Re: Su-57 is a misunderstood aircraft

milosh wrote:@ricnunes
Sting is that thing behind engine it was called like that for ages (on Flankers). Sting and pushed back engines make Su-57 quite longer then F-22 is. But I will try when have time (weekend probable) to do size comparison of both.
Not much difference there.
Ok, now I know what you mean with "sting". Anyway, that "sting" isn't stretched much longer compared to the rest of the aircraft (namely engine and horizontal stabs edges) and in the case of the F-22 it's the horizontal stabs that stick out and contribute for its length, so I fail to see you point unless you're again as usual using stupid semantics in order to try to justify your wrong point. And the Su-57 wingspan and wing area continue to be bigger than the F-22.



milosh wrote:Btw expensive titanium isn't really the case. Flankers do have lot of titanium and it wasn't problem but all the sudde cost of titanium would be problem for their pride project?!?
@milosh,
JEEZZZ, you are playing dumb or just being plain dumb??

Of course it's because it's expensive! High performance planes usually use smaller amounts of titanium, namely in the wing edges and other parts where highest strength while keeping the weight to a minimum is required! It's not only the Flankers that use titanium is some parts, many/most other high performance aircraft do as well!
The F-22 using 39% of titanium in its structure is very impressive indeed! And this was done in order to increase the aircraft's strength while keeping its weight the minimal as possible. But this should be one of the reasons why the F-22 is so expensive!
According to the link below the Flanker uses 18% of titanium in its structure, so basically the same as the Su-57:
https://inf.news/en/military/43d3bbf493 ... 40140.html
milosh wrote:Reason to use Al is to reduce weight. Btw USSR did thought of switching toward next gen Al-Li alloys in 1980s but metallurgy wasn't there yet. Then 1990s happened and only in 2000s they could continue work on new alloys.
AGAIN, titanium do increase cost - It's a RARE and HARD TO WORK material! - and since the Russians can hardly procure the Su-57 which have most of its structure built in aluminum, imagine how harder would it be - COST WISE - to procure Su-57 whose structures would be made with a (much) higher % of titanium??
AND AGAIN, titanium has twice the strength of aluminum while weighting only 60% more and THIS MEANS THAT:
1- EITHER, you can build a structure using titanium with the SAME STRENGTH but LIGHTER compared to if it was build using aluminum.
2- OR, you can build the a structure using titanium which would have a BIGGER STRENGTH but have the SAME WEIGHT compared to if it was built using aluminum.
CAPICHE, for Christ sake??



And because of this, there's no way that a production Su-57 weights less than the F-22!
milosh wrote:Btw you have info that Su-57 is better in subsonic acceleration then even Su-35, that say something about Su-57 mass. If it have next gen engine it wouldn't be strange and we could say well it is heavier but engine thrust compensate that. Su-35 last data we go is 19tons, so with 18.5tons and maybe little more powerful engine (new combustion system) Su-57 would have noticeable better acceleration.
But I think we are running in circles while everywhere weight of Su-57 is 18 to 18.5tons I think we need official number to be clear.
Btw interesting info I found about Izd30 engine, it look like have variable bypass ratio so it is more like F120 then F119.
Sorry but I don't speak Garblish and Russian troll/"propagandish"...
