Каталог - Оружие России 2000 c82-795

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301

PART 2  2

FIGHTER-BOMBERS -

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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2W_2 Xa`b2761\, 7\b2, _b3 -21w3, 11300

Basic Characteristics

Crew 1

Takeoff weight, kg:

normal 16,400

maximum 19,500

Normal/maximum combat load, kg 1,000/4,250

Maximum operational g-load, g 7

Maximum flight speed, km/h:

near ground 1,250

at altitude 1,850

Service ceiling, m 14,700

Near-ground tactical radius, km 330

Overall dimensions (length x height x wing span), m 19 x 4.97 x 10/13.7

Engine type and thrust, kgf AL-21F3, 11,300

- R-60 and R-60M air-to-air missiles;

- S-24, S-25, S-8M and S-5 unguided rockets;

- aerial bombs, cluster bombs, submunitions dis-

pensers and incendiary tanks of up to 500 kg;

- two NR-30 built-in 30mm guns with ammunition load

of 160 rounds;

- two 23mm SPPU-22 twin-barrel gun pods with

ammunition load of 260 rounds per gun to deliver fire

to the forward and aft hemispheres.

The aircraft can carry up to four PTB-800 and up to

two PTB-1150 external fuel tanks.

The aircraft design features and the PrNK-54 aiming

and navigation complex peculiarities make it possible

to modernize the Su-17M4 to enhance its strike capa-

bility.

The Su-17M4 aircraft can be based on second-

category airfields.

The export version of the Su-17M4 is designated

Su-22M4, which differs from the Su-17M4 only in the

components of individual avionics units and in the IFF

system.

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302

PART 2  2

RECONNAISSANCE-STRIKE

AIRCRAFTS

-



GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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12344 1510 3562789

Su-32MF RECONNAISSANCE-STRIKE AIRCRAFT

The Su-32MF reconnaissance/strike aircraft is desig-

ned to search for and defeat enemy surface ships and

submarines at significant ranges from the home air-

field. The aircraft is able to cover a maritime econom-

ic zone of coastal states against naval and air attack

weapons by day and night, in adverse weather condi-

tions and electronic countermeasures environment.

The Su-32MF, much like the Su-27 aircraft, is

designed around an integrated conventional aerody-

namic configuration with a canard and an adaptive

wing. The wing leading and trailing edges, as well as

the canard, are controlled by an electric remote-con-

trol system with due regard for an angle of attack and

g-load.

The tail portion of the fuselage, far extended to the

rear, accommodates a magnetometer.

The aircraft is equipped with an in-flight refueling sys-

tem provided with an extendible refueling boom.

The aircraft is provided with a welded armored cabin

equipped with the K-36DM pilot’s and navigator-

operator’s ejection seats arranged side-by-side. The

ejection seats enable the crew to abandon the air-

craft in all flying modes, including zero-altitude/zero-

speed escape. If required, the crewmembers can

leave their seats and stand upright.

The aircraft is equipped with an onboard avionics com-

plex that facilitates the execution of combat missions

involving antisubmarine warfare with a high degree of

automation and using data obtained from both onboard

systems and other means, including space-based

ones, over the entire range of operating conditions.

The complex operates mainly in the automatic mode,

with the operator only tracking processed and dis-

played data until the moment a decision is made to

select one of options offered by an intellectual crew

assistance system.

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303

PART 2  2

RECONNAISSANCE-STRIKE

AIRCRAFTS

-



GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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12344 1510 3562789

The onboard avionics complex comprises:

- a radar system that functions jointly with a sonar;

hydroacoustic buoys, including passive directional

ones, operating in the acoustic and infrasonic frequen-

cy ranges, and active directional buoys; as well as blast

munitions;

- a magnetic anomaly transducer that detects distortion

of the Earth’s magnetic field caused by the ferromag-

netic body of a submarine;

- an IR/TV system with two independent data acquisi-

tion channels: TV (optical) and infrared, which are used

separately or jointly, depending on the weather condi-

tions and time of the day.

The aircraft weaponry is suspended from 12 hardpoints

and comprises:

- ASM-MSS and ASM-MS antiship missiles with an

operating range of up to 250 km;

- ASM-M and ASM-M2 antiship missiles with an oper-

ating range of up to 70 and 180 km, respectively;

- AGM-TVC TV/command-guided antiship missiles;

- torpedoes;

- hydroacoustic buoys;

- R-73 and RVV-AE air-to-air missiles;

- guided aerial bombs.

The export versions of the aircraft may be fitted out

with foreign-made equipment. In this case, the sonar

system and software are modified and adapted to

operate with hydroacoustic buoys used abroad.

The Su-32MF reconnaissance/strike aircraft has no

rival in the world and has good export potential.

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Basic Characteristics

Crew 2

Weight, kg:

normal/maximum takeoff 42,000/44,360

combat load 8,000

Maximum flight speed:

at low altitude, km/h 1,400

at high altitude, Mach number 1.8

Flight range, km:

without in-flight refueling 4,000

with in-flight refueling 7,000

Engine type, number x thrust, kgf AL-31F, 2 x 12,500

304

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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'()** 1510 )+,(-./

Su-27SK FIGHTER

The Su-27SK fighter is intended to defeat aerial tar-

gets in free airspace and against earth background,

by day and night, in VFR and IFR weather conditions,

as well as in the active and passive jamming environ-

ment, and also to control airspace, block enemy air-

fields at a great depth and engage ground (surface)

targets.

The Su-27SK is designed around an integrated con-

ventional aerodynamic configuration with a lifting fuse-

lage, which makes it possible to achieve high aerody-

namic lift and efficiency of air combat. At subsonic

speeds, the Su-27SK is statically unstable in the lon-

gitudinal-control channel that decreases trim losses.

The required stability and controllability characteristics

are assured by a quadruple-redundant remote control

system.

The avionics of the Su-27SK comprises a powerful

pulse-Doppler radar, an optronic aiming system, a

flight control and navigation complex, electronic and

optronic countermeasures equipment and communica-

tions facilities.

The surveillance/aiming equipment, which is part of the

weapon control system, assures radar-aided automatic

all-aspect detection and tracking of up to ten aerial tar-

gets in free airspace at ranges of up to 120 km and

against earth background. The optronic aiming system,

comprising an infrared radar and a laser rangefinder,

features a high-altitude effective range comparable

with that of the airborne radar.

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305

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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'()** 1510 )+,(-./

The airborne radar operates in conjunction with the

optronic aiming system that markedly improves target

detection probability and target tracking reliability,

especially in the ECM environment.

The head-up display and the helmet-mounted target

designator provide virtually instant inputs into the mis-

sile homing heads. The electronic and optronic coun-

termeasures equipment makes it possible to detect a

radiating source and determine its coordinates, classi-

fy the threat type and select the right countermeasures

to jam the direction, range and speed channels and fire

infrared and chaff decoys.

The Su-27SK weaponry is arranged at ten hardpoints

and comprises:

- up to six R-27E air-to-air missiles with semi-active

radar and infrared homing heads;

- up to six R-73E short-range missiles.

To defeat ground targets, the aircraft can carry aerial

bombs of up to 500 kg, clusters, and unguided rock-

ets. The fighter is equipped with the GSh-301 built-in

gun with an ammunition load of 150 rounds.

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m)GZ) HPN[).-(L, Z,(-P, R .L[), Z[* q-31r, 2 R 12500

Basic Characteristics

Crew 1

Maximum takeoff weight, kg 33,000

Combat load, kg 8,000

Maximum flight speed, km/h:

near ground 1,400

at high altitude M=2.35

Service ceiling, m 18,500

Ferry range, km 3,700

Normal operational g-load, g 9

Engine type, number x thrust, kgf AL-31F, 2 x 12,500

306

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

" #$ ! " %##$

'()** 1510 )+,(-./

Su-30MK (Su-30KI) MULTIROLE FIGHTER

The Su-30MK multirole aircraft is intended to defeat

aerial targets by modern long-, medium- and short-

range guided and unguided weapons and engage

ground/sea targets by using a wide range of unguided

and guided weapons, including high-precision ones, in

the daytime and at night, in VFR and IFR weather con-

ditions.

The enhancement of Su-30MK aircraft combat capabili-

ties is mainly achieved due to upgraded avionics and use

of new weapons to defeat aerial and ground targets.

The upgraded radar and optronic aiming systems, hel-

met-mounted target designator, flight control/naviga-

tion complex and display system enable the crew to

employ the R-73, R-27 and RVV-AE short-, medium-

and long-range air-to-air missiles and guided weapons

to engage ground targets: Kh-29T short-range, Kh-31P

antiradar and Kh-59M medium-range missiles, as well

as KAB-500Kr and KAB-1500 guided aerial bombs.

To use TV/command-guided and passive radar-homing

missiles, the aircraft is equipped with weapon control

system pods.

Unguided aerial bombs, bomb clusters, incendiary

tanks, submunition dispensers and airborne unguided

rockets with a total weight of 8,000 kg can be arranged

at 12 hardpoints.

Technical parameters, tactical situation and crew action

monitoring and recording built-in facilities ensure

ground and in-flight testing of the airborne equipment,

as well as logical data processing, documentation and

display of information about faults and troubles.

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307

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

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Basic Characteristics

Crew 1

Maximum weight, kg:

takeoff 34,000

combat load 8,000

Maximum near-ground flight speed, km/h 1,400

Maximum Mach number 2.3

Service ceiling, m 17,500

Maximum operational g-load, g 9

Operational range, km:

without in-flight refueling 3,000

with in-flight refueling 5,200

Overall dimensions

(length x height x wing span), m 21.9 x 6.4 x 14.7

Engine type, number x thrust, kgf AL-31F, 2 x 12,500

Ground servicing of the aircraft can be carried out

with the use of Western-standard ground servicing

equipment.

The Su-30MK is a foreign customer-oriented aircraft. In

terms of its design, it is largely standardized with the

Su-27SK and Su-35 aircraft.

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.)+R T-27' R T-35.

308

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

" #$ ! " %##$

'()** 1510 )+,(-./

Su-35 (Su-37) MULTIPURPOSE FIGHTER

The Su-35 (Su-37) multipurpose fighter is intended to

defeat existing and prospective aerial targets, remote-

ly piloted vehicles, cruise missiles and other maneuver-

able targets against earth background, in the daytime

and at night, in VFR and IFR weather conditions, and

also to destroy ground/waterborne targets by deliver-

ing standoff attacks with diverse guided weapons,

including high-precision ones.

The Su-35 is a heavily modernized version of the Su-27

aircraft to significantly enhance its combat effective-

ness against aerial, ground and sea targets.

For better agility and takeoff/landing performance, the

aircraft is provided with a canard. In terms of its aero-

dynamic configuration, the Su-35 is an unstable triplane

(wing + horizontal tail + canard). The required stability

and controllability characteristics are assured through a

quadruple-redundant digital-analog remote control sys-

tem. The Su-35 is equipped with a newly developed

wing featuring an increased relative thickness. The main

landing gear struts are modified and the nose leg is

replaced with a reinforced two-wheel strut. The aircraft

is equipped with an in-flight refueling system. The KD-

36DM ejection seat back is inclined at 30°, which helps

the pilot withstand high g-loads during air combat.

The Su-35 is equipped with an integrated aiming and

navigation system comprising:

- new-generation multifunction multimode phased-

array radar able to detect and track up to 20 aerial tar-

gets and simultaneously engage eight of them;

- optical locator which combines functions of an infrared

imager, laser range finder and target illuminator;

- rearward-looking radar;

- helmet-mounted target designator;

- electronic reconnaissance and defense systems;

- integrated data system;

- communications facilities and flight control and navi-

gation equipment.

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309

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

 15  ! !

" #$ ! " %##$

'()** 1510 )+,(-./

Once the automatic flight control system receives infor-

mation from the integrated aiming and navigation sys-

tem, it solves problems associated with en-route flight,

return to the landing airfield, performing a prelanding

maneuver and landing approach, as well as directing

the aircraft to a target and delivering an attack.

To penetrate enemy air defenses, the Su-35 can fly at

low altitudes using an automatic terrain-following flight

mode.

The Su-35 weaponry is arranged at 12 hardpoints and

comprises:

- RVV-AE, R-27R1, R-27ER1, R-27T1, R-27ET1 and

R-73E air-to-air missiles;

- Kh-31A, Kh-31P, Kh-29L, Kh-29T and Kh-59M air-to-

surface missiles;

- unguided and guided aerial bombs and incendiary

tanks of various size and purpose. The aircraft is also

equipped with the GSh-301 built-in gun with an ammu-

nition load of 150 rounds.

A great variety of its armament versions, sophisticated

equipment and high performance characteristics allow

the Su-35 to fly the most diverse tactical missions.

A further development of the Su-35 is a Su-37, the

newest superagile fighter powered by the AL-31FP

engines provided with a thrust vector control system inte-

grated with the remote control system. This enables the

pilot to fly maneuvers at low speeds down to near-zero

values without angle-of-

attack limitations.

The cockpit is equipped

with a side aircraft con-

trol stick and engine

control levers with a

strain sensitive system

responding to the pilot’s

hand pressure.

The Su-37’s cockpit

indication system is

built around wide-

scope color displays.

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Basic Characteristics

Crew 1

Maximum weight, kg:

takeoff over 34,000

combat load 8,000

Maximum flight speed, km/h:

near ground 1,400

at high altitude corresponds to M=2.35

Service ceiling, m 18,000

Maximum operational g-load, g 9

Flight range, km:

without in-flight refueling 3,300

with in-flight refueling 6,500

Overall dimensions

(length x height x wing span), m 22.2 x 6.4 x 14.7

Engine type, number x thrust, kgf AL-31F(FP), 2 x 12,500

310

PART 2  2

FIGHTERS 

GROUP 15 AIRCRAFT AND AIRFRAME

STRUCTURAL COMPONENTS

Class 1510 Aircraft, Fixed Wing

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MiG-29 FRONT-LINE FIGHTER

The MiG-29 front-line fighter is designed to destroy air

targets in the daytime and at night in VFR and IFR weath-

er conditions and jamming environment and defeat

ground (surface) targets in visual flight conditions.

The fighter is equipped with a two-channel engage-

ment radar system, comprising:

- N-019 airborne radar;

- optical locator intended to search, detect, lock on and

automatically track air targets. The optical locator com-

prises an infrared search/track sensor, a laser

rangefinder and a helmet-mounted target designator.

The information and algorithmic integration of the air-

borne radar with the optical locator into a unified sys-

tem enhanced the jamming immunity of the engage-

ment radar system.

The MiG-29 is armed with the 30mm GSh-301 built-in

gun with an ammunition load of 150 rounds.

The MiG-29’s suspendable weapons are arranged on

six external hardpoints and consist of:

- R-27 air-to-air medium-range missiles (up to 2 pcs);

- R-73 or R-60 air-to-air short-range missiles (up to 6 pcs);

- S-5, S-8, S-24 unguided rockets (up to 4 rocket pods);

- aerial bombing armament weighing up to 2000 kg.

To enhance its flight safety and combat survivability,

the fighter is equipped with:

- powerplant enabling the crew to perform single-

engine flight and landing;

- dedicated automatic system preventing the aircraft

from falling beyond critical flight modes;

- effective firefighting system and self-sealing fuel tanks;

- K-36M ejection seat-based crew escape system.

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