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Technical description
MIG-25 technical specifications:
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Length of an airplane |
22.3 m |
Wing span |
13.9 m |
Maximal take-off weight |
36.2 tons |
Maximal velocity |
2.8 sound speeds |
Altitude of flying |
25 000 m |
Operational acceleration |
+ 4.5 g |
Engines |
2 x R-31 |
Thrust |
2 У 12250 kg |
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MIG-29 technical specifications:
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Length of an airplane |
17.3 m |
Wing span |
11.4 m |
Maximal take-off weight |
17.7 tons |
Maximal velocity |
2.3 sound speeds |
Altitude of flying |
18 000 m |
Operational acceleration |
+ 9 g |
Engines |
2 x RD-33 |
Thrust |
2 У 8300 kg |
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L-39 technical specifications:
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Length of an airplane |
12.13 m |
Wing span |
9.12 m |
Maximal take-off weight |
4700 kg |
Maximal velocity |
760 km/h |
Operational acceleration |
+ 8 g / -4 g |
Engines |
1 x AI-25 |
Thrust |
1 У 1722 kg |
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MiG-31 technical specifications:
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Wing span, m |
1979 |
Length, m |
13.46 |
Height, m |
22.69 |
Take-off weight, kg : |
5.15 |
- normal |
41000 |
- maximum |
46200 |
Engine |
2 TSEA D-Ц0F-6 |
Maximum trust, kN |
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- dry |
2 с 91.00 |
- afterburner |
2 с 152.00 |
Maximum speed, km/h: |
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- in altitude |
3000 (M=2.82) |
- on sea level |
1500 |
- cruising |
2447 (M=2.3) |
Service ceiling, m |
20600 |
Range, km: |
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- without AFT |
2500 |
- with AFT |
3300 |
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SU-30 technical specifications:
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Length of an airplane |
21.9 m |
Wing span |
14.7 m |
Maximal take-off weight |
33 tons |
Maximal velocity |
2.35 sound speeds |
Altitude of flying |
17 680 m |
Operational acceleration |
+ 9 g |
Engines |
2 x юl-31F |
Thrust |
2 У 12500 kg |
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