Chinese Loyal Wingman (sensor, A2A and A2G) UAV/UCAV thread

Deino

Lieutenant General
Staff member
Super Moderator
Registered Member
There don't seem to have any visible cutouts on the UAV's rear section that would allow the angled vertical stabilizer pair to fold down and fit into the fuselage's streamlined shape of the UAV, which is quite different to the foldable tail design seen on some of the H-20 illustrations so far.

View attachment 127210

But it is also possible that this UAV is just one of the scaled test models that are used for, among others, verifying the viability of having such tail design (in one of the two/folded-up configurations) on the H-20 and/or other U(C)AVs of similar design.

So truth to be told, I'm not exactly sure.

exactly my thought too … otherwise it is 11m long, has a 18m span - if it is a UCAV it could be a full scale model.
 

ACuriousPLAFan

Colonel
Registered Member
GJ-11 likely spotted again, this time at Gaobeidian in Hebei.


View attachment 127208

Big Bun on Weibo put that flying wing U(C)AV beside an F-117 for comparison.

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Hopefully those tail fins can be eliminated/made to fold-down for the final service model (if any).
 

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ougoah

Brigadier
Registered Member
Looks more like H-20 mockup, scaled model, or RCS test rig? Looks exactly like the H-20 renderings and location of canted control surfaces.

Definitely not a GJ-11. GJ-11 has single wing sweep angle and has long been in service with PLA and from memory, its operational use has been talked about by the PLA since 2020. Unless this is some GJ-11A model that's basically changed the entire design of the UCAV, it is clearly a model of another program.
 

by78

General
More illustrations of various UCAV designs from several research papers, none of which I have access to.


Single-engine flying wing:
53632769802_ebd2cef66c_o.jpg


Twin-engine flying wing:
53633999244_fdfb5aab54_o.jpg
53633874988_646b5d8b47_b.jpg



Active aerodynamic control by diverting a portion of the exhaust to a control surface:
53634105190_cffa718769_o.jpg



High subsonic UCAV:
53633999419_9ce35d97c0_h.jpg
 
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