Getting the engine would be a problem, even today if i am right, China needs to buy Russian engines for its fighters.What if North Korea decides to plan and manufacture an indigenous fighter/attack aircraft.I think it would seemed like this:
Getting the engine would be a problem, even today if i am right, China needs to buy Russian engines for its fighters.What if North Korea decides to plan and manufacture an indigenous fighter/attack aircraft.I think it would seemed like this:
China buys Russian engines for some of their fighters because they can produce airframes, avionics and armarment faster than they could produce huge jet engines to fit them and for lesser projects oriented at export they prefer to have Ukrainian and Russian that are readily available.Getting the engine would be a problem, even today if i am right, China needs to buy Russian engines for its fighters.
China buys Russian engines for some of their fighters because they can produce airframes, avionics and armarment faster than they could produce huge jet engines to fit them and for lesser projects oriented at export they prefer to have Ukrainian and Russian that are readily available.Getting the engine would be a problem, even today if i am right, China needs to buy Russian engines for its fighters.
As for North Korea, it is known that they are able to produce RD-9 turbojet since at least early 1980s, RD-9 is used in Mig-19 / J-6 along Yak-25 and Q-5 while also Su-25 prototype. They recently tested land attack cruise missile with 1500 kilometer range and boasted about producing turbofan engine, longer range than Iranian LACM that is using R95-300 engine and demonstrated 1200 kilometer range while Chinese LACM has at least 1500 kilometer range and probably TRDD-50 equivalent engine.
A cruise missile turbofan engine only needs to keep running as long as it takes to cover the 1,500km, it needs to work for probably less than 3 hours. Its expendable, you don't need to worry too much about quality control at all.They recently tested land attack cruise missile with 1500 kilometer range and boasted about producing turbofan engine,
They invest in ballistic missiles and cruise missiles because it is most cost effective and most potent way to increase military power for them at the moment as those will be most potent weapons when ever if ever Korean War continues without any restriction, all out war.So why have we not seen a North Korean clone of, lets say the Mig-29, is it because North Korea knows that in a war the air force will be outnumber and mostly used for defense while balletic missiles and cruise missiles can be used for offensive warfare.
First of all there is no evidence that North Korea is modding up An-2's as UAVs and you are likely confusing them with Azerbaijan or you saw North Korean modifying An-2s with terrain radar for their special forces to fly as low as possible during night and heavy fog.A cruise missile turbofan engine only needs to keep running as long as it takes to cover the 1,500km, it needs to work for probably less than 3 hours. Its expendable, you don't need to worry too much about quality control at all.
Smaller turbofans for cruise missiles are not super advanced, nations like South Africa for example were able to develop extensive series of such engines relatively inexpensively.
A turbofan for a fighter needs far better quality control and service life of tens of thousands of hours. North Korea would have built its own lighter aircraft, trainers or helicopters by now if it really had a working aero engine industry but instead they are modding up old An-2s as UAVs.
The RD-9 is a museum piece, they were building them in the 1980s when the design was already over 30 years old!
It doesn't change fact that they gain knowledge and experience that is applicable to larger engines by applying what they learned.And in fact the Soviet R-15 engine demonstrated exactly that problem. The engine had been originally designed for an expendable Mach 2 drone, and required considerable design work both to have acceptable (by Soviet standards, even) reliability and to be able to handle the variable speeds of a fighter rather than the constant cruise of the drone.
Fighter engines have not gotten any less sophisticated, and the need for long service lives has only increased.
Superficially, but there's likely a profound difference in the blade metallurgy you need for a couple of minutes of rocket boost with continuous acceleration longitudinal to the vehicle, and the blade metallurgy you need for a couple of hours of flight with sudden acceleration transients coming in from a variety of directions in an aircraft manouvering under high-gee. Amd especially if you want the ability to go out and do it again tomorrow, and the day after, etc. This particularly applies if the rumours a considerable chunk of NK rocket technology actually came from the Ukraine are true, as it may mean NK has the knowledge to manufacture turbopumps, but not necessarily to design them, and their metallurgy, from scratch.production of turbopumps for rocket engines is not entirely separate from jet engines
The K-10S is an antique of a missile dating back to the 1950s, which doesn't speak well to the viability of its engine in the modern day. The Hound Dog missile was a contemporary, also supersonic, and its J52 engine is long since out of production with the remaining engines on aircraft either twenty years retired or else replaced with more modern engines.As for RD-9, variants of it were used for K-10S along prototype or initial version of Tu-141 and for Su-25 prototype hence that museum piece has a lot of potential considering K-10S is supersonic anti-ship cruise missile and consider that if North Korea made such class of ASCM powered by RD-9 with modern sensor suite that their Kh-35U equivalent with thermal seeker being used in terminal stage.
We don't know what else they may produce, we can speculate on basis of what they have and since they became capable of producing RD-9 turbojet engine in early 1980s thus it would be wise that we don't assume that they didn't reverse engineer and produce more relevant jet engines around 40 years after they started producing RD-9. So who knows, maybe right now they produce R-25-300 ...
Ukraine and Russia both made it very political about from whom allegedly North Korea acquired covertly information about liquid fuel rocket technology involving RD-250 among other things, no solid evidence ever released of any of their rocket scientists from either country coming to North Korea unlike when through proxy purchase of Foxtrot and Golf class submarines as scrap metal in 1990s.Superficially, but there's likely a profound difference in the blade metallurgy you need for a couple of minutes of rocket boost with continuous acceleration longitudinal to the vehicle, and the blade metallurgy you need for a couple of hours of flight with sudden acceleration transients coming in from a variety of directions in an aircraft manouvering under high-gee. Amd especially if you want the ability to go out and do it again tomorrow, and the day after, etc. This particularly applies if the rumours a considerable chunk of NK rocket technology actually came from the Ukraine are true, as it may mean NK has the knowledge to manufacture turbopumps, but not necessarily to design them, and their metallurgy, from scratch.
The difficulty China has had reaching similar standards to Russian engines, even with an export relationship and an existing jet engine manufacturing capability, illustrate that there is not simply a logical progression from one techology to the other.
The fact is your reply doesn't make sense considering what I wrote and I suggest you to read again my reply, in case you are not able to understand it even after reading it again then I simply suggest you to not bother replying as it would again not make any sense.The K-10S is an antique of a missile dating back to the 1950s, which doesn't speak well to the viability of its engine in the modern day. The Hound Dog missile was a contemporary, also supersonic, and its J52 engine is long since out of production with the remaining engines on aircraft either twenty years retired or else replaced with more modern engines.
The fact that the Soviets did, in fact, replace the RD-9 on the Su-25 prototype almost fifty years ago also doesn't speak well to the current viability of the RD-9.
As for the R-25, that's no spring chicken of an engine either. It was first run in 1971, and is wholly inferior not only to current engines, but also last-gen engines like the RB199, F404, and RD-33.
And the F-5 is not a competitive fighter anymore, what's your point?China continues to use RD-9 for their Q-5 ground attack jet aircraft and there are other jet engines from around same time that are used to this day including J85 on F-5s that still fly to this very day while single RD-9 is roughly comparable to two J85 engines used by F-5.
Exactly, we have almost no evidence of any indigenous aircraft industry at all.As for their aero engine industry, we don't know much except very few details that I have mentioned while you choose to grasp straws by essentially asserting that they can't do this or that simply because I have not made assertion that they could do something else too.
Yes and why do you say that? Did I anywhere assert it to be the case? No.Bluntly, the ability to produce cruise missiles is not an indication of ability to produce a decent fighter.
Which is what we're talking about, not a supersonic antiship missile.
Why are you focusing on F-5 when you were talking about viability of RD-9? Because I pointed out that J85 is still in use while being still in use just as is when Chinese produced RD-9 designated WP-6 with JJ-6 and Q-5 still in service as decommission process is gradual.And the F-5 is not a competitive fighter anymore, what's your point?
I did not say it wasn't retired and just because it is retired does not mean that it is not being used.The Q-5 is retired, according to every public source I can find.
RD-9 is 25% heavier than two J85-GE-21 combined.Also, no, a single RD-9 is not comparable to two J85s. A single RD-9 is less thrust (6600/8300 versus 7000/10,000) for more weight (1600 lbs versus 1280 lbs) and fuel consumption (1.02 lb/(h·lbf) versus .96).
Exactly, we have almost no evidence of any indigenous aircraft industry at all.
Then why the hell do you keep talking about cruise missiles when this is a thread about the North Koreans developing a fighter? I assumed you were in some way tying it to fighter development, because otherwise this is extremely off-topic.Yes and why do you say that? Did I anywhere assert it to be the case? No.
You are framing it as such when I stated what is know about what they achieved and it certainly was not focused on jet engines for cruise missiles as you and other choose to grasp straws about that while ignoring other elements besides jet engines such as ability to produce passive electronically scanned array radars such as 30N6E and 48N6 equivalent surface to air missile along recently testing new surface to air missile reminiscent of 9M96E2 with addition of large solid fuel booster thus they have decent radar and anti-air missile technology.
I'm focusing on the F-5 precisely because you pointed out that the J85 is in use - it is in use on a fighter that's not competitive in air to air and is on the way out. As for the J-6 and Q-5, well, I'll admit to being a little hasty in declaring the Q-5 out of service, but the J-6 definitely is (pg.15), and this brings me back to my original point: just because the engine is being used does not mean it's a viable fighter engine. The Q-5 is old, a dedicated ground attacker, being shoved out of service as fast as the Chinese can afford to do so, and was produced at a time when China couldn't do any better than modify the MiG-19. None of this points to it being useful for a current fighter project.Why are you focusing on F-5 when you were talking about viability of RD-9? Because I pointed out that J85 is still in use while being still in use just as is when Chinese produced RD-9 designated WP-6 with JJ-6 and Q-5 still in service as decommission process is gradual.
That is my point when you complained about RD-9 not being viable while its still being used just like J85.
As for F-5 when you mention about it not being competitive fighter, do you mean in original configuration made by its manufacturer or localized upgrades since Brazil arranged extensive upgrades of F-5s that those can use Derby BVRAAM and they outlived Mirage 2000.
You have zero evidence that that 2.3-fold increase carries over the -21 model. And even if it did that doesn't change all the rest of the advantages the twin J85 setup has over a single RD-9.RD-9 is 25% heavier than two J85-GE-21 combined.
Two J85-GE-21 combined produce 6 percent more thrust without afterburner and RD-9 consumes 6 percent more.
RD-9 when using afterburners consumes (1.66 lb/h·lbf) per kN.
J85-GE-5 on T-38 Talon for example consumes (0.57 lb/h·lbf) per kN and (1.34 lb/h·lbf) per kN using afterburners.
Apply that 2.3 fold increase to J85-GE-21 used on F-5E Tiger II and that would be (2.23 lb/h·lbf) per kN when using afterburners.
J85-GE-21 would be consuming 34% more per kN with afterburners while generating 20% more afterburner thrust than RD-9.
That means that North Korea has managed to seriously developed her aerospace industry so the designing and production of an indigenously fighter aircraft must be considered as likely.
Is North Korea’s MiG-29 Fleet Growing?
License production contracts with Russia and technical assistance deals may be strengthening North Korea’s air force.thediplomat.com
This story is a great demonstration of my maxim that any headline which ends in a question mark can be answered by the word "no." The reason why journalists use that style of headline is that they know the story is probably bullshit, and don’t actually have the sources and facts to back it up, but still want to run it.
That is the problem, you assume too much by going with reading between lines attitude to assert something I didn't.Then why the hell do you keep talking about cruise missiles when this is a thread about the North Koreans developing a fighter? I assumed you were in some way tying it to fighter development, because otherwise this is extremely off-topic.
It is relevant as armament is one of factors involving development of fighter jets as you could have AAM with range of 300km at most against AWACS / AEW yet radar that is not competent enough to detect and track it to guide AAM to shot those down or you could have radar with range to detect and track yet don't have AAM that could reach those hence not fully utilizing potential of one or another.If I'm ignoring something, it's because it's either not relevant, in the case of the SAMs, or I've already conceded it in the case of the PESA radar. See, this is my point: why on earth is their ability to develop a surface to air missile relevant to their ability to develop a fighter? It's not.
I said JJ-6 that is two set trainer jet of J-6 and which Q-5 as there is Q-5B with Type 317 and 317A radar thus is a strike fighter.I'm focusing on the F-5 precisely because you pointed out that the J85 is in use - it is in use on a fighter that's not competitive in air to air and is on the way out. As for the J-6 and Q-5, well, I'll admit to being a little hasty in declaring the Q-5 out of service, but the J-6 definitely is (pg.15), and this brings me back to my original point: just because the engine is being used does not mean it's a viable fighter engine. The Q-5 is old, a dedicated ground attacker, being shoved out of service as fast as the Chinese can afford to do so, and was produced at a time when China couldn't do any better than modify the MiG-19. None of this points to it being useful for a current fighter project.
And I mean both - Brazil's F-5s are rocking a small pulse-doppler radar set and frankly would get eaten alive by any sort remotely modern fighter. They've outlasted Brazil's Mirage 2000 fleet not on any sort of technical merits, but because the Mirage 2000s were hand-me-downs from the French Air Force (And thus old) and the maintenance contract with Dassault was about to run out.
Yes, without consideration of 2 engines compared 1 engine involving provisions to mount those 2 engines along there being 2 intakes.You have zero evidence that that 2.3-fold increase carries over the -21 model. And even if it did that doesn't change all the rest of the advantages the twin J85 setup has over a single RD-9.
They certaintly did not license from USSR to domestically produce Mig-29 and I know individual that worked as journalist before being game developer for an MMO that did some research, from what they could figure out from trade documents and what not that North Korea may have received technical data to produce some components of Mig-21 such as airframe along likely that North Korea got technical data along manufacturing tools to produce R-60 short range air to air missile.Some sources indicates that North Korean MIG-29 fleet is growing by assembling imported parts from Russia. These sources claims that the North Koreans have managed to locally produced improved versions of MIG-29 by a rate of five aircrafts per two years for the past 25 yeras. It seems that North Korea MIG-29 fleet numbers more than 100 samples(36 of the initial order from USSR in 1988+ 12 MIG-29S imported from Kazhakstan along with 70 MIG-21bis in 1992 + 60+ planes locally being assembled). That means that North Korea has managed to seriously developed her aerospace industry so the designing and production of an indigenously fighter aircraft must be considered as likely.
Iran is producing reverse engineered J85-GE-21 turbojet engine and has also reverse engineered FJ33 turbofan engine.Most countries start with something simple like a piston trainer and work up from there. India, Turkey and South Korea all demonstrated wide capabilities in general aerospace, large quantities of licensed builds, and engaged major partnerships with US and/or European industry to get to the point where they could design an indigenous fighter. North Korea at best could aspire to be an Iran.
North Korea is much larger than for example Taiwan that at most it is 390 kilometers from one end to another at most and shortest is 130 kilometers compared to North Korea being 700 and 300 kilometers respectively hence argument based on size is flimsy one.North Korea doesn't seems to be interested much in refitting their air force. The possible reason is, that they realize, that attempts to produce ingenious combat aircraft would consume a lot of time and resources - and would not bring significant advantages. The aerial superiority of potential adversaries is just too great, and North Korea territory is too small to provide for sufficient aircraft dispersion.
They are and there is no arguing about that yet they have limitations, ballistic missiles are useful against land targets are too cruise that can also target ships yet then aircraft carriers come into play as you may not have range to target them with cruise missiles unless you are Russia or China that even has anti-ship ballistic missiles along Iran that has short range ones.So, they invested mostly in missiles, which are just more cost-efficient.
At some point they will have to invest in designing and producing fighter jets.
*pinches nose*That is the problem, you assume too much by going with reading between lines attitude to assert something I didn't.
It is loosely tied to fighter development, issue is how you try to portray it as direct when it is not as you miss my point or are disingenuous.
When I mentioned cruise missiles, it is not about fighter development as you jumped to that conclusion as it is about their defense industry and technology used that in current state would not be use of for development of fighter jet thus I stated contextually that should be very obvious to you that by continuing to further develop and advance related technologies that at some point will be of use for fighter jet.
Why don't we look at Iran for example, at first they developed manufacturing capacity to reproduce various small turbojet engines for cruise missiles and they continued to invest in capability to produce jet engines which resulted in them being able to domestically make J85-GE-21 turbojet engine that is much larger and more complex than Tri-60 series used in Iranian cruise missiles and target drones.
Iran has reverse engineered FJ33 that is downscaled older FJ44 thus Iran has option to invest resources in upscaling it to FJ44 then attempt to reach performance of FJ44-4 that is larger than and as heavy as J85-GE-21 while providing same dry thrust at the half fuel consumption.
Then finally they would need to develop afterburner component for it and considering it being turbofan and diameter of FJ44 that thrust from afterburning should be considerably greater than 22kN that J85-GE-21 is capable of producing, at least 30 kN seems reasonable.
Okay, but it still doesn't tie into the ability of North Korea to design and build an indigenous fighter.It is relevant as armament is one of factors involving development of fighter jets as you could have AAM with range of 300km at most against AWACS / AEW yet radar that is not competent enough to detect and track it to guide AAM to shot those down or you could have radar with range to detect and track yet don't have AAM that could reach those hence not fully utilizing potential of one or another.
Its absurd to write off AAM from fighter development process, might as well be fine with F-22 without BVRAAM.
What does any of this have to do with the ability of North Korea to develop an indigenous fighter?I said JJ-6 that is two set trainer jet of J-6 and which Q-5 as there is Q-5B with Type 317 and 317A radar thus is a strike fighter.
Q-5 came around same time as J-7 and production of both ended around same time.
EL/M-2032 is used by by Thai and Chilean F-5E's and Grifo-F is being used in Brazilian and Singaporean F-5E's.
EL/M-2032 was also implemented for Chinese J-7G and had 60km range.
Grifo-7 radar with weight of 55kg implemented for Pakistani F-7P and had range 55km range..
Weight of Grifo-F in F-5E's is 87kg hence you can speculate how much larger and more powerful is compared to Grifo-7.
Same for EL/M-2032 between implementation in J-7 and F-5E's.
Elbit states maximum range for look up air target detection at most 120 miles that is 220 kilometers. Not specified on what platform.
Fair enough. This site has the data for the J85-GE-21: 35.15 g/kN/s (Pg. 16). The same site gives the RD-9F's SFC as 25.48 g/kN/s (Pg.12). So it looks like yes, the twin J85s would consume more fuel than the single RD-9.Yes, without consideration of 2 engines compared 1 engine involving provisions to mount those 2 engines along there being 2 intakes.
Also we don't know if figures you cited are for J85-GE-21 and if you took those figures from Wikipedia where it is vague by not being specific which model of J85 is as maximum thrust is stated as 11-22 kN as 11kN is J85-GE-5 dry thrust and 22kN is J85-GE-21 afterburner.
Iran has been refurbishing, modifying and modernizing various models of F-5 and same for J-85 turbojet engines while main obstacle to domestic production of new fighter jets based on F-5 was J85 engine which Iran has few years ago reverse engineered to the J85-GE-21 equivalent while there are differences such as different sound of the jet engine and lack of black smoke trail from exhaust which I have to note that in general it is indication of better fuel efficiency and maybe also greater thrust compared to original as was the case with Russia involving RD-33MK compared to original RD-33 that also introduced digital FADEC thus if we refer to Iranian claim of 4th generation avionics in Kowsar for which digital FADEC would fit right in as one of crucial features of a 4th generation fighter jet avionics.Why? The alleged Iranian projects to date have been somewhat wobbly. The furthest they've gotten in actual flyable hardware is minor changes to the F-5, which was already obsolescent back when the Shah was still in charge. If Iran needs competitive combat aircraft I'd expect them to buy from China, because (looking across the Gulf) there is no chance of Iran being able to build an aircraft, plus AAMs, indigenously that's capable of taking on late-model F-15s, F-16s, Rafales, and Typhoons using AIM-120.
It defies belief that they couldn't copy the RD-33 if they choose to do so
Yes...'cold feet'....after 8yrs of development (1996 program start to initial F404 buy) which has turned into ~25yrs now and yet there are still no production Tejas flying with Kaveri engines.so instead of persevering to fix the issues they got cold feet, they just buy engines from abroad.