
History:
The first flight of the Su-37
prototype was in April 1996 at the Zhukovsky flight testing center
near Moscow. The aircraft demonstrated new manoeuvres, such as
the 'Cobra-manoeuver' where the nose is pointed upwards and away
from the flight direction for longer periods or rotating the nose
through 360 degrees and recovering from a tail slide by rolling
into a completely different position. This single-seat all-weather
multi-role aircraft derived from the SU-27 and has an updated
airframe which contains a high proportion of carbon-fibre and
aluminium-lithium alloys. The engines, avionics and armaments
have also been updated to those installed in the SU-27.
The most impressive feature of the high-manoeuvrable Su-37 fighter
are the thrust vector control engines, which gives the aircraft
the ability to recover from spins and stalls at almost any altitude.
The pilot has a side short-travel control stick instead of a central
stick and the aircraft is equipped with full digital fly-by-wire
controls. The Su-37 has a all-weather radar which is configured
for simultaneous surveillance of airspace and the ground and a
high-precision laser-inertial/satellite navigation system. This
multifunctional, forward-looking Doppler radar can track up to
15 targets simultaneously. The Su-37 is also fitted with a rearward
facing radar in the tail stinger area of the fuselage. The engines
provide each 83.36kN thrust (142kN with afterburner) and are steerable
up and down from -15 to +15 degrees. The thrust vector control
is integrated into the digital flight control system which can
be operated manually by the pilot or automatically by the flight
control system. There are twelve external hardpoints under the
wings which can carry air-to-air missiles, air-to-surface missiles,
bombs, rockets and an ECM (electronic countermeasures) pod located
in the wing-tips. The aircraft is equipped with one GSh-301 30mm
gun with a maximum rate of fire of 1,500 rounds per minute. The
Su-37 can carry up to 14 air-to-air missiles and additionally
up to 8000kg of ordnance.
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Function: |
All-weather multi-role attack
aircraft |
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Dimensions (wingspan/length/height): |
14.7 m / 22.2 m / 6.43 m |
|
Weight: |
8,500 kg empty; (34,000 kg
max. takeoff weight) |
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Engines: |
2 x Lyulka AL-37FU vectored-thrust
afterburning turbofans |
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Cruising speed: |
1.400 km/h |
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Max. speed: |
2,500 km/h |
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Range: |
3,800 km |
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Maximum climb rate: |
230 m/s |
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Ceiling: |
18,000 m |
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Armament: |
1 x GSh-30-1 30mm cannon |
|
(combination of:) |
R-27, R-40, R-60, R-73A and
R-77 Air to Air missiles |
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|
Kh-25ML, Kh-25MP, Kh-29, Kh-31
and Kh-59 Anti Ship missiles |
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S-25 IR and laser guided rockets |
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GBU-500 and GBU-1500 laser
guided bombs |
|
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GBU-500T and -1500T TV guided
bombs |
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Crew: |
1 |
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Manufacturer: |
Sukhoi; Russia |