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Thank you for an educated reply. I'm just passing on the exasperation of US aeronautical engineers when they see a fighter jet made of aluminum alloy. Now, I am not saying go 100% with composites. Particularly when you talk of key structural components of wide bodied airliners. Those are gigantic and highly complex things. We are discussing instead components of a small fighter. Does it make sense to build so much of it from aluminum? It seems for the PAF it does. It seems also that US aeronautical engineers don't share that enthusiasm. Hope I made my point a bit clearer.

You've sort of answered your own concern. The JF-17 has composites in nonstructural places already. Those are relatively easy to design, maintain, replace. Keep in mind it's hard to find anything on an aircraft that isn't load carrying (even the skin carries a lot of load in some places).

There's plenty metal in US designs still. It's not like US engineers are looking at Aluminum with disdain or anything. It's an engineering decision not a high-school popularity contest. If the US DoD can dish out $220 million per plane, then the engineers have the freedom to incorporate all sorts of fancy composite structural members. It would be cost-prohibitive even for the US to go 100% composite. It's what you can afford and what capability it gets you.

It's not about lacking the capability to manufacture, diagnose, and maintain composites. There's plenty of people and tech in Pakistan that can do this correctly I can assure you of that. It's about the cost, both in manufacturing and maintenance.

Also whatever I said about composite aircraft structures was equally (if not more) true for small fighters. Airliners go through predictable cycles during operations. It's easier to account for composite fatigue in that case with decent models. Fighters go through harsh maneuvers that are "non-standard" and that's where you need either complicated models, sensors, or both to guess how your structure has degraded. My point is it isn't as simple as carbon fibre cloth lay up in an oven and you're done.

Searching google scholar for 'composites in aerospace' turns up this gem. It validates some of what you say, but it corroborates that composites are heavily used in modern aircraft:

https://ihsmarkit.com/pdf/Composites-Aerospace-Applications-whitepaper_264558110913046532.pdf
Yes they are. My point was simply an aircraft made with composites is significantly more expensive to design, manufacture, and operate. Just because you can doesn't mean you should. I am sure we will see much more significant use of composites in Azm because that will be an expensive and high-end aircraft. The JF-17 is a budget workhorse. It doesn't make sense for it to have a high percentage of composites. That would've reduced your JF-17 numbers by half and in return you would get maybe 10% more thrust to weight and 10% endurance. Not worth it if you ask me.
 
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Yes but if memory serves me right ... Block-IIs have increased payload capacity w.r.t. Block-I
as per engineer who is/was incharge of sub-assembly manufacturing for JF-17 in PAC wings for JF-17 are manufactured for 25 years of service life, so I don't think they have upgraded wings of 50 blk-I aircrafts which mean 100 wings therefore I believe the previous figures of payload capacity of JF-17 blk-I was representing the restricted figures rather the actual payload carrying capacity.
furthermore Block-II's come with IFR probe or at least the plumbings in place.
only from 16-229 and onward
 
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85l62y4af3n41.jpg



 
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You've sort of answered your own concern. The JF-17 has composites in nonstructural places already. Those are relatively easy to design, maintain, replace. Keep in mind it's hard to find anything on an aircraft that isn't load carrying (even the skin carries a lot of load in some places).

There's plenty metal in US designs still. It's not like US engineers are looking at Aluminum with disdain or anything. It's an engineering decision not a high-school popularity contest. If the US DoD can dish out $220 million per plane, then the engineers have the freedom to incorporate all sorts of fancy composite structural members. It would be cost-prohibitive even for the US to go 100% composite. It's what you can afford and what capability it gets you.

It's not about lacking the capability to manufacture, diagnose, and maintain composites. There's plenty of people and tech in Pakistan that can do this correctly I can assure you of that. It's about the cost, both in manufacturing and maintenance.

Also whatever I said about composite aircraft structures was equally (if not more) true for small fighters. Airliners go through predictable cycles during operations. It's easier to account for composite fatigue in that case with decent models. Fighters go through harsh maneuvers that are "non-standard" and that's where you need either complicated models, sensors, or both to guess how your structure has degraded. My point is it isn't as simple as carbon fibre cloth lay up in an oven and you're done.


Yes they are. My point was simply an aircraft made with composites is significantly more expensive to design, manufacture, and operate. Just because you can doesn't mean you should. I am sure we will see much more significant use of composites in Azm because that will be an expensive and high-end aircraft. The JF-17 is a budget workhorse. It doesn't make sense for it to have a high percentage of composites. That would've reduced your JF-17 numbers by half and in return you would get maybe 10% more thrust to weight and 10% endurance. Not worth it if you ask me.

Actually, the biggest reason not to use composites is because you actually want your aircraft to have some mass. Mass creates inertia, which means a mere gust of wind cannot throw you off course. This becomes even more important for light fighters that already have a low mass. The result of going overboard with composites on a light fighter is something like Tejas. If you see the videos of Tejas firing missiles during IOC, the mere act of firing a missile causes the aircraft to sway. Of course the FBW controls are the main culprit, but the job would be easier if the aircraft had some bulk. Overuse of composites in a light fighter creates an airshow queen.

The other aspect is commercial. The aircraft is being sold to Nigeria and Myanmar. Neither of them have the kind of setup that could monitor and maintain composites if they were to be used in load bearing areas. The aircraft is a workhorse meant for third world countries.

Finally, it doesn't simply use aluminum, but an aerospace grade aluminum alloy. I am not aware what exactly is the composition of this alloy. Other metals are used as and when needed
 
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Actually, the biggest reason not to use composites is because you actually want your aircraft to have some mass. Mass creates inertia, which means a mere gust of wind cannot throw you off course. This becomes even more important for light fighters that already have a low mass.
I am very very sure that that's not true. No fighter is in danger of being too light.
 
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You've sort of answered your own concern. The JF-17 has composites in nonstructural places already. Those are relatively easy to design, maintain, replace. Keep in mind it's hard to find anything on an aircraft that isn't load carrying (even the skin carries a lot of load in some places).

There's plenty metal in US designs still. It's not like US engineers are looking at Aluminum with disdain or anything. It's an engineering decision not a high-school popularity contest. If the US DoD can dish out $220 million per plane, then the engineers have the freedom to incorporate all sorts of fancy composite structural members. It would be cost-prohibitive even for the US to go 100% composite. It's what you can afford and what capability it gets you.

It's not about lacking the capability to manufacture, diagnose, and maintain composites. There's plenty of people and tech in Pakistan that can do this correctly I can assure you of that. It's about the cost, both in manufacturing and maintenance.

Also whatever I said about composite aircraft structures was equally (if not more) true for small fighters. Airliners go through predictable cycles during operations. It's easier to account for composite fatigue in that case with decent models. Fighters go through harsh maneuvers that are "non-standard" and that's where you need either complicated models, sensors, or both to guess how your structure has degraded. My point is it isn't as simple as carbon fibre cloth lay up in an oven and you're done.


Yes they are. My point was simply an aircraft made with composites is significantly more expensive to design, manufacture, and operate. Just because you can doesn't mean you should. I am sure we will see much more significant use of composites in Azm because that will be an expensive and high-end aircraft. The JF-17 is a budget workhorse. It doesn't make sense for it to have a high percentage of composites. That would've reduced your JF-17 numbers by half and in return you would get maybe 10% more thrust to weight and 10% endurance. Not worth it if you ask me.

The internet is a funny place, we really don't know who we are talking to. Otherwise I would have given full weight to your assurances. However, I do think there is a level of phobia when it comes to something new and for the Pak military base, composites may be one such phobia.

To every argument, the unimaginative reply typically is "it will cost too much". And then, bam, they buy something incredibly expensive from abroad. Case in point, the SMG purchase. Later this turned out to be a case of brown envelopes changing hands.

Here is a quote from Burt Rutan on aircraft design:
"If composites had preceded aluminum, we would have never certified aluminum for aircraft, due to its fatigue characteristics and its corrosion issues."
Think you might find it interesting and perhaps detracting from your understanding of the greater scheme of things.

We have a lot of engineers and scientists trained abroad and they come back thinking they know the world. But there is something they don't know. The evolution of those technologies they learned about. When Boeing puts sensor and takes microscopic care to ensure there is no fault in the aircraft, they imagine this is how its done and should be done.

Yet, they never learned the pioneer spirit that is needed that preceded the stage where Six Sigma black belts were needed. Such engineers and scientists can never truly be innovators. Because when you have a nascent industry, you need people who are passionate pioneers, hobbyists. Not "I memorized notes, went abroad and got a degree, now don't try to tell me what I know".

You see, the Wright Flyer wasn't built with Six Sigma. it wasn't stress tested. Neither were the vast majority of the innovations coming out of the West. One does not need to put sensors between composite sandwiches because that is where the bozzo who got his degree from Amreeka is stuck at.

When you have a pioneer mindset, you are willing to make leaps of faith. You are willing to take a risk and "see what happens". That mindset is sorely lacking.

Instead of saying "lets put sensors in the structure" one could have easily said "how does this part generally perform in other similar aircraft". "Can we have a ball-park figure on the MTBF".

If Pak military industrial complex and PAF were such straight thinkers, they would not be needing Chinese assistance at every baby step. Al Khalid would be a proper tank built in numbers and not derided during the Saudi tests. Pak would be able to build a corvette on its own and have some form of SAM systems for all services developed. Drones would not need to be imported left right and center.

So forgive me if your assurances about the competence in the back room is taken with a dose of salt.
 
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Impressive, yet every female is somehow one of the first PAF female fighter pilots.

Soon she'd also end up on transports or helis like the so many before her,not sure why are they even sending them to 18 OCU when no one has actually been posted to a fighter squadron afterwards.
 
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C4iSR: Joint & Common Equipment
Pakistan aiming to procure radomes for its AN/TPS-77 and YLC-18A radar systems
Gabriel Dominguez, London - Jane's Defence Weekly
16 March 2020



The Directorate of Procurement (Air) for the Pakistan Air Force (PAF) has issued invitations for tenders to procure an undisclosed number of radomes for the service's Lockheed Martin AN/TPS-77 and China Electronics Technology Group Corporation (CETC) YLC-18A ground-based air-defence radar systems.

The move, which was announced on 11 March, comes after Pakistan's Ministry of Defence Production (MoDP) revealed in its yearbook for 2017-18, which was released in September 2019, that the PAF had placed an order worth USD24.9 million for five of the Chinese-made YLC-18A radars.

The PAF has invited responses to the radome tender by 1 April. No further details were provided.

ylc18.jpg
 
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I am very very sure that that's not true. No fighter is in danger of being too light.

I can help you become 100% sure.

At a minimum, a fighter needs a human, ammunition, communication, thrust, and maneuvers. The human needs life support systems, thrust needs an engine, and maneuvers need an aerodynamic body. All these factors combine with available technology to set a minimum weight for a fighter. No fighter jet can have lesser weight.

Next, although I said mass plays an important role, to be technically precise I should say mass distribution. For the example I gave of instability caused by firing a missile, rotational inertia would help the control system designer. Rotational inertia is determined by the second moment, which in turn depends on mass distribution. For a fighter jet, there is certainly such a thing as being too light in the wrong places.
 
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The internet is a funny place, we really don't know who we are talking to. Otherwise I would have given full weight to your assurances. However, I do think there is a level of phobia when it comes to something new and for the Pak military base, composites may be one such phobia.

To every argument, the unimaginative reply typically is "it will cost too much". And then, bam, they buy something incredibly expensive from abroad. Case in point, the SMG purchase. Later this turned out to be a case of brown envelopes changing hands.

Here is a quote from Burt Rutan on aircraft design:
"If composites had preceded aluminum, we would have never certified aluminum for aircraft, due to its fatigue characteristics and its corrosion issues."
Think you might find it interesting and perhaps detracting from your understanding of the greater scheme of things.

We have a lot of engineers and scientists trained abroad and they come back thinking they know the world. But there is something they don't know. The evolution of those technologies they learned about. When Boeing puts sensor and takes microscopic care to ensure there is no fault in the aircraft, they imagine this is how its done and should be done.

Yet, they never learned the pioneer spirit that is needed that preceded the stage where Six Sigma black belts were needed. Such engineers and scientists can never truly be innovators. Because when you have a nascent industry, you need people who are passionate pioneers, hobbyists. Not "I memorized notes, went abroad and got a degree, now don't try to tell me what I know".

You see, the Wright Flyer wasn't built with Six Sigma. it wasn't stress tested. Neither were the vast majority of the innovations coming out of the West. One does not need to put sensors between composite sandwiches because that is where the bozzo who got his degree from Amreeka is stuck at.

When you have a pioneer mindset, you are willing to make leaps of faith. You are willing to take a risk and "see what happens". That mindset is sorely lacking.

Instead of saying "lets put sensors in the structure" one could have easily said "how does this part generally perform in other similar aircraft". "Can we have a ball-park figure on the MTBF".

If Pak military industrial complex and PAF were such straight thinkers, they would not be needing Chinese assistance at every baby step. Al Khalid would be a proper tank built in numbers and not derided during the Saudi tests. Pak would be able to build a corvette on its own and have some form of SAM systems for all services developed. Drones would not need to be imported left right and center.

So forgive me if your assurances about the competence in the back room is taken with a dose of salt.

I mostly agree with the philosophical argument you are making. What had happened if composites had preceded aluminum. We might have had the advanced models for composite fatigue that we have for metals. I also agree about the lack of imagination in Pakistani military complex. If you go through my post history you'll know how I write about those things too.

But the undeniable fact is that composites didn't precede metals. Even the "US aeronautical engineers who look at PACs aluminum aircraft with disgust" have to either spend money modeling their composite structures or instrumenting them or both. And the fact that they are expensive remains.

Furthermore, my post was about a very specific aspect of aircraft design: the heavy use of composites. And I gave an argument on why it made sense to limit it. This wasn't an argument about the greatness or dumbness of PAC.

And you are right. There's nothing I can say that will convince you of my assurances. It is the web. I have a certain reputation and people might guess what I do and what I know but those are only guesses. I could be a RAW agent for all that matters. But the technical part of my argument stands regardless of who makes that argument. So I hope we all have a better appreciation of the practical challenges associated with the use of composites in aircraft.

With that being said this is the PAF News & Discussion thread, which I do not want to derail anymore.

I can help you become 100% sure.

At a minimum, a fighter needs a human, ammunition, communication, thrust, and maneuvers. The human needs life support systems, thrust needs an engine, and maneuvers need an aerodynamic body. All these factors combine with available technology to set a minimum weight for a fighter. No fighter jet can have lesser weight.

Next, although I said mass plays an important role, to be technically precise I should say mass distribution. For the example I gave of instability caused by firing a missile, rotational inertia would help the control system designer. Rotational inertia is determined by the second moment, which in turn depends on mass distribution. For a fighter jet, there is certainly such a thing as being too light in the wrong places.
I will respectfully disagree. And I am sorry I am unable to respond to your argument because I feel it will waste both our times.

Also, this is the PAF News & Discussion thread, which I do not want to derail anymore.
 
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Okay if you say so MK : )

Hi,

I got my focus back today---yesterday I was busy looking for groceries---only found 1 dozen eggs and a gallon bottle of milk---.

See---in the video the guy is just making a mould---a mould for just general use---.

So---leaving aside the making of the carbon fibre before moulding it to the shape you need---we won't talk about that---.

When you are making carbon fiber for fighter aircraft skin---the process is very high quality control intensive---. Then you have testing done on the material to see the longevity of your mould and wear and tear factor over a period of time---.

One of the biggest concern in using carbon fiber is that testing for micro cracks is not easy---.

An interesting 207 page thesis if someone wants to read it---.

Bottomline---carbon Fiber is wonderful but not without issues---. It is very cost and labor intensive---.

For paf---nothing works like the conventional Aluminum skin---.

But for stepping into the 21st century---one has to use the Carbon Fiber just to show that we use it---we know how to use it---we know how to manage and maintain it---and generally speaking---it is a good selling tool that we are a modern aircraft manufacturer---.
 
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