J-20 5th Generation Fighter VII

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Schwerter_

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So already an aborted take-off?

And here an even better comparison of both the J-20A and J-20B (?). (artwork via @CadderFli and @大包CG from Weibo)

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Radome profile seems to have changed? I vaguely remember seeing a patent from CAC somewhere talking about a new radome design that can reduce drag, wonder if this has anything to do with it
 

Tirdent

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All the "hump for fuel" ideas are based on one assumption that the baseline J-20 has its main fuel tank just behind the cockpit. In that case increasing the thickness of the tank by 10cm at maximum thickness (center line) would give some meaningful volume.

If there is no fuel tank to begin with, one need to not only add a tank but also pumps and tubes to move fuel around to balance the center of mass. Therefor a max 10cm thickness but quickly tapering volume is not going to add meaningful volume of fuel. It is just wasteful.

Volume is nothing unless it is in a desirable shape. Think about this, 10cm increase of depth of your car's back trunk or 10cm increase of leg room in the cabin, both equally increase the length of the car, which one gives you more volume for carrying luggage?

This logic also applies to the "increased room for electronics". Electronics are not plasticine that can be fitted in any volume.

On the other hand, virtually no space is left empty inside a modern 5th generation fighter - even if you are adding volume for primarily aerodynamic reasons, you will be taking advantage of it for other purposes.

Since its fuselage packaging is virtually the same, the F-22 offers a reasonable clue on the J-20 fuel tank configuration, and that indicates there should indeed be a tank there. There's another reason fuel capacity is the most likely use of the additional volume: fuel is the only component that is "malleable" in shape and scales continuously. As you say, electronics have a limited ability to conform to an aerodynamically determined shape, and you'd have to wonder what the original J-20 was even lacking in the avionics department. Is a seventh MAWS sensor (for instance) really sensible, when the six on the base model already provide full spherical coverage?

The one scenario where I can see the volume being used for electronics is if it is occupied by boxes displaced from elsewhere on the airframe by a new piece of (non-avionics) equipment. Say, this new variant gets a gun, and something which originally sat where the gun now is located was moved into the spine.

Like fuel, more weapons would obviously also be always welcome, but missile payload scales in discrete increments and has a fixed geometry. Additionally, the spine adds the most volume well forward of the weapons bay, approximately above the nose gear well. To gain meaningful bay depth, you'd have to move the intake ducts (which curve inward to almost meet on the centreline over the bay) and I just don't see enough new volume in that place for this to happen.

TL,DR: the spine is not going to be empty, and fuel is by far the most likely thing to occupy the additional space.
 

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by78

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Some close-up images to start off the week.

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