All F-16s will undergo Özgür and the structural upgrade. None will be retired from 2035.replacement for the F16 starting from the 2035
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All F-16s will undergo Özgür and the structural upgrade. None will be retired from 2035.replacement for the F16 starting from the 2035
Imho when our Ramjet powered BVR missiles enter serial production, we only need platforms which can launch them, also powerful Radars and EW systems. As a launch platform we only have to mass produce supersonic capable UCAVs and some MUM-T capable manned Jets. I still want to see an unmanned AEW.IMHO, the size of the Air Force's combat fleet should be large enough to avoid ceding air superiority in contested theaters to the opposing side while fighting on two fronts(you know which fronts) simultaneously. Therefore, we need all types of combatant jets: F-16s, EFs, KAANs, even Hurjets... On the unmanned side, if TEI can successfully bring the TF6000/10000 project to mass production, then with the Kızılelma variants and Anka variants, as whole picture we need to create not only qualitative parity but also quantitative superiority, even in a 1:2 situation. Not only these, also saturation/RF decoy/jaming drones in hundreds like Super Şimşeks... Things are heating up, and the Air Force, in particular, needs to take significant steps in both training and procurement planning. Without underestimating any local capacity, I believe we need everything. Everything we can use!
I guess that would be Akıncı with Fulmar 500, Antidot 2 electronic support pod to listen for radar and Aselflir-600 from the current stock and whatever Aselsan might come up with later on.I still want to see an unmanned AEW.
To me Fulmar 500 is optimized for Air-to-Ground operations. Air-to-Air is listed but they don't emphasize it much.I guess that would be Akıncı with Fulmar 500, Antidot 2 electronic support pod to listen for radar and Aselflir-600 from the current stock and whatever Aselsan might come up with later on.
i think with air to air function they meant locating low flying kamikaze drones and maybe cruise missilesTo me Fulmar 500 is optimized for Air-to-Ground operations. Air-to-Air is listed but they don't emphasize it much.
FULMAR 500-A
The FULMAR 500-A System is a multi-function Active Electronically Scanned Array (AESA) reconnaissance and surveillance radar system integrated into UAVs and manned reconnaissance aircraft. It features sea search, detection/tracking of surface/air/land targets to create a comprehensive surface picture, as well as surface ISAR imaging and terrestrial SAR imaging functions.
The FULMAR 500-A System possesses the advanced features listed below and has been developed to meet the day/night and all-weather operational requirements of Naval Forces.
More importantly it should have bigger IWB to accommodate larger missiles like Som-j. The larger wing area together with the prospective higher output thrust from TF6000 will give higher performance to the plane and the indigenous engine’s inherent stealthy structure would help with the low observability of the aircraft as a whole.So Anka 3 will now be able to carry 1600kg, they also increased the wingspan and the length. Hopefully that extra meter of length means they're finally covering the nozzle.
There are changes in the new brochure for the Tusaş ANKA III Unmanned Aerial Vehicle System:
Length: 8.9 m (previously 7.9 m)
Wingspan: 13.1 m (previously 12.5 m)
Height: 2.6 m (previously 2.5 m)
Take-off weight: 7,250 kg (previously 6,500 kg)
Payload: 1,600 kg (previously 1,200 kg)
Average Turkish consistency
Can it at least carry HGK 83 then?The increase in the aircraft's MTOW appears to have increased both structural and fuel weight. In addition to the structural weight increase resulting from the dimensional growth, we can estimate that approximately 100-150 kg of this increase has gone towards additional fuel capacity thanks to the expanded wing and fuselage volume.
Most probably, the most critical benefit of the structural growth is the estimated 20-25% increase in the internal weapon bay (IWB) volume. A rough geometric calculation yields a new volume ratio of 1.126 (length) x 1.04 (height) x 1.05 (width) = 1.23. While this is an optimistic estimate, it's certain that the weapon bay directly benefits from this growth. A 23% increase in IWB volume may have brought the ammunition length that can fit inside the bay to the critical threshold of 3.8-4.0 meters. Also onsidering that the payload capacity of each station within the IWB was 650 kg in the old specifications, we can talk about a maximum ammunition carrying capacity of 900 kg in the new structure, ideally around 750-800 kg. This increase represents a very critical geometric transformation that can roughly double the destructive power of ANKA-3 on the target in its full stealth mission profile.