Can Volvo RM-12 Jet Engine Replace Thunder's RD-93 ?`

[F86 Saber]

ummmm i think the key word here is "Future"........

 

[Kompromat]

ummmm i think the key word here is "Future"........

Yes Block II/III

 

[wangrong]

another Project WS-12 "tian shan"

 

[bc040400065]

Who sold us the SAAB AWACS ?

yes i know it is sweden but my post was that sweden has banned any "future" weapons systems sales to pakistan.. it was here on this forum just few weeks ago.. but may be i m wrong.

 

[Kompromat]

Any specs wangrong ?

 

[wangrong]

notice this pic

 

[wangrong]

Any specs wangrong ?

JF-17 can use WS-12

 

[Kompromat]

JF-17 can use WS-12

So this was the Unnamed TVC Engine i was talking about , cool.

Do you know about the amount of thurst it can produce and what is the development status ?

 

[TaimiKhan]

So this was the Unnamed TVC Engine i was talking about , cool.

Do you know about the amount of thurst it can produce and what is the development status ?

9500kgf equal to something like 93kN if rounded.

 

[Kompromat]

9500kgf equal to something like 93kN if rounded.

It will do the job

 

[TaimiKhan]

It will do the job

Well i hope it goes to 100kN or more, as that will do the job perfectly.

 

[Aslan]

What are the differences between turbo fan and turbo shaft and turbo jet engines.

 

[TaimiKhan]

What are the differences between turbo fan and turbo shaft and turbo jet engines.

Turbojet - Wikipedia, the free encyclopedia

Turbofan - Wikipedia, the free encyclopedia

Turbo Jet Engine layout


Turbo Fan Jet Engine layout

 

[Aslan]

@ TaimiKhan


Thank you for the links khan sahib, I was actually reading the same ones right now. What I understood from it is that the Turbofan engines are more durable are high and low speed, give you more speed with the burners and after burns while cruising. And are less noisy then the jet engines. And also by looking at the pics I can safely assume that they are less complicated then the Jet engines as well.

 

[hataf]

notice this pic

weight of engine ????
thrust to weight ratio of engine????
bypass ratio of engine????

please