H-20 bomber (with H-X, JH-XX)

Brumby

Major
But also that missiles would be better than a stealthy fighter-bomber in most scenarios.
My focus in the conversation isn't about stealth vs stand off weapons. That being said, there are scenarios where standoff munitions would simply not be capable of delivering the intended effects e.g. against highly mobile integrated defenses.

My main question is what constitute the technological or capability attributes of a JHXX that a new platform needs to be built that a re-purposed J-20 cannot deliver. We know as a fact the F-22 has been enhanced with air to ground capabilities. We know that the UK Euro Typhoon has assumed the role of the retired Tornado plane. Modern trend is to go for multi purpose platform by enhancing capabilities - not building dedicated platforms. The JHXX seems to be going in the opposite direction. More payload in my view is a superficial argument.

Desert Storm was a long time ago.
I disagree. The underlying technological capability is not a function of time but technological obsolescence. You need to sustain your argument based on technological facts not brute force reasoning ie. because you think so.

I think a modern stealth fighter-bomber (whether based on the J-20 or a new larger JHXX) would nowadays need electronic jamming aircraft, protective fighter cover, and surface-to-air missile suppression as well.
What is your underlying technological argument and/or CONOPs that you would advance to support your assertions. .

I know as a fact the F-35 community do not want a Growler anywhere near it when it is executing its mission. Active ECM is a sure give away of your presence and directly contrary to the intended usage of VLO i.e. ingress undetected to deliver its munition. The Gulf War experience and the change in tactics support this view where ECM was employed (if any) during egress and not ingress.
The other major problem is stand off jamming creates RF fratricide. You clearly don't want to be blind while going in.

Further ancillary support if any does not change the argument between J-20 vs JHXX as those support are independent considerations . .

And my guess is that a JHXX is being pushed by Xi'An as a JH-7 replacement because they want the work.

SAC is also pushing the J-31 mediumweight fighter, but the Air Force has decided not to pursue it. So I see the JHXX as being in the same situation.

Assuming all planes are equal (which they're not) but just to reply to this particular question: Because real world politics. Because one can't expect that Xian or SAC will ever be given to produce J-20s. Or that CAC will be given so much funds that they triple their production of J-20 while at the same time Xian and SAC get their funds cut (as funds are finite, so if CAC gets more, others will get less)
If the program rs sustained on political lobbying rather than merit than that is beyond my ability to comprehend and I would not labor on it..

I absolutely agree on close in delivery needs. But standoff delivery is not all the same. Say one has a missile with nominal range of 300 km. What if the enemy has air defenses and interceptors positioned 200 km in front of the target. Suddenly the plane needs to get to 100 km of the enemy defenses. VLO may stand a chance there where non VLO won't.
I actually don't understand the point you are making. Obviously stand in vs stand of are not the same.

A VLO platform is tasked with a specific mission because it has the features that can deliver the intended effects. For example, the F-117 was tasked to go after Saddam in the opening air campaign because a stand in delivery was needed. Of course downtown Baghdad would be heavily defended. The account of a F-117 pilot said that an Iraqi plane actually flew next to it. The sudden appearance of any fighter is part of the calculus. The platform is designed to have the capabilities to navigate its way into the intended target area undetected.

My point is stand in delivery require VLO. If stand off delivery is needed you don't need VLO. A non VLO platform can do the job e.g. J-16. As such I don't understand the reasoning why you need big internal bays for standoff weapons. Such reasoning in my view is self conflicting in application. . .

There's no question that a larger airframe that is primarely designed for a strike mission is inherently more capable of achieving more range, more payload and better stealth. That doesn't need to be proven.
Except that what is intuitively relevant is not necessarily sound when Billions of dollars are at stake. Try promoting a product that is inherently better in the real world without consideration of other factors and see how far that gets you.

Another thing with stand off weapons is that range often isn't used in a straight forward way. If the target it 300 km away, one won't just launch the missile and have it go down that shortest, most obvious route. Especially if we're talking about stealthy missiles. Rather, those JASSMs will go along various waypoints around the target, possibly crossing even double the distance, in order to reach the target from less expected and thus less monitored/defended directions.
I am not sure how this is connected to the J-20 vs JHXX conversation
 
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Blitzo

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I agree because without context the entire conversation is meaningless. IMO, we all need to define what we believe are the intended mission sets of the platforms under discussions. Having a greater payload or range is a good thing but platforms in reality are often built on trade offs (F-35) or planned capabilities (F-22). In the context of our conversation my underlying premise is that the H-20 and JHXX are two different platforms and not one. This is based on my understanding of the Pentagon's current assessment While separate platforms, both will incorporate VLO features. The H-20 will probably be of blended wing design with extended range and payload to deliver against targets into the 2nd island chain. That said, I don't believe it will have intercontinental range due to propulsion technology limitations. In contrast, the JHXX is a tactical bomber with range similar to the Flanker family variants. Its primary role is for penetration strike into contested airspace or to engage in SEAD/DEAD missions that would not be permissible with 4th gen assets. Its range would be sufficient to cover most of the immediate theaters associated with the 1st island chain.

I'll elaborate a little bit on what my vision of JH-XX is.

I envision an aircraft with MTOW of 60-70 tons, stealthy, with the internal payload volume to carry the equivalent of 2 YJ-12 sized AShMs (or an equivalent volume of smaller powered standoff missiles, or smaller direct attack munitions), with or without two small sidebays for self defense MRAAMs (PL-15 sized).

This aircraft will have a combat radius of 1500-2000km, with the ability to persist with time on station at that combat radius for over two hours.
The aircraft will be designed optimally for higher and medium altitude flight (not low altitude flight, different to what a few others before have written). I also do not envision this aircraft to be capable of sustained supercruise over mach 1.5, but rather to seek to achieve sustained supersonic dash of over mach 1.5 instead, as part of its normal combat radius + time on station.
Propulsion initially will be high rated WS-10s as stop gap. WS-10s will obviously limit its kinematic performance relative to WS-15s, which will be its intended propulsion.

Those are the main physical characteristics, to establish first, for my vision of JH-XX.


View attachment 56129

The question that keeps surfacing in my mind is why is a JHXX even needed? Where capabilities permit, the J-16s and JH-7s can perform the necessary strike missions. If VLO penetation missions are needed, why can't the J-20s be modified with the targeting systems to conduct such roles? Is a JHXX really necessary because it adds another maintenance tail in to the picture besides the whole supply chain of parts to support another platform? Is payload that important for a tactical bomber to warrant another platform?

During the opening night of Desert Storm, twenty F-117 stealth fighters were able to strike 28 separate targets. Conversely, it took forty non-stealthy legacy aircraft to hit one target because of the need for electronic jamming aircraft, protective fighter cover, and surface-to-air missile suppression. In the first 24 hours, the coalition flew 2,775 sorties. The F-117, combining stealth and precision, hit 31 percent of the targets the first day. In those missions, it wasn't about deep payload but the capability to execute it.


Your take on F-117 is not inaccurate, however I think you are taking the wrong message from the F-117's performance.
The F-117's stealth and precision absolutely allowed it to hit a significant proportion of targets on the first day.
Compared to other aircraft that the coalition had during the Gulf War, the F-117 was leaps and bounds ahead of other aircraft they had for the deep strike role.

However, if the USAF had B-2s in service and mature during that time along with modern munitions, the number of B-2s needed to strike the same number of targets that the twenty F-117s hit would've probably been only a handful.
In other words the B-2's persistence and payload capacity is far superior to that of the F-117, and the benefit of having a larger aircraft with a greater payload capacity despite having a similar degree of survivability or stealth is basically such that you can free up your other "smaller" aircraft for other missions while your larger aircraft does the strike mission.
B-2s would've also been able to carry larger munitions than F-117 could carry if such munitions were available -- and if there were targets that required larger munitions to service then B-2 would've been able to do so while F-117 would not.

Of course the F-117 to B-2 comparison is not perfectly equal to our J-20 vs "JH-XX" comparison. JH-XX will likely only be up to 2-2.5 times as large as the J-20 at most whereas B-2 is many times larger than F-117.
In terms of equivalent A2G payload mass, my vision of JH-XX is able to carry 3 times as much as a single J-20 internally. E.g.: JH-XX would be able to carry 36+ SDB equivalent bombs compared to a J-20 that would be able to carry a maximum of say, 12 in its main ventral bay (hypothetically speaking -- as of yet we have to see J-20 integrated with an SDB like weapon yet or how many it can carry, but it's just to demonstrate the point)
For some large weapons like YJ-12, obviously a J-20 is unable to carry that internally at all whereas my vision of JH-XX is able to carry two.


So, my reasoning for why a JH-XX (or at least my vision of it) is logical for the PLA and why it offers capabilities that the PLA won't have in its other aircraft, is because:

1: payload number/mass: compared to a single J-20, my vision of JH-XX is able to carry three times as much equivalent payload (e.g.: direct attack PGMs like JDAM or SDB equivalents) than a single J-20. That means to hit the same number of targets, you only need 1/3rd the number of JH-XXs to hit those targets compared to J-20. Of course, one can make the argument that having a larger J-20 fleet for that job may be a better investment than buying more JH-XXs, which is why there are two following points below:

2: range and endurance: my vision of JH-XX is able to conduct the mission at a range similar to what a J-20 can do, but with longer time on station than what J-20 is likely able to do. This is not an insignificant difference IMO.

3: payload size: the J-20 has a reasonably sized payload bay for its size. However it also does not have a payload bay that is sufficient to carry large weapons. Weapons like YJ-12 will require a much larger aircraft to carry, and it is likely that there will be a range of future A2G weapons, some of which will be sufficient in size for J-20 to carry but also some that will be too large for J-20. For certain missions, you need the ability to carry a larger weapon, either because you need to launch your weapon at longer standoff range, or because you need your weapon to have a larger mass overall, or you need your weapon to travel at higher speed -- all of which requires your weapon to overall be larger to a smaller weapon if both weapons are of equivalent technological level.


.... now, to repeat, I personally do not believe that my vision of JH-XX is a "must have" for the PLA.

Personally, I can see the reasoning for why JH-XX could be useful but also why JH-XXs mission could be done with a mix of J-20s + H-20s. However, depending on how ambitious the PLA are and how many J-20s and H-20s and JH-XXs they are able to fund and procure, it could also be very reasonable to procure JH-XXs as well in a way that the overall air fleet maintenance or logistics burden is outweighed by the capabilities that JH-XX could offer.

We don't have an answer for what kind of number and mix of J-20s and H-20s the PLA aim for nor what their overall funding and procurement and logistics burden with or without JH-XX is like into the future.
So IMO, it's unreasonable to say that the JH-XX is definitely an aircraft that the PLA "must have" -- but I also think it's unreasonable to say that the JH-XX is an aircraft whose capabilities that the PLA can simply achieve with other aircraft in its fleet of the near future.



(Additionally, between H-20 and JH-XX, I believe H-20 is the more important platform to acquire, because I think H-20 can do many of the missions that JH-XX can do while JH-XX can do much less of the missions that H-20 can do.)
 
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Blitzo

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The reason why a VLO platform is needed for delivery is because the mission requires close in delivery. If standoff delivery is to be employed then a VLO platform is not needed. Just send in a J-16 and fire off from 500 kms away.

This is a separate point that I want to address, because I think the idea of "standoff" and what it means in practice may differ depending on what kind of foe you are facing.
Against a less capable foe, in a situation where the geography of both sides major "targets" and "deployable combat forces" are more equally distant to each other, then perhaps what you're suggesting is more viable.


But for the PLA, their opfor has very capable combat air power, as well as very strong airborne and seaborne sensors -- and importantly they are positioned in a manner that will likely be relatively close to China during periods of high tension and/or conflict.
IMO this means that PLA air superiority in the intermediate range beyond China's immediate airspace in the vital early stages of a conflict will be very challenging to attain, and the opfor has a very capable sensor network both in the air and on the sea.

This is to say, that if the goal is to deliver a standoff weapon with 500km range to a target that is say, 1000km away from China, chances are you will need a VLO aircraft to carry your standoff weapon 500km away to the launch point to begin with, because a non-stealthy 4th gen aircraft will have a significantly higher risk of being intercepted to begin with.

Even in the later stages of a conflict when/if the PLA is able to attain air superiority in the intermediate range, the opfor's longer range sensors that defend their bases and staging areas as well as naval ships and carrierborne aviation will be able to pick up non-stealthy 4th gen aircraft at hundreds of km away and have the ability to intercept or threaten them (either with SAMs, or more importantly with carrierborne fighter aircraft) before your 4th gen aircraft gets within adequate launch range of its standoff weapon.
 

Brumby

Major
This is a separate point that I want to address, because I think the idea of "standoff" and what it means in practice may differ depending on what kind of foe you are facing.
Against a less capable foe, in a situation where the geography of both sides major "targets" and "deployable combat forces" are more equally distant to each other, then perhaps what you're suggesting is more viable.


But for the PLA, their opfor has very capable combat air power, as well as very strong airborne and seaborne sensors -- and importantly they are positioned in a manner that will likely be relatively close to China during periods of high tension and/or conflict.
IMO this means that PLA air superiority in the intermediate range beyond China's immediate airspace in the vital early stages of a conflict will be very challenging to attain, and the opfor has a very capable sensor network both in the air and on the sea.

This is to say, that if the goal is to deliver a standoff weapon with 500km range to a target that is say, 1000km away from China, chances are you will need a VLO aircraft to carry your standoff weapon 500km away to the launch point to begin with, because a non-stealthy 4th gen aircraft will have a significantly higher risk of being intercepted to begin with.

Even in the later stages of a conflict when/if the PLA is able to attain air superiority in the intermediate range, the opfor's longer range sensors that defend their bases and staging areas as well as naval ships and carrierborne aviation will be able to pick up non-stealthy 4th gen aircraft at hundreds of km away and have the ability to intercept or threaten them (either with SAMs, or more importantly with carrierborne fighter aircraft) before your 4th gen aircraft gets within adequate launch range of its standoff weapon.

I would like to pursue the stand off munitions deployment as this is central to the issue under discussions - at least for me.

I note from your earlier related post in arguing for a bigger inner bay for the JH-XX is the requirement to carry at least 2 YJ-12's. According to Wiki, this AShipM has a range of 250 to 400 kms. This mean at a minimum, the launch platform needs to close in to at least 400 kms of the target. The question then is whether a JH-XX vs a J-16 would make any difference in achieving this launch point. I would argue that if the ingress is at sea level, the type of launch platform is irrelevant because, the earth's curvature will limit any detection to less than 50 kms. Say we add complexity into the equation by adding protective CAP over the intended target. Typically F-18s CAP are maintained at 650kms ring around the target. A JH-XX might be detected at 750 kms (650+100) or a J-16 at 850 kms (650+200). In either case, the launch distance is more than 400 kms for the deployment of the YJ-12

I suggest you nominate your scenario to support the idea why a JH-XX is necessary vs other platforms to deliver at effective stand off distances.
 

Blitzo

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I would like to pursue the stand off munitions deployment as this is central to the issue under discussions - at least for me.

I note from your earlier related post in arguing for a bigger inner bay for the JH-XX is the requirement to carry at least 2 YJ-12's. According to Wiki, this AShipM has a range of 250 to 400 kms. This mean at a minimum, the launch platform needs to close in to at least 400 kms of the target. The question then is whether a JH-XX vs a J-16 would make any difference in achieving this launch point. I would argue that if the ingress is at sea level, the type of launch platform is irrelevant because, the earth's curvature will limit any detection to less than 50 kms. Say we add complexity into the equation by adding protective CAP over the intended target. Typically F-18s CAP are maintained at 650kms ring around the target. A JH-XX might be detected at 750 kms (650+100) or a J-16 at 850 kms (650+200). In either case, the launch distance is more than 400 kms for the deployment of the YJ-12

I suggest you nominate your scenario to support the idea why a JH-XX is necessary vs other platforms to deliver at effective stand off distances.

Two reasons.

The first, and less important one, is that flying at sea level means your aircraft will suffer from a meaningfully shortened effective overall range and thus combat radius. This is just a reflection of air resistance.

The second, and much more important reason, is because the opfor will have AEW&C and their own fighter screen equipped with highly networked individual sensors.
That is to say, the opfor will have a very powerful airborne sensor net. The radar horizon limit you described (<50km) is true for naval ships or ground based radar, however the radar horizon for an aircraft operating at cruise altitude of say, 7500m, will have a radar horizon of about 370 km vs your J-16 flying at say an altitude of 10m above the sea surface.

There is a reason why low altitude ingress flight profiles against technologically advanced opfors started to go out of vogue in the late Cold War, and it's because both NATO and the USSR started to field AEW&C and look down radars, making low altitude penetration far less viable than it once was. Not only did AEW&C and look down radars mean aircraft couldn't hide among ground clutter, but it also significantly increased the effective radar horizon that your sensor net had, because now instead of your radars on the ground only having a 50km radar horizon it means you now have a radar horizon which is a function limited only by the power of your radar and how high your aircraft can fly.

Now as we enter the second decade of the 21st century where AEW&C and even fighter radar technology have advanced significantly compared to the late cold war when this technology began to enter service ----- if you are comparing the survivability of a 4th generation strike fighter laden with weapons doing a low altitude flight profile strike mission....

...versus a stealthy supersonic dash theatre bomber...

And both being asked to get to a launchpoint in airspace monitored by a capable opfor with advanced AEW&C patrols and defended networked 5th + 4.5th gen fighter CAP ----- your 4th generation strike fighter's likelihood of getting near its launchpoint is far, far lower than the stealthy aircraft.


To be honest I'm a bit surprised I have to explain the second reason considering I did mention the "very strong airborne and seaborne sensors" part fairly early in my previous post.
 

ougoah

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I see we're still rubbing ourselves on this thread. Think I mentioned something about this going nowhere pages back.
 

Totoro

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My writing here assumes PLAAF sees a strong need for penetrating strikes into heavily defended airspaces on a regular, sustainable basis:

If so, missile strikes are unsustainable option and an option that simply can't perform all mission sets. So a strike aircraft is needed.

It can be a simple, lightly modified J-20. (Basically just avionics) Probably around 40 ton MTOW.
Pros: low cost. Still retains air to air capability so the airframe is multirole, can be used for other missions as well.
Cons: Stealth levels could be better. short range, probably not over 1000 km radius. Low payload and limited payload options. Altogether limited mission set.

It can be a heavily modified J-20. Basically a FB-22 in J-20 form. Probably in the 50-60 tons MTOW range.
Pros: May be able to retain some air to air capability, but probably sacrificing maneuverability and agility. Probably 50-100% greater range. High payload, quite a few options for weapons.
Cons: probably quite costly. Stealth levels, though probably a bit better than with basic J-20, still could leave some to be desired.

It can be a completely clean sheet design. Possibly in the 50-60 tons MTOW range but perhaps more probably in the 60-70 MTOW range.
Pros: could be as stealthy as tech/money allows. Could have greatest range and payload benefits. Size may open up new possibilites such as arsenal plane role and energy weapon platform.
Cons: Costliest option. The larger the plane is, maneuverability and agility is likely to suffer even more.

All three options may use WS20 engines, as heavier planes, if optimized for strikes, could make do with poorer weight to thrust ratio. Heavier planes may have issues attaining supercruise though, but that may or may not be acceptable.
 

Blitzo

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My writing here assumes PLAAF sees a strong need for penetrating strikes into heavily defended airspaces on a regular, sustainable basis:

If so, missile strikes are unsustainable option and an option that simply can't perform all mission sets. So a strike aircraft is needed.

It can be a simple, lightly modified J-20. (Basically just avionics) Probably around 40 ton MTOW.
Pros: low cost. Still retains air to air capability so the airframe is multirole, can be used for other missions as well.
Cons: Stealth levels could be better. short range, probably not over 1000 km radius. Low payload and limited payload options. Altogether limited mission set.

It can be a heavily modified J-20. Basically a FB-22 in J-20 form. Probably in the 50-60 tons MTOW range.
Pros: May be able to retain some air to air capability, but probably sacrificing maneuverability and agility. Probably 50-100% greater range. High payload, quite a few options for weapons.
Cons: probably quite costly. Stealth levels, though probably a bit better than with basic J-20, still could leave some to be desired.

It can be a completely clean sheet design. Possibly in the 50-60 tons MTOW range but perhaps more probably in the 60-70 MTOW range.
Pros: could be as stealthy as tech/money allows. Could have greatest range and payload benefits. Size may open up new possibilites such as arsenal plane role and energy weapon platform.
Cons: Costliest option. The larger the plane is, maneuverability and agility is likely to suffer even more.

All three options may use WS20 engines, as heavier planes, if optimized for strikes, could make do with poorer weight to thrust ratio. Heavier planes may have issues attaining supercruise though, but that may or may not be acceptable.

As far as what the JH-XX may be like, if it were real, I think opening the various options to a variety of different hypothetical categories is sensible for the sake of discussion.

But I think if we're wanting to be guided by what little indications we have of JH-XX, I think we cannot help but to take this concept below as guidance as that is the concept which has been most strongly associated with the JH-XX moniker.

CrdWi5s.jpg


ZpRMSHH.jpg



IMO, discussions around the idea of the PLA actually acquiring a hypothetical JH-XX should seek to consider what kind of performance and capabilities that particular concept may offer -- which of course in turn informs my vision of what I believe JH-XX would be, i.e.: that the aircraft looks like it is in the 60-70 ton MTOW range.


=====

That said, I agree with all of what you've written in regards to the potential roles and benefits that JH-XX may bring (within all three of your different visions).


However, I think we should take a step back and take stock of what we can reasonably ask at this stage based on what we know of the PLA's present and future stealthy strike capable platforms in context of its overall strike requirements.

IMO, once we review that, here are two important questions which I think we can only reasonably ask at this stage, where the second follows the first.


Question one: is the PLA interested in a JH-XX or working on JH-XX?
Answer one: IMO the best answer we can give is we do not know. We all consider the H-20 to be "near-confirmed" in terms of its existence and expectation, and I think everyone has a bit of a consensus for what H-20 will look like more or less (flying wing, four engines, stealthy, subsonic), and what kind of capability set it will aim for. However, JH-XX at this stage is a "rumour" or at best a "credible rumour" and we don't know if it is actively being worked on or pursued by the PLA.

Based on the answer of question one, we get question two, and this is the one we're all quibbling over.....

Question two: could the PLA seek to procure a hypothetical JH-XX?

IMO the answer to this question is "yes, depending on a number of other factors".
Those other factors include:
- the exact capability/mission profile of what a hypothetical JH-XX might be
- the overall funding and resources that the PLA has (or will have in future) at large
- the procurement size that the PLA will want for their stealth combat aircraft whose existence is confirmed (J-20) or near confirmed (H-20), both of which may be able to fill some of the roles that a hypothetical JH-XX can do -- but where the introduction of JH-XX could still provide a significant and unique capability which may be worth the investment into another platform and its own unique logistics and support chain.


IMO beyond those questions and answers we aren't able to get into much more detail with great confidence in terms of what we know and what we can reasonably estimate for this JH-XX rumour that has been persistent over the last year or two.

The question of "whether JH-XX is needed" IMO is the wrong kind of question to ask, because it should really be translated as "whether the PLA will seek to procure it" -- which in turn is really asking "could the JH-XX offer capabilities the PLA will benefit from, and would it be the best choice to offer the PLA the best balance of capabilities in the future when considering the opportunity-cost of alternative procurement plans".... and that is a question that we of course aren't able to answer.

(And edit: I assume you mean WS-15 or WS-10 rather than WS-20. A high bypass engine like WS-20 for a supersonic stealthy regional bomber doesn't really make sense)
 

Xizor

Captain
Registered Member
My writing here assumes PLAAF sees a strong need for penetrating strikes into heavily defended airspaces on a regular, sustainable basis:

If so, missile strikes are unsustainable option and an option that simply can't perform all mission sets. So a strike aircraft is needed.

It can be a simple, lightly modified J-20. (Basically just avionics) Probably around 40 ton MTOW.
Pros: low cost. Still retains air to air capability so the airframe is multirole, can be used for other missions as well.
Cons: Stealth levels could be better. short range, probably not over 1000 km radius. Low payload and limited payload options. Altogether limited mission set.

It can be a heavily modified J-20. Basically a FB-22 in J-20 form. Probably in the 50-60 tons MTOW range.
Pros: May be able to retain some air to air capability, but probably sacrificing maneuverability and agility. Probably 50-100% greater range. High payload, quite a few options for weapons.
Cons: probably quite costly. Stealth levels, though probably a bit better than with basic J-20, still could leave some to be desired.

It can be a completely clean sheet design. Possibly in the 50-60 tons MTOW range but perhaps more probably in the 60-70 MTOW range.
Pros: could be as stealthy as tech/money allows. Could have greatest range and payload benefits. Size may open up new possibilites such as arsenal plane role and energy weapon platform.
Cons: Costliest option. The larger the plane is, maneuverability and agility is likely to suffer even more.

All three options may use WS20 engines, as heavier planes, if optimized for strikes, could make do with poorer weight to thrust ratio. Heavier planes may have issues attaining supercruise though, but that may or may not be acceptable.
WS-20 is high bypass engine ? I thought High bypass engines were subsonic friendly and were not going to function well in supersonic flight. Wouldn't the Fan up front that generates much of the high thrust, find difficulty "catching" supersonic airflow ?
Maybe WS-15. And we don't even know much about its readiness. In my books, it is a mythical engine. It doesn't exist.
WS-10 is the only good hope for China.
 

Brumby

Major
Two reasons.

The first, and less important one, is that flying at sea level means your aircraft will suffer from a meaningfully shortened effective overall range and thus combat radius. This is just a reflection of air resistance.
While I agree to ingress at sea level will degrade effective range, that itself does not necessarily exclude it as a viable option. They are not mutually exclusive.

The second, and much more important reason, is because the opfor will have AEW&C and their own fighter screen equipped with highly networked individual sensors.
That is to say, the opfor will have a very powerful airborne sensor net. The radar horizon limit you described (<50km) is true for naval ships or ground based radar, however the radar horizon for an aircraft operating at cruise altitude of say, 7500m, will have a radar horizon of about 370 km vs your J-16 flying at say an altitude of 10m above the sea surface.

The main question is whether it gets you to your effective launch point even with the airborne sensor net. I don't see a compelling argument you are making that changes the equation.

There is a reason why low altitude ingress flight profiles against technologically advanced opfors started to go out of vogue in the late Cold War, and it's because both NATO and the USSR started to field AEW&C and look down radars, making low altitude penetration far less viable than it once was. Not only did AEW&C and look down radars mean aircraft couldn't hide among ground clutter, but it also significantly increased the effective radar horizon that your sensor net had, because now instead of your radars on the ground only having a 50km radar horizon it means you now have a radar horizon which is a function limited only by the power of your radar and how high your aircraft can fly.
I would differ with your view as to the reason why low level ingress fell out of fashion. Manpad and anti aircraft guns became a problem. Most of the air losses from Iraqi freedom came from it and not from SAMs. The Kosovo campaign had flight restriction on allied aircraft below 10000 feet for the same reason. In the case of an engagement at sea, such problems do not exist.

Now as we enter the second decade of the 21st century where AEW&C and even fighter radar technology have advanced significantly compared to the late cold war when this technology began to enter service ----- if you are comparing the survivability of a 4th generation strike fighter laden with weapons doing a low altitude flight profile strike mission....

...versus a stealthy supersonic dash theatre bomber...

And both being asked to get to a launchpoint in airspace monitored by a capable opfor with advanced AEW&C patrols and defended networked 5th + 4.5th gen fighter CAP ----- your 4th generation strike fighter's likelihood of getting near its launchpoint is far, far lower than the stealthy aircraft.
You have yet to demonstrate specific numbers why 4th gen aircraft using standoff weapons cannot achieve the desired end effects. It is not a 4th gen vs 5th gen conversation. It is a 4th gen with stand off delivery vs 5th gen with stand in delivery conversation.
To be honest I'm a bit surprised I have to explain the second reason considering I did mention the "very strong airborne and seaborne sensors" part fairly early in my previous post.
Making a statement of strong airborne and seaborne sensors is meaningless because it is about their relevancy to the equation and not simply their presence.
 
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