JF-17 - Updates, News & Discussion

If JF17 PFX…is a thing…
…my guess would be a future version with WS19 engine rather than RD93(assuming WS19 has demonstrated it’s reliability and is significantly more powerful by that future time).

With the WS19…maybe a slightly larger body of the aircraft to make full use of extra thrust of WS19…along with upgraded avionics(like liquid cooled AESA with more TRMs)
…and perhaps more focus on integrating locally produced munitions.
I'm going to provide you with two images to think about.
1.jpg
2.jpg
This is a screenshot of Chief Designer Huang's speech at the China Aviation Propulsion Technology Forum 2022.
As a side note: the WS19 has been fitted to the J35 and is being scaled up for production.

I doubt the Chinese would want it…so it would go similar route to a JF17…as in PAF acquiring it to replace older aircrafts(which I assume would be F16s at the time).
What makes you think that?

PLAAF has always disliked light fighters, they favor heavy. Among the PLAAF's active fighters, the J10 series is among the lowest configurations, except for a handful of older fighters that are already in the decommissioning process. If it were not for economic factors, the PLAAF would not want the J10.

This factor also affects the J31, which the PLAAF does not like, and which has no advantages over the J20 and is not much cheaper than the J20. Without orders from PLAAF, the J31 has never been able to start production on a large scale. the amount of orders from PAF is obviously not enough to start the production line.

However, I mentioned an idea before. If the JF-17B was upgraded to a 5th generation stealth two-seater version, it would definitely sell. There are no similar products or plans in the world.
 
Any indication the PAF will work on a retractable inflight refueling probe? Something akin to the Tornado’s IFR probe or that on the J-20?

Considering the tech has already been developed for the J-20 and will invariably be put on the J-31/35, putting a similar system on the JF-17 and J-10 will help lower RCS and improve the aerodynamic performance. It’s a technology that would be needed if the PFX is minimize the RCS, so developing it for the JF-17 will help not just future projects but the majority of the current fleet.

If the PAF also wants to develop a UCAV from a fighter this sized and sell it on to PLAAF (as a sub-contractor with Chengdu perhaps) or for export. The demands for atritable UCAVs will likely be large, so Pakistan will have a lot of contracts to bid for.

1727624441640.jpeg
 
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Any indication the PAF will work on a retractable inflight refueling probe? Something akin to the Tornado’s IFR probe or that on the J-20?

Considering the tech has already been developed for the J-20 and will invariably be put on the J-31/35, putting a similar system on the JF-17 and J-10 will help lower RCS and improve the aerodynamic performance. It’s a technology that would be needed if the PFX is minimize the RCS, so developing it for the JF-17 will help not just future projects but the majority of the current fleet.

View attachment 68417
The refueling probe is either externally fixed or internally telescopic, depending on the choice of head design. There are no technical problems.
Any design work is a play on the art of balance. Based on the design specifications, the best choice is made from the arsenal of technical modules already at your disposal.
The JF17 fuselage is so small that it is approaching the limits of its internal space usage. It doesn't have enough internal space to accommodate a built-in telescopic refueling probe.

You'd be surprised when you carefully compare the size of the JF-17 and the J20.
 
I'm going to provide you with two images to think about.
View attachment 68211
View attachment 68212
This is a screenshot of Chief Designer Huang's speech at the China Aviation Propulsion Technology Forum 2022.
As a side note: the WS19 has been fitted to the J35 and is being scaled up for production.


What makes you think that?

PLAAF has always disliked light fighters, they favor heavy. Among the PLAAF's active fighters, the J10 series is among the lowest configurations, except for a handful of older fighters that are already in the decommissioning process. If it were not for economic factors, the PLAAF would not want the J10.

This factor also affects the J31, which the PLAAF does not like, and which has no advantages over the J20 and is not much cheaper than the J20. Without orders from PLAAF, the J31 has never been able to start production on a large scale. the amount of orders from PAF is obviously not enough to start the production line.

However, I mentioned an idea before. If the JF-17B was upgraded to a 5th generation stealth two-seater version, it would definitely sell. There are no similar products or plans in the world.
I think u misunderstood what I said.
I said exactly the same thing in my post…that China wouldn’t want a fighter like JF17 for its airforce.
This is bcuz China has a large landmass…and its adversaries are a good distance away that would make it hard to tackle with light fighters.
 
The refueling probe is either externally fixed or internally telescopic, depending on the choice of head design. There are no technical problems.
Any design work is a play on the art of balance. Based on the design specifications, the best choice is made from the arsenal of technical modules already at your disposal.
The JF17 fuselage is so small that it is approaching the limits of its internal space usage. It doesn't have enough internal space to accommodate a built-in telescopic refueling probe.

You'd be surprised when you carefully compare the size of the JF-17 and the J20.
I know the JF-17 is very small compared to the J-20, but perhaps it need not be fully internal, just like the Panavia Tornado’s probe is hosed in an external conformal housing.


1727625580146.jpeg
1727625865852.jpeg

Building the tech for the JF-17’s evolution into the PFX could lead to the creation of just large enough UCAV for fly with the J-20 as loyal wingmen.


1727625783334.jpeg
 
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I know the JF-17 is very small compared to the J-20, but perhaps it need not be fully internal, just like the Panavia Tornado’s probe is hosed in an external conformal housing.


View attachment 68423
View attachment 68425

Building the tech for the JF-17’s evolution into the PFX could lead to the creation of just large enough UCAV for fly with the J-20 as loyal wingmen.


View attachment 68424
The J-10 is slightly larger than the JF-17 and also uses an external fixed refueling probe.
Forcing the JF-17 to have a built-in retractable probe would require a complete nose redesign and, at the same time, would require a realignment of the overall aerodynamic profile layout. The cost would be too great.

The JF-17 is a Sino-Pakistani cooperation program for Pakistan and export markets only.
The J-20's loyal wingman has a wide choice of completed programs. the FH-97, GJ-11, etc., and a few more yet to be disclosed. It has a wealth of options.

I still maintain that the JF-17 should be developed as a fifth generation two-seat stealth fighter in the future. It could be returned to the Chinese market as a trainer. Currently, no country, including China, has developed a similar program. If the program is successful, PLAAF will certainly choose to buy it to replace the JL-10.
Pakistan needs to pre-empt the CAC and offer to cooperate in the program. Once a similar program emerges for subsequent upgrades of the JL-10, there is a possibility that CAC may refuse to cooperate on the program as it creates a competitive conflict relationship.
 
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The J-10 is slightly larger than the JF-17 and also uses an external fixed refueling probe.
Forcing the JF-17 to have a built-in retractable probe would require a complete nose redesign and, at the same time, would require a realignment of the overall aerodynamic profile layout. The cost would be too great.

The JF-17 is a Sino-Pakistani cooperation program for Pakistan and export markets only.
The J-20's loyal wingman has a wide choice of completed programs. the FH-97, GJ-11, etc., and a few more yet to be disclosed. It has a wealth of options.

I still maintain that the JF-17 should be developed as a fifth generation two-seat stealth fighter in the future. It could be returned to the Chinese market as a trainer. Currently, no country, including China, has developed a similar program. If the program is successful, PLAAF will certainly choose to buy it to replace the JL-10.
Pakistan needs to pre-empt the CAC and offer to cooperate in the program. Once a similar program emerges for subsequent upgrades of the JL-10, there is a possibility that CAC may refuse to cooperate on the program as it creates a competitive conflict relationship.
Fair enough. Also good advice on developing the J-17B further first, as a 5th gen trainer. Perhaps a collaboration with chengdu will prevent CAC from seeing it as competition, and a joint way to develop a trainer for the PLAAF and a fighter for the PAF under the PFX program.
 
Fair enough. Also good advice on developing the J-17B further first, as a 5th gen trainer. Perhaps a collaboration with chengdu will prevent CAC from seeing it as competition, and a joint way to develop a trainer for the PLAAF and a fighter for the PAF under the PFX program.
I posted my take on this earlier in another thread.

This is what I consider to be the optimal solution for the JF-17 follow-on development. It could work perfectly with the J31 purchased by PAF to form a complete advanced fighter force. Moreover, it will not create any conflict of interest with China and can be fully supported by China. Pakistan can maximize local manufacturing according to its situation. To build their own chain of fighter jet manufacturing.
 
Any indication the PAF will work on a retractable inflight refueling probe? Something akin to the Tornado’s IFR probe or that on the J-20?

Considering the tech has already been developed for the J-20 and will invariably be put on the J-31/35, putting a similar system on the JF-17 and J-10 will help lower RCS and improve the aerodynamic performance. It’s a technology that would be needed if the PFX is minimize the RCS, so developing it for the JF-17 will help not just future projects but the majority of the current fleet.

If the PAF also wants to develop a UCAV from a fighter this sized and sell it on to PLAAF (as a sub-contractor with Chengdu perhaps) or for export. The demands for atritable UCAVs will likely be large, so Pakistan will have a lot of contracts to bid for.

View attachment 68417

The refueling probe is either externally fixed or internally telescopic, depending on the choice of head design. There are no technical problems.
Any design work is a play on the art of balance. Based on the design specifications, the best choice is made from the arsenal of technical modules already at your disposal.
The JF17 fuselage is so small that it is approaching the limits of its internal space usage. It doesn't have enough internal space to accommodate a built-in telescopic refueling probe.

You'd be surprised when you carefully compare the size of the JF-17 and the J20.


A retractable inflight refueling probe for JF-17?

What benefits it bring compare to cost and efforts required for it? What's the need for a retractable inflight refueling probe for JF-17?
 

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