| Specifications
|
|---|
| Prime contractor | MiG-MAPO
|
| Country of origin | Russia
|
| Function | Multi-role fighter
|
| First Flight | February 7, 2007
|
| In-service year | 2019
|
| Unit cost | US$40 million ???
|
| Use of designations in other projects |
At various times, the designation "MiG-35" was used in the title:
Project multipurpose fighter of the fifth generation MiG 1.44 ;
further development of the project MiG-29M2 second half of the 1990s (they MiG-29M3 and MiG-29M4 );
demonstrators test radar " Zhuk-A " (opytnyx copies of the MiG-29M , MiG-29K , MiG-29KUB )
project on the Indian Competition MMRCA (Eng.) Russian. ;
development project of aircraft MiG-29K / KUB for the Navy and MiG-29M / M2 for the Russian Air Force; Single version labeled as the MiG-35, two-seater version is designated MiG-35D.
|
| differences MiG-35 from the MiG-29 |
Radar " Zhuk-A " with an active electronically scanned array ;
increase payload;
increased fuel with possibility of in-flight refueling tanker and use like;
corrosion protection by type of MiG-29K;
lowering of radar visibility;
three-channel FBWCS with fourfold redundancy;
increased reliability, service life, and the life of the aircraft engines;
reducing the cost of flight hours is 2.5 times;
an increase in the autonomous-based features (such as kislorododobyvayuschaya station on board);
new electronic engine management system of the RD-33MK ;
the possibility of using the RD-33MK versions with thrust vectoring, tried and tested at the pilot of the MiG-29M OVT;
built container and optical location station (OLS) and helmet-mounted target designation system and sighting;
defense system with electronic warfare means, detectors attacking missiles and laser irradiation, guns ejection of decoys;
open architecture avionics .
|
| Length | 17.32 m
|
| Wing Span | 12 m
|
| Wing area | 42 m²
|
| Height | 4.44 m
|
| Mass |
|
| empty | 13,500 kg
|
| normal take-off weight | 18,500 kg
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| maximum take-off weight | 29,700 kg
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| Engine |
|
| Engine type | Turbojet dual circuit with afterburner
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| Model | RD-33MK or its modification with UHT RD-33MKV with
all-view thrust vector deviation (within + - 20 °).
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| Maximum Thrust | 2 × 9000 kgf
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| Flight performance |
|
| Maximum speed |
|
| at height | 2560 km / h
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| at land | 1450 km / h [25]
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| Practical ceiling | 17,500 m
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| Range with normal combat load | 1000 km
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| Flight range without refueling | with PTB 3,500 km
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| Maximum operating overload | +10 G
|
| Armament |
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| Cannon | 30 mm aircraft gun GSH-30-1
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| Weapon suspension units | 9
|
| Suspended weapons weight | 6 tons
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| Suspended armament | all types of guided and unguided
air-to-air and air-to-surface munitions
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| Crew | 1 or 2 people [D & UB models]
|
