I wish they asked the turbine inlet temperature of TF6000. Maybe a question about cooling techniques or SCB thermal barrier coatings would be nice, too.
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I wish they asked the turbine inlet temperature of TF6000. Maybe a question about cooling techniques or SCB thermal barrier coatings would be nice, too.
Maybe they can ask during this fair. As i understand ,all information is given during latest teknofest.I wish they asked the turbine inlet temperature of TF6000. Maybe a question about cooling techniques or SCB thermal barrier coatings would be nice, too.
Cabatlı, where to access these?
Btw do you think that MMU engine can be ready for 2026 first ignition?
I think it can but wanna hear your perspective
I wonder we will use KTJ 3700 for SOM variants or a new type of ALCM or not.It is aimed to start ground tests with KTJ3700 before the end of 2022 and use the KTJ3700 in the fist firing test of Kara-Atmaca in 2023
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When we calculate 0,8 Mach average speed, It may be over 300 kms if the engine works about 20 minutes (with 60-70kg fuel) when launched from Akıncı/Aksungur.KTJ-1750 consumes roughly 190-200kg of fuel in an hour at full thrust. We can roughly deduce the range of Çakır from this.
BMC Power will sign a diesel engine agreement for SİDA with Sefine shipyard.
Why does Baykar Makine buy Sungur manpads from Roketsan?
There was a signing ceremony today.
But how do we know how much fuel tank can hold ?When we calculate 0,8 Mach average speed, It may be over 300 kms if the engine works about 20 minutes (with 60-70kg fuel) when launched from Akıncı/Aksungur.
We don't know right now and we probably never will. We can only guess. Çakır weighs 275kg and carries a 70kg warhead. The engine can run for 15+ minutes with 50kg of fuel. This means the missile can travel more than 250km(1000km/h) if the missile is loaded with 50kg of fuel.But how do we know how much fuel tank can hold ?
Your estimation probably more or less correct! I think cakır's range will increas step by step like SOM. If I remember correctly it was first announced to be 100 nm and now with som j it's 150nm.We don't know right now and we probably never will. We can only guess. Çakır weighs 275kg and carries a 70kg warhead. The engine can run for 15+ minutes with 50kg of fuel. This means the missile can travel more than 250km(1000km/h) if the missile is loaded with 50kg of fuel.
i honestly expect MMU engine to be similar to F110-GE-132, as TEI already has experience with it.TEI has been closely working with GE on Blisk fan technology for years. The F110GE129EFE engine AKA F110GE132 is an engine that TEI is responsible for maintaining and servicing as well as producing parts for it.
So it is only logical that the Blisk (Bladed Disc) technology is adapted for our TF6000 engine.
GE has been working on Blisk fan since the beginning of 2000s.
This technology improves engine efficiency immensely. Keeping internal temperatures at check and more manageable levels it gives immense power increases to the engine output.
By enlarging the engine diameter to F110 levels (120cm) and adding a few more fan and compressor stages, hence elongating the engine the power levels needed for the MMU will be reached.
From that perspective the F6000 is a vitally important engine to produce.
As TF6000 tests are being done, it is most likely that the indigenous MMU engine will be developed along side it, coming about a year or so from behind, manufactured with experience and expertise attained from TF6000.
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