
History:
The Yak-141 (formerly known as
Yak-41) was originally developed to replace the Yak-38 for air
defence missions aboard the Kiev class carriers/cruisers. These
carrier-borne operations are air interception, close air combat
and also maritime and ground attacks. The development of the Yak
began in 1975, but the prototype did not fly until March 1989.
Four prototypes were used for flight testing until 1995. The Yak
is a V/STOL (Vertical/Short Take-Off and Landing) airplane, similar
to the British Hawker Harrier. The Yak-141 uses the common Soviet
V/STOL principle which combines lifts and propulsion jets. Two
fuselage mounted lift jets in tandem are mounted behind the cockpit
for vertical lift while the cruise power is provided by a single
Tumansky R-79 jet engine with afterburning capability for conventional
take-off. The Yak is equipped with a digital fly-by-wire system
and uses the same multi-mode radar as the MiG-29. The airframe
is made of composites materials and aluminum lithium alloys.
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Function: |
V/STOL aircraft for air interception,
close air combat and maritime and ground attacks |
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Dimensions (wingspan/length/height): |
10.1 m / 18.4 m / 5.0 m |
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Weight: |
11,650 kg empty (15,800kg
VTO max. take-off weight and19,500kg STO max. take-off weight) |
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Engines: |
1 Kobchenko/Soyuz
R-79-300 vectored-thrust lift/cruise turbofan + 2 Rybinsk RD-
41 turbofan lift engines |
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Cruising speed: |
1,250 km/h |
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Max. speed: |
1,800 km/h |
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Range: |
650 km |
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Ceiling: |
+15,000 m |
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Vertical climb rate: |
250 m/s |
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Armament: |
1 x 30mm cannon with 250 rounds |
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(combination of:) |
AA-10 Alamo radar-guided medium-range
AAM |
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AA-11 Archer shortrange IR-guided
missile |
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different bombs or unguided
rockets |
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Crew: |
1 |
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Manufacturer: |
Yakovlev; Russia |