It is not that I know a better one, but how this an undefinined item like “corner of forward edge of wing” or “nozzle rotation angle” is relevant to this comparison??
Do you have a complaint about the methodology or the translation? Or are you sad that I prevented the 400-page flame from growing? 😛
If you have another way to compare planes, introduce us
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MiG-29 – 0.9
Su-27 – 0.76
F-16 – 0.9
F-15 – 0.81
F-35A – 1.42
F-22 – 1.68
The difference is not essential. The ability of a pilot in this system is 0.05 – 0.15
The J-10 is unified in the engine with J-11, so they chose him
Total combat effectiveness:
J-20 – 1.28
J-31 – 1.3
J-10 – 0.85
FC-1 – 0.88
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Su-35S, combat load
4 RVV-MD, 4 x 106 kg = 424 kg. 4 P-72 x 49 kg = 196 kg.
6 RVV-SD, 6 x 190 kg = 1140 kg. AKU-170E 6 x 61 kg = 366 kg.
2 RVV-BD, 2 x 510 kg = 1020 kg. AKU-58AE 2 x 186 kg = 372 kg.
424 kg + 196 kg + 1140 kg + 366 kg + 1020 kg + 372 kg = 3518 kg
4 RVV-MD, 4 x 106 kg = 424 kg. 4 P-72 x 49 kg = 196 kg.
4 RVV-SD, 4 x 190 kg = 760 kg. AKU-170E 4 x 61 kg = 244 kg.
4 RVV-BD, 4 x 510 kg = 2040 kg. AKU-58AE 4 x 186 kg = 744 kg. distance of 200 km / 300 km, warhead. 60 kg.
424 kg + 196 kg + 760 kg + 244 kg + 2040 kg + 744 kg = 4408 kg
Take-off weight in this configuration
19300 (empty) + 100 kg (pilot) + 11500 kg (fuel) + 4408 kg (load) = 35308 kg
Flight distance in this configuration with a load of 3300 km.
RCS in this configuration.
RCS min. = 2.5 sq.m.
RCS = (2.5 m + 12 m) * 0.5 = 7.25 sq.m.
weight empty (Su-30MKK) 24900 – 570 (weapons) – 5270 (fuel) – 200 (pilots) = 18860 kg (equipped with pylons), normal – 24900 kg
weight empty (Su-30MKI) 25700 – 570 (weapons) – 5270 (fuel) – 200 (pilots) = 19660 kg (equipped with pylons), normal – 25700 kg
the maximum weight – 38800 kg (weapons 8000 kg + 100% of fuel)
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Su-35S weght empty 19300 kg
2хР-27 + 2хР-73 + 1хПТБ-1500 (without discharge) -1380 km / 1 hour 38 min.
air to air 1380 km * 0.35 = 483 km or 300 mies
2xFAB-250 + 2хР-73 + 1хПТБ-1500 (without discharge)
air to surface (1380 km – 5%) : 2 = (1380 km – 69 km) : 2 = 656 km or 408 miles
5% – aero-navigational fuel stock
manual
on the ground (Н = 200м, М = 0,5) – 710 km
-H = 12000m … 13000m M = 0.8, without tank – 1 430 km
Without weapons and external tanks – 1250 km / 1h.22 min.
2хР-27 + 4хР – 73 – 900 km / 1 hour 10 min
2хР-27 + 2хР-73 + 1хПТБ-1500 (without discharge) -1380 km / 1 hour 38 min.
the maximum – 2,230 km / 2 hours 42 min
MiG-29A, range without weapons
without external tanks (3240 kg) – 1200 km, combat radius A2A <420 km, A2S <570 km
1 PTB-1500, (1160 kg + 3240 = 4400 kg) – 1530 km, combat radius A2A <536 km, A2S <727 km
MiG-29 +
2 PTB – 1150, (955 * 2 = 1910 kg + 3240 = 5150 kg) – 1800 km, combat radius A2A < 630 km, A2S < 855 km
3 PTB (1160 + 1910 + 3240 = 6310 kg) – 2100 km, combat radius A2A < 735 km, A2S < 998 km
This engine NK-65 for PAK DA (there are doubts in the title)
AL-41F (izd.20) – a large engine, for a fighter weighing 39 – 42 tons.
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