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History
MiG-35 was firstly introduced to the public at ¡°Aero India-2007¡± international air show.
Manufacture of MiG-35 is to be organized on the ¡°Sokol¡± plant in Nizhny Novgorod in 2009-2010.
MiG-35D – two-seat version
Main Characteristics | |
Length, m |
17,3 |
Height, m |
4,5 |
Wingspan, m |
11,99 |
Weight, kg: |
|
nominal |
17500 |
maximal |
23500 |
Landing maximal |
16800 |
Max load |
6500 |
fuel |
4800 |
Max Speed, km/h: |
|
at low altitude |
1400 |
at high altitude |
2100 |
Operating Ceiling, m |
17500 |
Operating Acceleration, g |
9 |
Flying Range, km: |
|
without External Fuel Tanks |
2000 |
with 3 External Fuel Tanks |
3000 |
with 3 External Fuel Tanks and refueling in the middle of the distance |
6000 |
Crew, members |
1 |
Power Unit | |
Engines |
RD-33MK |
Thrust, kgf: |
|
at full augmented power |
9000 |
at full power without augmenting |
5400 |
Length, mm |
4229 |
Diameter, mm |
1040 |
Dry weight, kg |
1055 |
Service Life Limit, h |
4000 |
Overhaul Period, h |
1000 |
Weapons | |
Gun |
GSh-30-1 |
Caliber, mm |
30 |
Ammunition, shells |
100 |
Suspended weapon |
¡°air-to-air¡± missiles R-27, RVV-AE, anti-ship missiles XX-31A and X-35, ¡°air-to surface¡± missiles X-31P, X-25ML, X-29T, X-29L, unguided missiles, correctable and free-fall aerial bombs, air mines |
....
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