Chinese UCAV/CCA/flying wing drones (ISR, A2A, A2G) thread

latenlazy

Brigadier
The DSI inlet, being non-adjustable, can only be optimised for a single cruising speed range. In contrast, conventional inlets feature internal or external adjustability, enabling them to maintain high efficiency across multiple cruising speeds. Therefore, it is not accurate to state that DSI inlets are only suitable for transonic or high subsonic ranges.
A “single” speed *range* is multiple speeds :p

Having a DSI also does not exclude possible adoption of other inlet adjustment mechanisms.
 

Nevermore

Junior Member
Registered Member
A “single” speed *range* is multiple speeds :p

Having a DSI also does not exclude possible adoption of other inlet adjustment mechanisms.
Speed is a range, just as different bypass ratios correspond to different optimal speed ranges. Additionally, it is indeed possible to internally modify the DSI intake duct to make it adjustable, but this could be extremely complex—at least I haven't seen such a design yet.
 

plawolf

Lieutenant General
Italian guy's new video on the type B UADF, some of his points:

1. He correctly recognizes it as very important and different in nature to other smaller CCAs from around the world
2. He reckons due to it having a rhomboidal wing without canard or wing tip devices that it's optimized for speed and not agility
3. He misidentifies the engine as WS-15 due to serrated petals, not realizing/forgetting that WS-10C has them too
4. He guesses from DSI intake that the aircraft is optimized at around transonic speed
5. He recognizes they can of course act as CCAs, but their larger size and evidentially capacity for electronics inside means they could also operate in a different mode. He guesses either full autonomous fighter or remote control fighter, he's leaning towards full autonomous fighter.

My opinions are I'm not sure why DSI would indicate optimized for transonic speed given J-20 has DSI intake and can reach Mach 2. I take Xiyazhou's argument that these UADFs can be thought of as a JF-17 sized aircraft fitted with J-10's engine, which should mean excellent thrust to weight ratio. Without the drag from a cockpit these things should be pretty fast as far as top speed go.

I wonder what kind of thrust to weight ratio an aircraft of that size would have if fitted with a WS-15, must be some scary number.

I think the choice of WS10 is more to do with the electrical power requirements of the UADF rather than raw thrust. Although that additional thrust is not going to hurt or go to waste either.

With no cockpit or vertical tails, that thing will have insanely good drag coefficient. As such, I don’t think it will be optimised for transonic flight, rather it will be optimised for high supercruise and will probably only drop to subsonic for take-off and landings and where speed restrictions are in place to avoid annoying people on the ground with sonic booms.

With the kind of TWR it will have, it can absolutely afford the thrust penalty from having stealthy nozzles. So either the RCS treatment on the existing nozzles are good enough; or they are waiting for stealth nozzles to be developed, or they need all that thrust for the kinds of high supercruise this thing is designed to live in.
 

Temstar

Brigadier
Registered Member
Shilao and Yankee talked again about the UADFs tonight among other things, although they used kind of vague terms. They implied:

1. CAC and SAC were rather surprised that the two UADFs were called to participate in the parade, in their opinion it's a lot earlier than expected

2. the UADFs actually have quite a lot of focus on dogfighting, as sort of insurance and bodyguard for J-20S and 6th gens which are highly focused on BVR. Yankee mentioned offhandedly "20G" but I'm not sure if that's just a figure of speech showing AI's advantage to human or if its meant to be taken literately

3. In experiments with manned fighter pairings it's found that UADFs are particularly fast at reaching for the kill shot compared to human pilots. To the point that human pilots afterwards complain of the AI doing "kill steal" on them. Pilots being highly prideful folks sometimes had to be comforted with words like "yeah but he's a computer, he's never going to get a promotion over you no matter how many kills he score" and "it's not about who gets the kill, it's about winning together as people's air force". Yankee joked that maybe for morale sake they need to figure out a way for AI to toast humans at the dinner afterwards to smooth things over.

4. The very best human pilots can still outfight an UADF, but it's physically and mentally exhausting and if immediately faced with another UADF they're very unlikely to win again.

5. Yankee described the UADFs as "not a gram of it was for a strike role, every bit of it is for air superiority". Instead of smaller CCAs (MQ-28, YFQ-42 and YFQ-44 mentioned here as examples) they said given their size and the power of their engine it's more useful to think of them as unmanned J-10.

6. Shilao described a scenario for their use. Imagine a J-20S (might have been J-36, I forgot) and a F-22 snuck on on each other with their stealth. They get into WVR combat and J-20S takes out a pair of PL-10 while F-22 starts spinning it's gun. Shilao describes using 5th gen this way ("knife fight in a phone booth" as he puts it) as "不体面" or "unbecoming" for high tech fighters. Instead if J-20S had a UADF bodyguard it could just tell it to dogfight and beat the F-22 while it gets away.

7. The very smooth and highly polished appearance was a requirement from higher up. In CAC and SAC's opinion these aircrafts have not yet reached a stage where such care and attention to detail are required. But the order from above was slick and aesthetic appearance was also a requirement for displaying such advanced aircrafts so they insisted on it much to CAC and SAC's annoyance. The new paint job for J-20A and J-20S was for similar reasons and to differentiate them from regular J-20. The powers that be understand the soft power advantages that came with showing off cool looking aircrafts.
 
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mack8

Junior Member
Ok so at least we now know they are from SAC and CAC. As for the 20g, well that is more than i expected, a lot more, but since there is no human pilot onboard the limit now will be airframe strength. Also the above implies they have been in testing for quite a while, which align with at least Type B being spotted back in 2021.

Not the topic, but did they said anything about the current status of J-36/J-50? Seems a few months have passed since the last confirmed flights. If there is anything perhaps a brief update can be posted in the relevant topics.
 

Nautilus

New Member
Registered Member
5. The very smooth and highly polished appearance was a requirement from higher up. In CAC and SAC's opinion these aircrafts have not yet reached a stage where such care and attention to detail are required. But the order from above was slick and aesthetic appearance was also a requirement for displaying such advanced aircrafts so they insisted on it much to CAC and SAC's annoyance. The new paint job for J-20A and J-20S was for similar reasons and to differentiate them from regular J-20. The powers that be understand the soft power advantages that came with showing off cool looking aircrafts.
I wonder if they were annoyed because the slick look required some (presumably minor) compromises in other areas or because it was simply effort that could have gone into other areas.

Also, "not yet reached a stage where such care and attention to detail are required" -> so these aircraft are still under active intensive development and not IOT&E?
 

Temstar

Brigadier
Registered Member
Ok so at least we now know they are from SAC and CAC. As for the 20g, well that is more than i expected, a lot more, but since there is no human pilot onboard the limit now will be airframe strength. Also the above implies they have been in testing for quite a while, which align with at least Type B being spotted back in 2021.

Not the topic, but did they said anything about the current status of J-36/J-50? Seems a few months have passed since the last confirmed flights. If there is anything perhaps a brief update can be posted in the relevant topics.
6th gen wasn't mentioned except the two UADFs were described as "little brothers" representing their "big brothers" who can't come. I guess that means Type A is from SAC and Type B is from CAC based on satellite photo of Type B at CAC?

I wonder if they were annoyed because the slick look required some (presumably minor) compromises in other areas or because it was simply effort that could have gone into other area.
I was thinking the later, like how prototypes usually don't need all the fine details that's required for production VLO aircrafts. Recall T-50 prototypes finish compared to production Su-57.
 

Deino

Lieutenant General
Staff member
Super Moderator
Registered Member
Shilao and Yankee talked again about the UADFs tonight among other things, although they used kind of vague terms. They implied:

1. CAC and SAC were rather surprised that the two UADFs were called to participate in the parade, in their opinion it's a lot earlier than expected

...


Any hint which one is from CAC and which from SAC?
 
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