TR Defence Exports & Updates

Huelague

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I am afraid you are grossly mistaken there.
The difficulty level of building an ICBM is exponentially more difficult than building SRBMs which we have so far been building.
Also it is claimed that Yildirimhan is supposed to be single stage. Currently there are no modern single stage liquid fuelled ICBMs. They are now obsolete as they are dangerous and posess operational difficulties.
Multi stage ICBMs are more complex to build. They need a great deal of specialised engineering know how.

Designing an ICBM is widely considered one of the most difficult engineering challenges, combining advanced propulsion, guidance, materials science, and physics under extreme constraints.
Managing flight characteristics in airless space, then flight for a while to reach apogee followed by re entry in to atmosphere is no easy task.
Guidance accuracy after having travelled 5500+km and releasing decoys in space are not the same as what you encounter with SRBMs.

During reentry the heat management and keeping structural integrity is a problem in its own right.

To reach such long distances, the booster mass may have to be 100 times bigger than the payload. Plus the rocket engines will have to be ultra efficient.
Testing is expensive and difficult due to international pressures.
The whole missile is just very very expensive to develop and manufacture.

What I have understood is, that we build a MRBM with Cenk already.
About the fuel, we have managed liquid fuel, if I am not mistaken.
About the Yildirimhan, it is expected to have a multi stage engine and not single stage.
 

Yasar_TR

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What I have understood is, that we build a MRBM with Cenk already.
About the fuel, we have managed liquid fuel, if I am not mistaken.
About the Yildirimhan, it is expected to have a multi stage engine and not single stage.
It says single stage here:
Nilüfer Kuzulu of MSB-ArGe has only mentioned that it has 4 rocket engines and is a 17.5 m long, 1.5m diameter rocket.
She also says that TSK's repair and maintenance factories had a hand in making it.

But we all know that apart from Delta-V and Roketsan no other entity in Türkiye has the technology to build rockets. Furthest we have managed in exo-atmospheric flight is just over 200 km altitude. Roketsan has been working on 400km altitude for sometime.
Yildirimhan missile is supposed to go above 1500 km altitude.
Cenk missile is a myth. We don't know if it even flew.
There are news that end of 2025 Tayfun Block 4 was flight tested. But no video yet.


EDIT

PS

Contrary to general belief when missile is travelling in upward direction, there is still the effect of gravity on the missile. There is no such thing as zero gravity. There is weightlessness. But not zero gravity.
So the missile has to climb to its apogee overcoming the force of gravity whilst burning fuel all the time.

Re: zero gravity vs weightlessness.

First remember how when a plane starts dropping towards earth with an acceleration of 9.8m/s2, everyone inside becomes weightless.
But the force of gravity is till there. By dropping at that acceleration it is temporarily nullified.

When a rocket is in space and is travelling at a tangential speed of 27600km/hr at 400km altitude (as per ISS), it is Infact dropping towards earth negating gravity and because of it’s speed, it is staying in orbit. Hence weightless situation for the inhabitants of the rocket/ISS.
 
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Huelague

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Nilüfer Kuzulu of MSB-ArGe has only mentioned that it has 4 rocket engines and is a 17.5 m long, 1.5m diameter rocket.
I am confused. Which one is correct? A single stage or a multi (4) stage engine ?

Cenk missile is a myth
Are you serious? You think we don’t have?
But we all know that apart from Delta-V and Roketsan no other entity in Türkiye has the technology to build rockets

Whom belongs the IP rights of these technologies?
 

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