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SU35
Sukhoi Su-35
The Sukhoi Su-35 is a Russian
fighter aircraft.
A derivation of the Su-27 it was originally identified as
the Su-27M. It was develped to better the US F-15 and
F-16, the proposed improvements would greatly enhance its
air combat capabilities and the addition of a proposed
new AAM missile with a 400 km range would render the
craft truly formidable.
Following flight tests from 1988, based on the 1985
experimental T10-24, the first prototype was publically
displayed in 1992 at Farnborough. Flight testing
continued and up to 1994 eleven prototypes were built.
Intended to enter service around 1995, the first test
flights of an improved Su-35, the Su-37, in 1996 and the
transfer of existing Su-35 prototypes to this program
appeared to suggest the end of the Su-35 without any
production aircraft.
It shares much in common with the
naval variant of the Su-27, the Su-33, notably the larger
wings and the more powerful engines. Other changes from
the Su-27 were canards, a larger nose, the greater use of
carbon fibre and aluminium-lithium alloy in the airframe,
and larger, squarer tail fins. The new nose holds an
improved radar and the aircraft had many other upgrades
to its avionics and electronic systems, including digital
fly-by-wire and a rear-radar for firing SARH missiles.
A two-dimensional asymmetric thrust vectoring system was
tested on the Su-35 and seems to be the basis for the
development of the Su-37.
Su-35
length: 22.20 m
span: 15.15 m
weight: 17,500 kg (empty), 33,000 kg (max take-off)
max speed: 2,450 km/h (high altitude), 1,400 km/h (sea
level)
ceiling: 18,000 m
range: 4,000 km
power plant: two 137.30 kN Lyulka AL-35MF turbofans, 137
kN each (proposed, known prototypes use Su-27 Al-31F
engines)
armament: one 30mm cannon, 14 hardpoints, max external
load 8,000 kg
Specifications
|
Country of Origin |
Russia |
Builder |
Sukhoi |
Role |
|
Armament |
Su-34
1 GSh-30-1 30mm cannon with 150 rounds
R-27/R-73 AAMs
Kh-29T/Kh-31P/Kh-59M ASMs
bombs, rockets, drop tanks
ECM pods
carried on twelve external points Su-37
1 x 30 mm gun: GSh-301 (150 rnds)
14 x Air-to-Air missiles: AA-10, AA-11,
AA-12
|
Cost |
approximately $35 million |
User Countries |
|
|
Su-33 |
Su-30M |
Su-30MKI |
Su-34 |
Su-35 |
Su-37 |
Crew |
2 |
2 |
2 |
2 |
1 |
1 |
Dimensions, m
Wing Span
Length
Height |
7.4 + 14.70
21.94
5.93 |
14.70
21.94
6.36 |
14.70
21.94
6.36 |
14.70
23.34
6.36 |
14.70
22.20
6.43 |
14.70
22.20
6.43 |
Wing Area, m2 |
62 |
62.04 |
62.04 |
62 |
62 |
62 |
Weights, kg
empty
Normal
Maximum |
-
-
30,000 |
-
24,000
33,500 |
17,700
25,670
34,000 |
-
39,000
45,000 |
18,400
25,700
34,000 |
18,500
25,670
34,000 |
Payload, kg
Maximum
Normal |
6,500
1,400 |
8,000
1,400 |
8,000
1,400 |
8,000
1,400 |
8,000
1,400 |
8,000
1,400 |
Fuel, kg
Maximum
Normal |
-
- |
5,090
9,400 |
5,090
9,400 |
-
12,100 |
11,000
13,400 |
11,000
13,400 |
Engine |
2 Lyulka AL-31
afterburning turbofans |
2 Lyulka AL-31
afterburning turbofans |
2 Lyulka AL-31
afterburning turbofans |
2 Lyulka AL-31MF
afterburning turbofans, 27,557 lb thrust each |
2 Lyulka AL-37F
afterburning turbofans |
2 Lyulka AL-37FU
afterburning turbofans |
Speed, km/h
Cruise
Maximum
[at 10 000 m] |
1,400
2,300 |
1,380
2,125 |
1,380
2,125 |
1,300
1,900 |
1,400
2,500 |
1,400
2,400 |
Maximum Speed, Mach |
2.17 |
2.3 |
2.3 |
1.8 |
2.3 |
2.3 |
Rate of Climb, m/s |
230 |
230 |
230 |
- |
230 |
230 |
Ceiling, m |
17,000 |
17,500 |
- |
14,000 |
18,000 |
18,000 |
Operating Range, km
Normal
Maximum
Ferry
Low Altitude |
3000
-
-
- |
3000
5200
6990
- |
3000
5200
6990
- |
4000 (4500)
7000
-
600 (1300) |
3200
6500
-
- |
3200
6500
-
- |
Takeoff Distance, m |
- |
550 |
550 |
1260 |
- |
- |
Landing distance, m |
- |
670 |
670 |
1100 (950) |
- |
- |
Maximum Turn, g |
+8 |
+9 |
+9 |
+7 |
+10 |
+9 |
Text is available under
the terms of the GNU Free Documentation License
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