PeeD
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The F-35B depicted in the picture mostly sacrifices fuel load. 1/3 less than the F-35A, in fact. And you want to have a lot of fuel.
My fuel is at other, better places to allow for one large central weaponbay.
My friend, neither the Yak-130 nor the Super Tucano have radars. The Super Tucano doesn't even have a jet engine, its a turboprop. You want the F-313 to have 2 turbofan engines, a radar, stealth, and sophisticated communications gear, but cost about the same as a Super Tucano?
I wanted to say that if Iran manages to produce a cheap turbofan and a cheap 120km max. track range AESA, it can significantly push down the price, it was not meant for comparison with those two trainers.
I can just tell you that the budget of Irans AIO is given by the state. In contrast to embraer its a non-profit company for Iran. Iran don't by its equipment from private companies.
Hence its a complete different thing.
Why do you think the price difference of a tucano compared to the Yak is just $1m? Does this makes any sense? Now Russia was forces to privatize parts of its aerospace industry. In Iran all is selfmade with no profit margin in the chain.
This is the key to get such prices.
Except because the F-313 will be operating at a low altitude for most of its time, it won't be facing the AWACS frontally, where the RCS is lowest. It will be showing its top, which has a much larger surface area.
No. Its main radar evasive asset would be terrain masking. LO would be just secondary for the pop-up and if something try to hunt it. Infact if designed correctly the 20° aspect to the top aspect RCS could be low enough, remember that the huge underside of the B-2 also has a very low RCS.
Link 16 is standard across all US combat aircraft that have radars, and even in some that don't.
Well if the U.S fleet can shot the AMRAAM with passive data via link-16, good for the Americans, could help. As said the AEW position would be certainly known to Irans IADS and they would operate at stand-off ranges. I have grave doubts about tracking the LO F-313 from 200km+ range with their AEW radars.
The F-313 has less of all of those. Sure, the weight and drag may help, but I think the low thrust especially is a big problem. And the margin of weight is still a matter of discussion because of the size.
To complex for such a judgment.
The Al-222 is 3.1 metres long and the F-135 is 5.6 metres long. Considering some of the F-135 pokes in between the weapons bays, their length behind the weapons bays is about the same.
Though the front fuselage needs to be a bit longer than conventional aircraft since the intake, canard, nose and cockpit are all in that section.
I don't follow you: So you have seen that a non-afterburning low power turbofan is about half the length than the F-135. You also know that there is no intake that act as a barrier nor a landing gear. So whats the problem?