Saudi Arabia Becomes Full Partner Nation in the Typhoon Program

[Mosamania]

Saudi Arabia Becomes Full Partner Nation in the Typhoon Program

 

[Yzd Khalifa]

Hellz yeah

It's the bestie news ever I heard of today!

 

[Nishan_101]

Saudi Arabia Becomes Full Partner Nation in the Typhoon Program

MASHA ALLAH, I have been Praying for this since long.
I really though that Saudi Arabia, UAE, Jordan, Oman and Yemen should have join it in the 1990s. And they would have produce it in 3 Trenches.

Also looked in to join some Trainer programs like of Basic, Intermediate and Advance trainer(T-50 Golden Eagle) with EU countries.

Saudi Arbaia: 380-410
UAE: 160+
Oman: 150 (increase the fleet)
Jordan: 150
Yemen: 140+

 

[TopCat]

Who else will be that stupid..

 

[Yzd Khalifa]

Who else will be that stupid..

KSA is pissing everybody off.

 

[T-123456]

With the experience you gain from this,you will be a good asset to the TFX program.

 

[Yzd Khalifa]

With the experience you gain from this,you will be a good asset to the TFX program.

It will be a great idea for us to join you folks in the TFX project.

 

[Kompromat]

@Yzd Khalifa

EJ-200 is on offer with full TOT. It will be a blunder not to get that full tech. As a full partner, RSAF must acquire full TOT for these engines.

 

[Yzd Khalifa]

@Yzd Khalifa

EJ-200 is on offer with full TOT. It will be a blunder not to get that full tech. As a full partner, RSAF must acquire full TOT for these engines.

I believe the RSAF will try to get involve in the EJ-200 ,let just hope it will happen sooner or later.

 

[Kompromat]

@Yzd Khalifa

ej-200 is the same class of engines,we power the JF-17 with.

 

[Argus Panoptes]

@Yzd Khalifa

ej-200 is the same class of engines,we power the JF-17 with.

Eurojet EJ200 - Wikipedia, the free encyclopedia

Specifications

General characteristics

Type: Turbofan
Length: 157 inches (4.0 m)
Diameter: 29 inches (0.737 m)
Dry weight: 2,180 lbs (989 kg)

Components

Compressor: 3-stage LP, 5-stage HP
Combustors: annular
Turbine: 1-stage LP, 1-stage HP

Performance

Maximum thrust: 13,500 lbf (60 kN) dry thrust / 20,000 lbf (89 kN) with reheat
Bypass ratio: 0.4:1
Overall pressure ratio: 26:1
Turbine inlet temperature: 1,800K
Specific fuel consumption: 21–23 g/kNs dry thrust / 47–49 g/kNs with reheat
Thrust-to-weight ratio: 9.175:1 (with reheat)


Comparable engines

General Electric F414
Snecma M88
GTRE GTX-35VS Kaveri
Guizhou WS-13
RD-93

 

[Yzd Khalifa]

@Yzd Khalifa

ej-200 is the same class of engines,we power the JF-17 with.

I didn't know that ,but that's an interesting thing to know. I mean the PAF will definitely could use some experience at this point. The RSAF is in the same track, The MOD has been kicking their a$$ over the last few years so hard!

 

[T-123456]

I believe the RSAF will try to get involve in the EJ-200 ,let just hope it will happen sooner or later.

EJ-200 not enough,lets wait for the new one EJ2x0.
Then get full TOT.

 

[Yzd Khalifa]

EJ-200 not enough,lets wait for the new one EJ2x0.
Then get full TOT.

You think so Sir? Hmm

 

[M.harris]

Congratulation saudi arabia:cheers