Turkish Space Programs

[Swezu]

If Rocketsan now officially broadcasts the schematics of his project. It is because it has this element in ToT either with Ukraine or with South Korea (Or both).

So make your video.

Has roketsan released any pic ?

@Bubblegum Crisis

 

[golgelerprensi]

Türk Savunma Sanainin Durduğunu iddia edebilirsiniz...

gerçek ise bu değil.. çok sistematik bir gidişat var..
Bazı projelerdeki aksamaların nedeni sözde müttefik ülkelerin ilan edilmemiş ambargoları ve platfor üretiminde Kritik Alt Bileşenleri üretme isteğidir..

Bizi engellemeye çalışanlar bilmelidir ki YAPACAGIZ...SADECE ZAMAN MESELESİDİR...

 

[SOHEIL]

Another probability !

Similar to KSLV-2 but without third stage !

 

[Muhammed45]

Another probability !

Similar to KSLV-2 but without third stage !

View attachment 416497

@SOHEIL
Is that rocket completely made by S.K?

 

[-------]

>>>

OK ... Probably 6 combustion chambers !

View attachment 416488

But it's much smaller than your estimations !

From what I see it's probably 40m tall and 3-3.3m in diameter !

Brother ... Testing a rocket engine for SLV creates a huge heat signature ! Spy satellites can easily locate the test site !

Here is Iran's engine test center in Semnan deserts :

You can't hide such a thing these days !!!

It's going to be a kerosene lox engine.

 

[SOHEIL]

@SOHEIL
Is that rocket completely made by S.K?

They can't develop a rocket engine in such a low period of time without technology transfer !

It's going to be a kerosene lox engine.

What do you mean by that?

 

[Islamic faith&Secularism]

He is not a mullah and he knows what he is talking about.

But of course ! ^^


Thank you @OguzSenturk

Old link :

https://defence.pk/pdf/threads/turk...dates-discussions.230540/page-45#post-9483263







Lenght (m) : 60.0
Stage 1 engines : 6 x ...


Old Link :

https://defence.pk/pdf/threads/turk...dates-discussions.230540/page-44#post-9476467


Mayak-M1

Lenght (m) : 47.4
Launch mass (t) : 370
Stage 1 engines : 2 × RD-810


Mayak-M2

Lenght (m) : 61.0
Launch mass (t) : 495 / 515
Stage 1 engines : 4 × RD-810


Mayak (rocket family) - Wiki Link –

Official Link


Old link :

https://defence.pk/pdf/threads/turk...dates-discussions.230540/page-43#post-9470263


KSLV-II (한국형발사체)

Lenght (m) : 47.2
Launch mass (t) : 200
Stage 1 engines : 4 x 75톤급

Official Link

...

Some recent news may have already made the picture old with regard to the specific part, which i guess is already shared in this thread as well.

Turkish defence industry does not target any country around but the technology in the world, therefore A comparison between the mullah copy-past situation and tech-based industry of Turkey for gaining some credibiliy/leverage does only mean a trolling/baiting or ignorance, but also wasting some precious time of people like you to inform the ignorant troll.

 

[Seyfullah]

https://twitter.com/x/status/894091165468852224

 

[OguzSenturk]

Thank you @OguzSenturk


Lenght (m) : 60.0
Stage 1 engines : 6 x ...

You forgot to quote this;

It is not possible to exactly know rocket's specs since we dont know the fuel type, we dont even know the scale of this pictures or diameter/lenght of the rocket.

I did not wrote the official info, i even clearly wrote that in my post. Lenght could be 60m, or not, it is just my prediction from the scale, like "if X is this, then 12x is this", and nothing else.

If you don't mention this, people will think that rocket's lenght will be 60m for sure

 

[Bubblegum Crisis]

...

@OguzSenturk

Thank you for these precisions.

Always is it that we do not reinvent the wheel. ^^

According to Turkey's needs, the rocket must at least be able of putting a 1.5 ton multipurpose satellite into low orbit at 600~800km altitude (Göktürk-1 : 1 ton).

To achieve later up to 5 tons, with a larger rocket, according to new capabilities acquired for satellite production.

In all cases, it should not exceed about 60 m.

But it can be fun to measure it approximately with the length of Göktürk-1 (4.2 m x 2.5 m x 1.6 m) for scale. ^^






...

 

[Bubblegum Crisis]

Has roketsan released any pic ?

@Bubblegum Crisis

Just No ! Still Classified Secret certainly, you do not think ?

 

[-------]

They can't develop a rocket engine in such a low period of time without technology transfer !



What do you mean by that?

What do I mean by what, the engine will be LOX Kerosine.

And pictures are a retort to your images on how rocket engines can be tested, without a need of large structures.

SpaceX Raptor Engine

 

[OguzSenturk]

SpaceX Raptor Engine

Raptor Engine is LOX Liquid Methane engine, not kerosine
https://www.wikiwand.com/en/Raptor_(rocket_engine_family)
https://space.stackexchange.com/que...hane-as-fuel-for-their-next-engine-the-raptor

" The engine will be powered by densified liquid methane and liquid oxygen (LOX), rather than the RP-1 kerosene and LOX used in all previous Falcon 9 rockets which use Merlin 1C & D engines. "

 

[-------]

Raptor Engine is LOX Liquid Methane engine, not kerosine
https://www.wikiwand.com/en/Raptor_(rocket_engine_family)
https://space.stackexchange.com/que...hane-as-fuel-for-their-next-engine-the-raptor

" The engine will be powered by densified liquid methane and liquid oxygen (LOX), rather than the RP-1 kerosene and LOX used in all previous Falcon 9 rockets which use Merlin 1C & D engines. "

I should be more clearer on how I post things huh? I was giving @SOHEIL an example of how engines can be tested without the massive investment in infrastructure.

 

[OguzSenturk]

I should be more clearer on how I post things huh? I was giving @SOHEIL an example of how engines can be tested without the massive investment in infrastructure.

Sorry, Soheil was in my ignore list so i though you were giving that video as an example of kerosene engine