Correct errors and add table 😉
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(Gripen A had an RCS of 0,1m2 in official verified documents released by FMV…
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EF-2000 domestic motor + domestic missiles
Rafale domestic motor + domestic missiles
MiG-35 domestic motor + domestic missiles
Gripen foreign motor + foreign missiles
Findings “combat potential” built on the calculation, it not propaganda 😉
Don’t tell me you’re trying to mount that missile on that plane lol! 🙂
It’s okay! 🙂
With such a missile can fly and fly. But it is impossible to sit down, that’s the problem
I painted Russian light fighter with a big cruise missile. Therefore, it was forced to move forward, “the nose landing gear” and the pilot cabin. To the length of the aircraft has not increased, he pushed back the radar.
American aircraft can be done on the classical scheme, with radar in the nose.
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It’s fantastic to see how the Russians underestimate the Gripen. Would come as a nasty surprise if, God forbid, a conflict were to break out.
Prove otherwise 😉
Let me remind you, Gripen lost in the Indian tender
I think I’d make a bomb with at least the equivalent of a mk-83 in terms of firepower. For instance with a more boxy shape than the Mk-80s series. The bomb could be 3.6m long to fit in a bay designed for an AMRAAM.
F119 15876 kgs / 11825 kgs
thrust-to-weight: F-22 1.23, F-35 1.07
15876 kgs : 1.25 = 12700 kg – take-off weight norm.
12700 kg * 1.3 = 16700 kg – take-off weight max.
assembly density, maximum take-off weight F-22 519 kg / m3
volume 16700 kg : 519 kg/m3 = 32.3 m3
relative volume of a compartment of the weapon F-22 10.3%
volume of a compartment of the weapon 32.3 m3 * 10.3% : 100 = 3.33 m3 (F-22 – 6.73 m3)
3.33 m3 : 4 = 0.83 m3 or 0.2 m2 * 4.16 m – one weapon bay
What’s the size of your antennas? They look small
1000 mm x 450 mm
No radar?
you need to be able to carry relatively large bombs.
Radar Antennas on the left and right of the cockpit.
fuselage volume does not allow to keep a bomb in the weapons bay. To increase the volume of the fuselage is required to increase the take-off weight.
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maximum takeoff weight of 20,000 kg
normal takeoff weight of 12,000 kg
the maximum speed of Mach 2.0
cruising speed of Mach 1.3
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Yes, it is not perfect.
You can check and suggest corrections 😉
Given that we’re all posting in English, you might want to translate that or better yet, have a 2nd sheet with links to the 1st but with headers & row descriptions in English.
196 wing angle
197 wing extension
198 wing loading
199 fuselage extension
200 Power steering engine / aircraft weight
201 deviation of the thrust vector
202 followed by a radar target
203 targets simultaneously being attacked
204 points of suspension
205 RCS
206 maximum overload
207 acceleration
208 flight distance
212 top speed
213 cruising speed
214 flight distance
215 Range Radar
216 followed by a radar target
217 targets simultaneously being attacked
219 RCS
220 range missiles “air – air”
223 efficiency / cost
225 generation
No Information F-16E and F-10B
Line 209 – compared to the Su-27 in “dogfight”
Line 221 – compared to the Su-27 in the “long range fight”
Example: MiG-35 in close combat in 1.64 times better than Su-27
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Airframe designed service life in hours: MiG-31: 3,500
Source?
Just to translate a little better (no offense Paralay), what he is referring is real-time health monitoring, versus fixed schedule of maintenance. The same thing that brought the MiG-29SMT 40% cheaper flight hours.
Ok :applause:
However, I suspect you are referring to Su-30M2 (or earlier) Paralay? Not Su-30SM surely.
I was referring to the Su-30MKM
so how did you come up with these numbers?
http://www.paralay.com/paralay_tab.xls
line 194 – 261
Characteristics of the aircraft compared to the Su-27 and Su-24