https://aviationweek.com/defense/ai...ator-progresses-critical-gcap-de-risk-efforts
Frames for each fuselage section have been aligned on jigs with the center fuselage section arguably the most revealing, showing two deep internal weapons bays positioned ahead of the main landing gear. Their size suggests the demonstrator could potentially carry around twice the internal weapons volume of the F-35's relatively shallow bays, and potentially could be capable of accommodating larger-diameter stores.
Where the landing gear will be fitted, faceted edges have been added to the frames to reduce the radar cross-section of where the gear doors will be fitted.
Individual ducts for the two Eurojet EJ200 engines wrap over the weapons bays and run almost the full length of the center fuselage, explaining the unusually shaped intake ducting displayed previously. It remains unclear whether the ducts stay parallel all the way to the rear of the aircraft or whether the engines are widely spaced, as journalists were not shown the aft section of the rear fuselage. The demonstrator will also feature modified engine nozzles rather than the standard Eurofighter Typhoon installation, Aviation Week has been told.
The intake-fuselage junction is manufactured as a single component using hot isostatic pressing (HIP), a process that BAE engineers said would not have been possible using conventional manufacturing techniques. The same process has also been used to produce titanium actuator cradles for the aircraft's large trailing-edge control surfaces.
Based on what was shown, the demonstrator appears to be at least one-third longer than the Eurofighter, as Aviation Week has previously reported, making it the largest aircraft assembled in the UK since the Nimrod MRA4. The production GCAP fighter is expected to be larger still.