Calculation of the book “Design of aircraft,” Jaeger. 1983.
Perhaps PAK FA will face even more issues than the F-35?
http://www.ainonline.com/aviation-news/ain-defense-perspective/2013-09-20/various-obstacles-confront-russias-t-50-project
Radar T-50 – N036, the motor T-50 – izd.117.
izd.117S – Su-35 :stupid:
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Dear paralay, why multiply it by 0.35? thank you very much in advance!!
The coefficient is taken on the basis of statistics. Approx.
BARS-130 (aka BARS-light) ?
Written Irbis-E for the Su-35
Darn, no. It was isometic technical drawing.
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I’m inclined to believe MiG still had some legacy (unfinished?) airframes or perhaps kits left, but you never know. Can any of our russian aviation experts with inside knowledge help us here? Paralay? Flateric?
😉
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Yes, you’re right
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What are the advantages/disadvantages of a sliding canopy ???
Placing the aircraft in a hangar with a low ceiling. The Russian aircraft carrier can have double decker hangar height of 5 meters.
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Paralay, brilliant work. Can you please share with us the english version? Also, if possible would love to take a look at the excel file. My email is [email]plamkii@gmail.com[/email]
We are working on an English version. Some lines have already been translated. A reference to the table I have already given in the message: http://paralay.com/paralay_tab.xls
Each aircraft is compared with the Su-27, so they are compared with each other. Controversial technique, but the other is not 😛
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JF-17 has a minimal advantage over the F-18A, F-15 and Gripen. Everyone else he loses.
The bottom line – the “success rate” or “combat power” – and worst of all (19.2). This number is derived from the date of the first flight. The highest value of the Tu-160
http://paralay.com/paralay_tab.xls
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For Gripen, in level flight canard does not create lift. Only J-20, Su-47 and Viggen 😉
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