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We have to take into account what many forget and that is the ungodly amount of workload on TAI. Hürjet in its earlier flights had a problem with flutter it seemed, like when it retracted the landing gear and it had a visible gain of altitude which might mean the flight controls were not compensating for the change in center of gravity sufficiently, maybe (?). This seems negligible in this flight now, but obviously there will be problems and this is the first time they're testing and gathering data in this regard, and the point is that this not the only thing they're doing, not even close. They are just doing so many things at the same time that I'm amazed they haven't been overwhelmed into a blunder of some sorts. So hats off to them.Guys, sorry for not being "patriotic" enough but WTH is going on with Hürjet tests? Not to mention ANKA3...
When will we find out top altitude and speed of Hürjet? Why is it still flying subsonic like it's being piloted by an elderly?
It should be able to fly at Mach 2.1 using F404 engine. If it can't it is because engineers in TUSAS shat the bed big time and made Hürjet with too much DRAG!!!
Consider how aerodynamic F20 is and compare that with Hürjet.
View attachment 63596 Considering S shaped intakes and massive frontal profile and not to mention HEAVY body this would mean KAAN also will suffer from same bad design practices. Even Mach 1.8 despite 2 F110s seem unlikely to me. I hope I will be proven wrong.
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The F-20A was powered by a single General Electric YF404-GE-100 engine. The F404 is a two-spool, axial-flow, low bypass turbofan with afterburner. It has a 3-stage fan section, 7-stage compressor and 2-stage (1 high- and 1 low-pressure stage) turbine. The the F404-GE-100 is rated at 17,000 pounds of thrust (75.62 kilonewtons) with afterburner. The engine has a maximum diameter of 2 feet, 10.8 inches (0.884 meters), is 13 feet, 2.8 inches (4.034 meters) long, and weighs 2,230 pounds (1,012 kilograms).
From a cold start, the prototype fighter could climb to 34,000 feet (10,363 meters) in 2½ minutes. It could accelerate from 0.3 mach to 0.9 Mach in 27 seconds. The F-20A had a maximum speed of Mach 2.1 at 36,000 feet (10,973 meters)—1,387 miles per hour (2,232 kilometers per hour). Its service ceiling was 55,000 feet (16,764 meters). The maximum range with external tanks was 1,715 miles (2,760 kilometers)."
IMO, this part of claim is very important.To that effect they are envisaging the second seat pilot to be used as weapons controller of drones.
I'm still not sure a naval Hürjet makes much sense, it feels like it would be an easy target not being a stealth jet and it's payload is too light but then again if Çakır can indeed be used against ships it might be more than enough.
Interesting video where the Tusas chief engineer informs us that when Hurjet first flew they were also gladly surprised that the plane did not red flag any faults. Even the accompanying F16 pilot commented and questioned if this was truly the first flight of this plane. This is expediting the plane being ready for serial production. They are planning to start delivering 12 planes per year in 2027-28 timeline.
He also mentions that for the last 5 years, they have been working on the specifics of this plane being a light attack aircraft. To that effect they are envisaging the second seat pilot to be used as weapons controller of drones.
Also they have tried on simulators, the ski lift take off possibility; and the plane can take off from a ski lift like the one on TCG Anadolu with 4-5000lb ammo load. Of course they need to improve landing gear and include hook to the plane and arresting mechanisms to the craft it is landing. (I would add that it would also need to be navalised)
I cannot agree with this. Unlike many conventional AJTs, the Hurjet is a platform with a high angle of attack and agile maneuvering capabilities. The +8/-3 g limitation is mostly used to define this class, but I believe that what is written on paper will not remain definite limits, considering that additional variant studies on this project have been going on since the very beginning. In other words, the technical specs will never be available in open sources until this jet is awarded an tender outside, but an ROT value that can compete with most of the 4th generation jets is certainly not an extraordinary expectation in near future.I'm still not sure a naval Hürjet makes much sense, it feels like it would be an easy target not being a stealth jet and it's payload is too light but then again if Çakır can indeed be used against ships it might be more than enough.
I think you are right about this, we could learn a lot from a project to make a naval Hürjet, before we, imo, inevitably make a naval version of Kaan. Navalization of our aircraft and helicopters is one of the obstacles we have to overcome sooner or later.Despite all the negative things, I believe that a Hurjet Naval would be an extraordinary step in the development of our defense industry and the development of our naval aviation. Even if it cannot go beyond just a Naval trainer aircraft, it will be a great industrial and military step forward.
I agree with this as well, I would rather have a light fighter Hürjet that we make ourselves (barring engines unfortunately) than something like JF-17.In addition to all this, there is also the case of the Air Force. Frankly, for the worst case scenario, I would rather have a fighter Hurjet with STOL capability than a JF-17.
About half of our projects right now remind me of Altay since whether they are aerial, naval or land projects, we seem to lack engines for half of them. I think Altay has caused a lot of ptsd in Turkish defence industry enthusiastsIt sounds familiar, reminding you of the Altay case, right? LOL
When TurAF forms a squadron, demonstrate and prove the aircraft to be a reliable platform as a workhorse from vanilla trainer version to light attack and many other roles for the needs of potential customers with the permission of the US of any export of American hardware on board, particularly F404.When will Hurjet actually fight FA-50 in the international market?
This doesn't make sense. Either it's 1.6 mach or did the jet actively slow itself with control surfaces while afterburner is on? It should usually reach 1.4 mach with that power. Or is it 0.6 mach on ground?HÜRJET reached Mach 0.6 HÜRJET Jet Training Aircraft made its 27th flight. The design phase of HÜRJET has ended.
Jet Training Aircraft HÜRJET took to the skies for the 27th time in October. In this flight, where the aircraft took off for the 27th time, having remained in the air for a total of 18 hours as of October 11, 2023, the calibration of the air data system and model verifications were carried out.
To carry out the high-speed tests, the aircraft's landing gear was assembled and the engine power was increased to Max A/B level.
As the engine power reached Max A/B, the propulsion system used in the aircraft produced 50 percent more thrust force, enabling the aircraft to accelerate to 0.6 times the speed of sound.
The speed envelope of HÜRJET, which will reach speeds above the speed of sound, continues to open. In the future, supersonic tests will be carried out with other HÜRJET prototypes.
No typos there unless TAI made one, it comes straight from their own magazine:This doesn't make sense. Either it's 1.6 mach or did the jet actively slow itself with control surfaces while afterburner is on? It should usually reach 1.4 mach with that power. Or is it 0.6 mach on ground?
Any news on when we can expect to see the 2nd prototype?HÜRJET reached Mach 0.6 HÜRJET Jet Training Aircraft made its 27th flight. The design phase of HÜRJET has ended.
Jet Training Aircraft HÜRJET took to the skies for the 27th time in October. In this flight, where the aircraft took off for the 27th time, having remained in the air for a total of 18 hours as of October 11, 2023, the calibration of the air data system and model verifications were carried out.
To carry out the high-speed tests, the aircraft's landing gear was assembled and the engine power was increased to Max A/B level.
As the engine power reached Max A/B, the propulsion system used in the aircraft produced 50 percent more thrust force, enabling the aircraft to accelerate to 0.6 times the speed of sound.
The speed envelope of HÜRJET, which will reach speeds above the speed of sound, continues to open. In the future, supersonic tests will be carried out with other HÜRJET prototypes.
I guess it must be some testing procedure where they test full afterburner without breaks to stop exceeding certain speed limit then, no idea.No typos there unless TAI made one, it comes straight from their own magazine: