 is the official certification deadline, as it is written into an actual contract to deliver B30 aircraft with TF35k engines starting in 2032.TF6000 first firing was in 2024 and its first flight is in 2028 earliest(from TAI CEO).
The 2029-30 for aircraft integration of TF35k is just integration, not first flight. The FF of the engine is expected in 2032.
2032 for the first delivery of the engine is no longer true. It's been pushed back by a year. The new target is 2033.2032 is the official certification deadline, as it is written into an actual contract to deliver B30 aircraft with TF35k engines starting in 2032.
He is saying that integration will occur in the 2029 to 2030 timeframe. That does not mean flight testing will begin immediately, as several months of ground testing on aircraft will be required first. A +/- two year test campaign leading up to certification and LRIP commencement in Q2-Q3 2032 would be a reasonable timeline if there's to be no major delays. (Albeit some things would get rushed, such as ground testing)
All engines mature as they enter operational service, with reliability improving over time throughout their service life. Neither the F110, F119, nor F135 were as reliable or as refined at entry into service as they are today.
and we are currently in the final stage of the approval process.
We will likely receive approval for the first batch of blocks 10 and 20 this month, or perhaps next month
The PDR phase was completed last week. We moved on to the CDR.
This takes approximately 1 to 1.5 years. In the meantime, sometimes risks are taken, and parts and systems that will take a long time to procure are worked on beforehand, and quickly, I think, we plan to start the first prototype tests in the 2028-29 range. So we will put it on the aircraft in the 2029-30 range. It's progressing fast right now, but we need to speed up even more.
“It’s a challenging project. It’s a very high-end engine in terms of design, in terms of material, in terms of manufacturing, and our goal is [by] 2032 for first test, and the 2033 is the final delivery,” he concluded.
He wildly throws dates around all the time. This fact makes them just his (more realistic) personal estimates with risks factored in, nothing more. Show me a contract and I'll believe ya.why the laugh? is it the authenticity of the source? It's coming directly from breakingdefense.
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Turkish Aerospace in 'final stages' of talks over Saudis in KAAN fighter program: Exec - Breaking Defense
Riyadh has been tightlipped about how it plans to expand or upgrade its fighter fleet, with several international options on the table.breakingdefense.com