Hello all,
The consensus here seems to be that the diamond -shaped CCA (Type E) is a mockup, but I would like to discuss what the evidence is, for or against. On the image above, rivets are visible along the front and bottom edge of the vertical stabilizers, and three rivets are visible on the outer tip of the main wing. There are also visible gaps for the panel with a cross (+) symbol below the intake, and a pitot tube on the nose.
I cannot see any discontinuity for the radome near the nose. The front landing gear does not seem to me to leave very much room for a radar system in this planform. It is quite strange to me what the role of this platform is if it does not have a radar sensing capability. Perhaps a purely strike platform, intended to be cued by other network nodes, but we have not yet seen a IWB. But maybe there is some innovative solution, relying on other sensors or conformal antennae (receiver-only radar?). Or maybe that a distinct radome is not necessary, because the entire aircraft is housed in composite (with any RAM material underneath).
The wing control surfaces appear to have actuator housings, although none are present on the rudder. It's possible the rudder uses electrical actuators like on the F-35. The main landing gear appears to have intact wiring for the brake system. I know the exhaust was a point of contention, but perhaps the engine is non-afterburning, so heat resistant materials are not necessary.
Are these details typical for mockups? I am not familiar with how these mockups are made. I wonder what you all think.
Regards
