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Su-35

Sukhoi Su-35
On the world fighter market Russia’s Sukhoi is pinning its hopes, in the near future, on a substantially modernized Su-35 multi-role fighter. The model must be an interim type between today’s Su-30MK in various configurations and a prospective fifth-generation fighter, whose deliveries may start in the second half of the next decade. The Su-35 is a 4++ generation aircraft employing technologies of the fifth generation. They make it superior to all other 4th generation fighters now under development worldwide. In 2009-2015, thanks to these technologies, the Su-35 will dominate the world market, outperforming other proposed multi-role fighters.
The first experimental Su-35, completed in summer 2007 at Komsomolsk-na-Amure Aviation Production Association (KnAAPO) first appeared at Russia’s MAKS-2007 air show.
A new aircraft with an old name
The Su-35 has long been a brand name in the aviation world. Since 1992, an export version of the Su-27 fighter (created under the order of the Russian Air Force) has been demonstrated at international air shows. At the turn of the millennium, Su-35 fighters participated in the tenders of Korean and Brazilian air forces. By the mid-decade of the new century, a general concept emerged of a considerably modified Su-27 fighter, which retained the name of Su-35.
What is new in the Su-35? First off, the fighter will get an improved airframe, which will dramatically increase its service life to 6,000 hours, 30 years of operation (the time before the first test and recondition and the between-repairs period has been increased to 1,500 hours, or 10 years of operation). Aerodynamically it is similar to the Su-27. But unlike the Su-30MKI it will feature no canard fins. All the three channels will have electrically signaled control without mechanical cabling. The use of a new integrated control system (developed by MNPK Avionika Moscow-based Research and Production Association) simultaneously performing functions of several systems – remote control, automatic control, limiting signals system, air signals system, chassis wheels braking system – will enhance the fighter’s handling capability and maneuverability.
Among the Su-35 design features, worth of note is the absence of an overhead brake flap, a standard characteristic of the Su-27. Its functions are performed by an active rudder. The Su-35 chassis has been reinforced because of the increased takeoff and landing weight of the aircraft. For the same reason, the front bearing has two wheels. The improved radar stealth reduces the reflectance of the Su-35 in the X radio waveband and in the angle range of ±60°.
The “heart” of the aircraft
Another important difference of the Su-35 from predecessors from the Su-27 family is the use, in its power plant, of new engines with an increased thrust. Those engines, known as 117S, have been developed by NPO Saturn Research and Production Association.
In terms of engineering, the engines are substantially modified AL-31F production engines employing fifth-generation technologies. They use a new fan, new high and low pressure turbines, and a new digital control system. A provision is made for using a vectored thrust nozzle. The modernization has increased the engine special mode thrust by 16%, up to 14,500 kgf. In the maximum burner-free mode it reaches 8,800 kgf. Compared to today’s AL-31F engines, their capabilities will grow substantially, by 2 to 2.7 times. For instance, the between-repair period will grow from 500 to 1,000 hours (the operating period before the first overhaul is 1,500 hours). The designed period will vary between 1,500 and 4,000 hours.
The 117S engines will be co-produced by Ufa-based Motor Building Association and Rybinsk-based NPO Saturn Research and Production Association. The first production 117S engines were delivered to KnAAPO in early 2007 for testing on the first experimental Su-35 aircraft.
New onboard systems
The distinctive feature of Su-35 is the employment of a new suite of onboard instruments. Its core is the information management system (IMS), which integrates functional, logical, informational and software subsystems into a single complex that ensures the interaction between the crew and equipment. The IMS includes two central digital computers, commutation and information devices and an indication system built on the “all-glass cockpit” concept.
The core of the Su-35 cockpit instrumentation suite are two full-color multi-function liquid crystal displays of MFI type, a multi-function panel with a built-in display processor, a wide angle collimatory display on the windshield and a control and indication panel.
MFI multi-function displays with a built-in processor measure 9 x 12 inches (diagonal 15 inches) and have a resolution of 1400x1050 pixels. They are intended for reception, processing and production, in a multiple window mode, of graphic, numeric, alphabetic and symbolic information. They also present televised information received from onboard TV sensors and impose on it synthesized numeric, alphabetic and symbolic information. Besides, they produce and send video signals in a digital format to the video record unit. The multi-function panel with a built-in display processor presents the required information and issues commands by pushing the buttons on the button array at any time in flight. The airborne collimatory display with a built-in processor monitors the space beyond the cockpit. The information is processed by control signals. The collimator angle of view is 20x30о.
The onboard systems and armament in the new cockpit of Su-35 are controlled by buttons and switches on the aircraft control joystick and engine control levers as well as by a button array on multi-function displays. Thus the HOTAS concept is realized on this type of aircraft. The displays and some other avionics systems of Su-35 are developed by Instrument Design Bureau of Ramenskoye and affiliated companies of Tekhnokompleks Research and Production Association.
“Eyes and ears”
The core of the Su-35 armament is a new radar control system with a phased antenna array (Irbis-E). It features unique capabilities in terms of the target detection range. This is a development V V Tikhomirov Research Institute of Instrument Production. In design, this is an X-waveband multi-role radar with a passive phased antenna array (PAA) mounted on a two-step hydraulic drive unit (in azimuth and roll). The antenna device scans by an electronically controlled beam in azimuth and angle of elevation in sectors not smaller than 60°. The two-step electro-hydraulic drive unit additionally turns the antenna by mechanic means to 60° in azimuth and 120° in roll. Thus, in using the electronic control and mechanical additional turn of the antenna, the maximum deflection angle of the beam grows to 120°.
Irbis-E radar control system detects and tracks up to 30 air targets, retaining continuity of space observation and engaging up to eight targets. The system detects, chooses and tracks up to four ground targets in several map-making modes with various resolution at a range of up to 400 km, without stopping to monitor the airspace.
Irbis-E radar detects air targets with an absolute cross section of 3 m2 on a head-on course at a range of up to 400 km.
Being an improvement on radars with a PAA, Irbis has much better capabilities: expanded (by more than twice) operating frequency band, increased from 70о to 120о target detection and tracking zone in azimuth, substantially (by 2-2.5 times) increased effective range, improved anti-jamming capability, etc. In this aspect, Irbis is comparable to the best foreign counterparts, outperforming most of the US- and Wes-European-made radars with passive and active PAA.
The Research Institute has been developing Irbis since 2004. By now, the engineering prototypes of the system have passed the required bench trials. The first of them has been installed on the Su-30MK2 flying laboratory and is undergoing flight tests. The first flight of the flying laboratory with Irbis onboard occurred in early 2007 at Gromov Flight Test Institute. During the flight, the laboratory proved the superior performance of the new radar in the air-to-surface operating mode.
Among other new onboard systems of the Su-35 is modern navigation and radio communication equipment, systems maintaining fighters operation in a formation and a highly efficient electronic countermeasures suite. The component package of the latter and its complementation with specific jamming devices can be determined by the customer.
Armament
In addition to the armaments onboard the modern Su-30MK, it is planned to additionally arm the Su-35 with new types of air-to-air and air-to-surface guided missiles, including long-range types. The maximum ordnance load of the Su-35 is 8,000 kg. This is placed in 12 weapon stations.

Su-33

Sukhoi Su-33
The Su-33 aeroplane has been developed on the platform of the Su-27; it is manufactured in Komsomolsk-on-Amur.
The Su-33 is a single-seat ship-based STOBAR fighter, with upward folding wings and horizontal tail surfaces (for hangar storage); it is equipped with probe-and-drogue flight refuelling capability. The Su-33 is designed for defence of naval ships from aerial threats.

Aircraft performance
Maximum takeoff weight, kg 33,000
Maximum ordnance, kg 6,500
Service ceiling (without external ordnance and stores), km 17
Maximum flight speed (without external ordnance and stores), km/h 2,300
G-limit (operational) 8
Maximum flight range, km 3,000
Landing approach speed, km/h 240
Crew 1
Aeroplane dimensions:
     - length, m 21.19
     - wingspan, m 14.7 (7.4*)
     - height, m 5.9
In-flight refuelling system
Maximum flow rate
(at entry pressure 3.5 kg/cm 2), l/min
1,100
Powerplant
Number and type of engines 2 x AL-31F
Thrust in afterburner, kgf 12,500 -2 %
Avionics
     1. Fire control system
          1.1. Search and track radar
          1.2. IRST and laser rangefinder
               1.2.1. Optical search and track station
               1.2.2. Helmet-mounted target designator
          1.3. IFF system interrogator
          1.4. Unbiased monitoring system
          1.5. Wide-angle HUD
     2. Flight navigation system
          2.1. Attitude and heading reference system
          2.2. Radiotechnical system for short-range navigation, landing approach and landing of ship-based aircraft
          2.3. Doppler navigator
          2.4. GPS system
          2.5. International navigation system
     3. Marker radio receiver
     4. Remote control system
     5. IFF transponder
     6.Electronic countermeasure equipment
          6.1. Radar warning receiver
          6.2. Chaff and heat flare dispenser
          6.3. Radio jamming transmitter (in pod)
     7. Communications system
     8. Onboard monitoring system
     9. On-board flight data recording device
     10. Onboard voice information playback equipment.
     11. Emergency warning system
     12. Aircraft responder
* With folded wing panels and foreplanes
Armaments
1. Guns Onboard 30mm gun
2. Guided air-to-air missiles R-27R1(ER1) R-27T1(ET1) R-73E
3. Unguided missiles S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25-OFM-PU
4. Bombs, calibre, kg 50, 100, 250, 500
5. Cluster bombs RBK-500
6. External fuel tanks n/a
7. Suspension points 12

Su-30МК

Sukhoi SU-30MK

The Su-30MK aeroplane has been designed on the platform of the Su-27UB; it is in series production in Komsomolsk-on-Amur and in Irkutsk.
The Su-30MK is a two-seat highly-manoeuvrable fighter designed for air-superiority and strikes at ground and naval surface targets using a variety of guided and unguided ADO, with an option of supporting group actions.

Aircraft performance
Takeoff weight:
     - normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg 24,900*
     - maximum, kg 34,500
     - max, kg 38,800
Maximum landing weight, kg 23,600
Max landing weight, kg 30,000
Maximum internal fuel, kg 9,640
Normal internal fuel, kg 5,270
Maximum ordnance, kg 8,000
Service ceiling (without external ordnance and stores), km 17.3
Maximum flight speed at sea level (without external ordnance and stores), km/h 1,350
Max Mach (without external ordnance and stores) 2.00 (1.9**)
G-limit (operational) 9
Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance):
     - at sea level, km 1,270
     - at height, km 3,000
     - with one refuelling (at 1.500 kg fuel remaining), km 5,200
     - with two refuellings in flight, km 8,000
Maximum airborne time (pilot-dependent), hours 10
Takeoff run at normal takeoff weight, m 550
Landing run at normal landing weight (with braking parachute), m 750
Aeroplane dimensions:
     - length, m 21.9
     - wingspan, m 14.7
     - height, m 6.4
Crew 2
In-flight refuelling system
Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min 1,100
Powerplant
Number and type of engines 2 x AL-31F (2 x AL-31FP***)
Thrust in afterburner, kgf 12,500 -2 %
Avionics
     1. Fire control system
          1.1. Air-to-air fire control system
               1.1.1. Search and track radar
               1.1.2. IRST and laser rangefinder
                    1.1.2.1. Optical search and track station
                    1.1.2.2. Helmet-mounted target designator
               1.1.3. Wide-angle HUD
               1.1.4. IFF system interrogator
          1.2. Air-to-surface fire control system
               1.2.1. Coloured multi-purpose LCD indicators
               1.2.2. Onboard digital computer
               1.2.3. GPS satellite-based navigation system
               1.2.4. Weapons control system
     2. Aeroplane remote control system
     3. IFF system transponder
     4. Antenna feed system
     5. Flight navigation system
          5.1. Digital computer
          5.2. Attitude and heading reference system
          5.3. Short-range radiotechnical navigation system
          5.4. GPS system
          5.5. Autopilot system
          5.6. Altitude and speed data processing and display system
          5.7. Air data system
     6. Electronic countermeasure equipment
          6.1. Radar warning receiver with an expansion block
          6.2. Chaff and heat flare dispenser
          6.3. Radio jamming transmitter (in pod)
     7. Communications system
          7.1. VHF and UHF band communications transceiver
          7.2. VHF and UHF band communications transceiver
          7.3. SW band radio communications transceiver
     8. Onboard automatic control system
          8.1. Integrated onboard control and crew warning system
          8.2. Flight information recording equipment
          8.3. Onboard emergency situation warning equipment
     9. Video recording system
          9.1. Onboard video recorder
          9.2. Forward vision video camera
          9.3. Video controller
     10. Aircraft responder
     11. Telecommand homing system
     12. Pod-type IRST and laser rangefinder
Limits
Aircraft limit:
     - SLL, hours 3,000
     - to first overhaul, hours 1,500
     - service life, years 25
Engine and outboard accessory-gearbox life:
     - to first overhaul, hours 500
     - service life limit, hours 1,500
*May vary depending on the equipment configuration installed upon customer's request
**With canard surfaces installed
***With thrust vector control engine installed
Armaments
1. Guns Onboard 30mm gun with 150 rds
2. Guided air-to-air missiles R-27R1(ER1) R-27T1(ET1) R-27P(EP) R-73E RVV-AYe
3. Guided air-to-surface missiles Kh-59ME Kh-31A, Kh-31P Kh-29T(TYe), Kh-29L
4. Guided bomb units KAB-500KR, KAB-500OD KAB-1500KR, KAB-1500L
5. Air bombs FAB-500T BETAB-500ShP ODAB-500PM OFAB-250-270 OFAB-100-120 P-50T Incendiary bombs
6. Cluster bombs RBK-500 SPBE-D
7. Unguided missiles S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU
8. External fuel tanks N/a
9. Suspension points 12

Su-32

Sukhoi Su-32
The Su-32 plane is a special-purpose version of the Su-27; its production is being set up in Novosibirsk.
The two-seat Su-32 fighter-bomber is designed for tactical deployment against air, ground and naval targets (including small and mobile targets) on solo and group missions in daytime and at night, under favourable and adverse weather conditions and in a hostile environment with counter-fire and EW counter-measures deployed, as well as for air reconnaissance.

Aircraft performance
Normal takeoff mass, kg 38,240
Maximum ordnance, kg 8,000
Service ceiling (without external ordnance and stores), km 15
Maximum flight speed at sea level (without external ordnance and stores), km/h 1,400
Maximum flight speed at altitude (without external ordnance and stores), km/h 1,900
G-limit (operational) 9
Maximum range, km 1,100
Ferry range, km 4,000
Maximum airborne time (pilot-dependent), hours 10
Aeroplane dimensions:
     - length, m 23.34
     - wingspan, m 14.7
     - height, m 6.09
Crew 2
In-flight refuelling system
Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min 1,100
Powerplant
Number and type of engines 2 x AL-31F
Thrust in afterburner, kgf 12,500 -2 %
Avionics
     1. Avionics
          1.1. Electronic countermeasures suite
          1.2. Multi-purpose forward-looking PAA radar
     2. Optical-electronic attack and navigation system
          2.1. Information visualisation system
          2.2. Onboard graphics station
          2.3. Laser/TV station
     3. Aeroplane control system
          3.1. Autopilot system
          3.2. Remote control system
     4. Communications system
     5. Integrated defensive aids suite
     6. Kh-59ME missile preparation and telecommand homing equipment pod
     7. Monitoring and recording system
          7.1. Onboard automatic monitoring and display system
          7.2. Unbiased monitoring equipment
          7.3. Flight information recording equipment
Armaments
1. Guns Onboard 30mm gun with 150 rds
2. Guided air-to-air missiles R-27R1(ER1) R-27T1(ET1) R-73E RVV-AYe
3. Guided air-to-surface missiles Kh-59ME Kh-31A, Kh-31P Kh-29T(TYe), Kh-29L S-25LD
4. Guided bomb units KAB-500KR, KAB-500L KAB-500KR, KAB-500L
5. Air bombs FAB-500T BETAB-500ShP ODAB-500PM OFAB-250-270 OFAB-100-120 P-50T Incendiary bombs
6. Cluster bombs RBK-500 SPBE-D
7. Unguided missiles S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU
8. External fuel tanks PTB-3000 (3,050 l)
9. Suspension points 12

Su-27UBK

Sukhoi Su-27UBK
The converted fighter Su-27UBK is designed for teaching airborne personnel piloting skills, aircraft navigation and operational use, as well as for destruction of airborne targets in daytime and at night, under favourable and adverse weather conditions and for ground attack using unguided ADO.

Armaments
1. Guns Onboard 30mm gun with 150 rds
2. Guided air-to-air missiles R-27R1(ER1) R-27T1(ET1) R-73E RVV-AYe
3. Unguided missiles S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU
4. Bombs, calibre, kg 100, 250, 500
5. Cluster bombs RBK-500SPBE-D
6. External fuel tanks n/a
7. Suspension points 10
Limits


Aircraft performance
Takeoff weight:
     - normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg 23,900*
     - maximum, kg 33,000
Maximum landing weight, kg 21,000
Max landing weight, kg 23,000
Maximum internal fuel, kg 9,400
Maximum ordnance, kg 4,430
Service ceiling (without appendages), km 17.5
Maximum flight speed at sea level (without external ordnance and stores, km/h 1,400
Max Mach (without external ordnance and stores) 2.0
G-limit (operational) 9
Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance):
     - at sea level, km 1,270
     - at height, km 3,000
Maximum airborne time, hours 4.5
Takeoff run at normal takeoff weight, m 550
Landing run at normal landing weight (with braking parachute), m 670
Aircraft dimensions:
     - length, m 21.9
     - wingspan, m 14.7
     - height, m 6.4
Crew 2
Powerplant
Number and type of engines 2 x AL-31F
Thrust:
     - in afterburner, kgf 12,500 -2 %
     - at full power, kgf 7,670 ± 2 %
Avionics
     1. Fire control system (to be upgraded for use of RVV-AYe rocket)
          1.1 Search and track radar (to be upgraded for use of new ADO types)
          1.2. IRST and laser rangefinder
               1.2.1. Optical search and track station
               1.2.2. Helmet-mounted target designator
          1.3. IFF system interrogator
          1.4. Wide-angle HUD
     2. Fire control system (to be upgraded for use of new ADO types)
     3. GPS satellite-based navigation system
     4. Flight navigation system
          4.1. Attitude and heading reference system
          4.2. Short-range radio navigation system
          4.3. Autopilot system
          4.4. Radio altimeter
          4.5. Air data system
          4.6. Limiting signal system
     5. IFF system transponder
     6. Communications system
          6.1. VHF/UHF-band communications transceiver
          6.2. SW band radio communications transceiver
          6.3. Data communication terminal equipment
     7. Electronic countermeasure equipment
          7.1. Radar warning receiver
          7.2. Radio jamming transmitter (in pod)
          7.3. Chaff and heat flare dispenser
     8. Monitoring and recording system
          8.1. Integrated onboard control and crew warning system
          8.2. Flight information recording equipment
          8.3. Onboard emergency situation warning equipment
          8.4. Emergency warning system
     9. Aircraft responder
     10. Command guidance equipment
Limits
Aircraft limit:
- SLL, hours 2,000
- to first overhaul, hours 1,000
- service life, years 20
Engine and outboard accessory-gearbox life:
- to first overhaul, hours 300
- service life limit, hours 900
*May vary depending on the equipment configuration installed upon customer's request

Su-27SК

Sukhoi Su-27SК

The Su-27SK aeroplane has been developed on the platform of the Su-27, one of the best fighters in its class; it is produced in Komsomolsk-on-Amur. The Su-27SK is a highly-manoeuvrable fighter designed for air-superiority and ground attack using unguided ADO.

Aircraft performance
Takeoff weight:
- normal (including rockets 2xR-27R1 + 2xR-73E, 5270 kg fuel), kg
- maximum, kg

23,430*
30,450
Maximum landing weight, kg 21,000
Max landing weight, kg 23,000
Maximum internal fuel, kg 9,400
Maximum ordnance, kg 4,430
Service ceiling (without external ordnance and stores), km 18.5
Maximum flight speed at sea level (without external ordnance and stores), km/h 1,400
Max Mach (without external ordnance and stores) 2.35
G-limit (operational) 9
Maximum flight range (with rockets 2xR-27R1, 2xR-73E launched at half distance):
- at sea level, km
- at height, km


1,340
3,530
Maximum airborne time, hours 4.5
Take-off run at normal takeoff weight, m 450
Landing run at normal landing weight (with braking parachute), m 620
Aircraft dimensions:
- length, m
- wingspan, m
- height, m

21.9
14.7
5.9
Crew 1
Powerplant
Number and type of engines 2 x AL-31F
Thrust:
- in afterburner, kgf
- at full power, kgf

12,500 -2 %
7,670 ± 2 %
Avionics
1. Fire control system:
1.1. Search and track radar
1.2. IRST and laser rangefinder linked to pilot's helmet-mounted target designator
1.3. Wide-angle HUD
1.4. IFF system interrogator
1.5. Weapons control system
2. Remote control system
3. IFF system transponder
4. Antenna feed system
5. Flight navigation system composed of:
5.1. Navigation system composed of:
5.1.1. Digital computer
5.1.2. Attitude and heading reference system
5.1.3. Short-range radiotechnical navigation system (SRRNS)
5.1.4. Automatic direction finder
5.2. Autopilot system
5.3. Altitude and speed data processing and display system
6. GPS satellite-based navigation system
7. Marker radio receiver
8. Electronic countermeasure equipment
8.1. Radar warning receiver
8.2. Chaff and heat flare dispenser
8.3. Radio jamming transmitter (in pod)
9. Communications system, including
9.1. VHF and UHF band communications transceiver
9.2. VHF and UHF band communications transceiver
9.3. SW band radio communications transceiver
9.4. Data communication terminal equipment
10. Onboard automatic monitoring system
10.1. Integrated onboard early warning system
10.2. Flight information recording equipment with operational storage unit
10.3. Onboard emergency situation warning equipment
10.4. Emergency warning system
10.5. Onboard recording device
11. Aircraft responder
Limits
A limit:
- SLL, hours 2,000
- to first overhaul, hours 1,000
- service life, years 20
Engine and outboard accessory-gearbox life:
- to first overhaul, hours 300
- service life limit, hours 900
*May vary depending on the equipment configuration installed upon customer's request

Armaments
1. Guns Onboard 30mm gun with 150 rds
2. Guided air-to-air missiles R-27R1(ER1) R-27T1(ET1) R-73E
3. Unguided missiles S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU
4. Bombs, calibre, kg 100, 250, 500
5. Cluster bombs RBK-500
6. External fuel tanks n/a
7. Suspension points 10


Su-25К

Sukhoi Su-25К

The upgraded single-seat armoured subsonic attack aircraft Su-25 is designed for close support of ground forces over the battlefield in daytime and at night, the targets being within visible range, as well as for support of installations with given coordinates on a 24-hour basis in all weathers.

Aircraft performance
Takeoff weight:
     - normal (with 2xFAB-500 + 2xR-73E), kg 14,440
     - maximum, kg 19,300
Landing weight:
     - normal (without external ordnance and stores), kg 11,020
     - maximum, kg 13,200
Maximum ordnance load, kg 4,000
Service ceiling (without external ordnance and stores), km 7
Maximum flight speed at sea level (without external ordnance and stores), km/h 950
Max Mach (without external ordnance and stores) 0.82
G-limit (operational) +6.5/-2.0
Practical flight range without external ordnance and stores, km:
     - at sea level, km 500
     - at height, km 1,000
     - with 4 x PTB-800 (to be dropped), km 1,850
Take-off run:
     - with normal takeoff weight, m 500
     - with maximum takeoff weight, m 1,050
Landing run:
     - with normal landing weight, m 550
     - with maximum landing weight, m 750
Aircraft dimensions:
    - length, m 15.05
    - wingspan, m 14.5
    - height, m 2
Crew 1
Powerplant
Number and type of engines 2 x R-195
Thrust in full power, kgf 4,500
Avionics
     1. Attack and navigation system
         1.1 Visualisation-of-information and control system composed of:
               1.1.1. On-board digital device
               1.1.2. Collimating aviation indicator
               1.1.3. Multi-purpose colour LCD indicator
               1.1.4. Output information generation block
               1.1.5. Information input system block
               1.1.6. Voltage control
               1.1.7 Mapping information generation block
         1.2. GPS system
         1.3. Attitude and heading reference system
         1.4. Short-range radiotechnical navigation system
         1.5. Doppler navigator
         1.6. Radio altimeter
         1.7. Air data system
         1.8. Laser target illuminator and rangefinder
         1.9. Control signal generation equipment
     2. Radio equipment:
          2.1. Radio communications transceiver
          2.2. Ground troops communications link set
          2.3. Voice information equipment
          2.4. IFF transponder
          2.5. Automatic direction finder
          2.6. Marker radio receiver
          2.7. Aircraft responder
     3. Electronic countermeasure equipment
          3.1. Radar illumination warning station
          3.2. Automatic device for passive jamming emission
          3.3. Small-size active jamming transmitter (in pod)
     4. Registration, monitoring and alarm instrumentation
          4.1. Onboard system of video surveillance and information recording
               4.1.1. Video recording system
               4.1.2. Onboard system for recording of tactical employment results
          4.2. Emergency warning system
          4.3. On-board device for flight configuration recording
               4.3.1. Onboard solid-state FLASH memory storage unit
          4.4. Multi-function flight recorder
     5. Weapons control system

Armaments
1. Guns Onboard 30mm gun with 250 rds
2. Guided air-to-surface missiles Kh-29L, Kh-25LD, (L)
3. Guided air-to-air missiles R-73E
4. Incendiary bombs ZB-500
5. Unguided missiles Type: S-8, S-13, S-24, S-25
6. Air bombs: 100, 250, 500
7. Small-size cargo pods KMGU-2
8. External fuel tanks PTB-800 (840 l),
PTB-1,150 (1,160 l)
9. Suspension points 11

Su-24МК

Sukhoi Su-24МК
The upgraded front-line bomber Su-24MK is designed for bombardment with bombs and missiles in favourable and adverse weather conditions, in daytime and at night, including at low altitudes with pinpoint destruction of ground and naval surface targets.

Aircraft performance
Takeoff weight:
     - normal, kg 38,040
     - maximum, kg 43,755
Maximum landing weight, kg 27,900
Maximum internal fuel, kg 11,100
Normal ordnance load, kg 3,000
Maximum ordnance load, kg 8,000
Service ceiling (without external ordnance and stores), km 11
Maximum flight speed at sea level (without external ordnance and stores), km/h 1,315
Max Mach (without external ordnance and stores) 1.35
G-limit (operational) 6
Operational radius of action at sea level in mixed mode (Vcr in the 200-km area, V=900 km/h in other areas) with PTB external fuel tanks and 6x FAB -500M-62 bombs, km 615
Ferry flight range with 2xPTB-3000 external fuel tanks, km:
     - with PTB external fuel tanks dropped 2,775
     - with one in-flight refuelling 5,000
Takeoff run at normal take-off weight, m 1,550
Landing run at normal landing weight (with braking parachute), m 1,100
Aeroplane dimensions:
     - length, m 24.532
     - wingspan, m 17.638 (10.366)
     - height, m 6.193
Crew 2
In-flight refuelling system
Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min 1,100
Powerplant
Number and type of engines 2 x AL-21FZA
Thrust:
     - in afterburner, kgf 111,200
     - at full power, kgf 11,200
Avionics
     1. Attack and navigation system
          1.1. Digital computer device
          1.2. Doppler navigator
          1.3. Optical sighting device
          1.4. I/O device (I/O)
          1.5. On-board switchgear (OBS)
          1.6. Photo recording equipment set
          1.7. Control signal conditioner
          1.8. Onboard module of Tekon-1 television guidance system
          1.9. Laser/TV search and track system (LTVSTS)
          1.10. Radio command linkage
          1.11. Passive radar:
     - letter A and A' instrumentation pod
    - letter B, B' and C instrumentation pod
          1.12. Nose radar scanner (NRS)
          1.13. Collision-warning radar (CWR)
          1.14. Small-size inertial instrument system
          1.15. Low-range radio altimeter
          1.16. NRS video signal onboard processing block
          1.17. TV display
          1.18. GPS satellite-based navigation system
     2. Autopilot system
     3. IFF equipment
     4. VHF-UHF communications transceiver
     5. Short-wave radio
     6. Automatic direction finder
     7. Aircraft responder
     8. Electronic countermeasures system
          8.1. Radar warning receiver
          8.2. Jamming capabilities control device
          8.3. Active jamming system
          8.4. Infrared search and track sensor (IRSTS)
          8.5. Cartridge ejection mechanism
     9. Integrated defensive aids suite
     10. Long-range radiotechnical navigation system
     11. Short-range radiotechnical navigation system
     12. Flight data recorder system
     13. Camera
     14. Tape-recording mechanism, solid-state storage unit
     15. Combat performance monitoring equipment
     16. VCR
     17. Weapons control system
* As per equipment delivery specification
Armaments
1. Guns Onboard 23mm gun with 500 rds
2. Guided air-to-surface missiles Kh-25ML
Kh-25MR (Kh-23M)
Kh-29L
Kh-29T
Kh-58E,
Kh-58E-01 (lit. A, A', B, C)
Kh-31P (lit. A, A', B, B', C)
Kh-31A
Kh-59,
Kh-59ME
S-25LD
3. Guided air-to-air missiles R-60MK (R-60), R-73E
4. Guided bomb units KAB-500KR, KAB-500L
5. Air bombs: AB-100
AB-250 (M54)
AB-250 (M62)
AB-500M-54
ODAB-500PM
6. Cluster bombs RBK-250
RBK-500
7. Incendiary bombs S-24B
8. Unguided missiles: S-25-OFM
9. Small-size cargo pods KMGU-2
10. Pod guns SPPU-6
11. External fuel tanks PTB-2,000 (1,860 l),
PTB-3,000 (3,050 l)
12. Suspension points 8


Su-22М4

Sukhoi Su-22М4
The upgraded supersonic fighter-bomber Su-22M4 is designed for destruction of ground and naval surface targets in daytime and at night under favourable and adverse weather conditions, comprehensive reconnaissance and air-to-air "dogfight" combat.
Armaments
1. Guns Two 30mm guns, with 80 rds each
2. Guided air-to-surface missiles Kh-58UE,
Kh-25ML
(MR, MP letter A),
Kh-29T (L),
S-25L,
Kh-31A
3. Guided bomb units KAB-500KR
4. Guided air-to-air missiles R-60 (R-60M)
5. Unguided missiles S-5,
S-24,
S-25
6. Bombs, calibre, kg 100, 250, 500
7. Cluster bombs RBK-500
8. Incendiary bombs ZB-500
9. Small-size cargo pods KMGU-2
10. Suspended guns (pivoting to shoot back and forth) SPPU
11. External fuel tanks PTB-800 (840 l),
PTB-1,150 (1,160 l)
12. Suspension points 10

Aircraft performance
Takeoff weight:
     - normal (with full internal fuel, 2xR-60, 1 tn of bombs), kg 16,400
     - maximum (with full internal fuel, 4 tn of bombs), kg 19,430
Maximum internal fuel, kg 3,770
Maximum ordnance, kg 4,000
Service ceiling (without external ordnance or stores), km 14.2
Maximum flight speed at sea level (without external ordnance or stores), km/h 1,400
Max Mach (external ordnance or stores) 1.7
G-limit (operational) 7
Maximum flight range (with 1 tn ordnance, 4x PTB-800):
     - at sea level, km 1,380
     - at height, km 2,300
Takeoff run at maximum takeoff weight, m
Landing run at normal landing weight (with braking parachute), m 950
Aircraft dimensions:
     - length, m 19.02
     - wingspan, m 10.02 (13.68)
     - height, m 5.12
Crew 1
Powerplant
Number and type of engines 1 x AL-21F3
Thrust:
     - in afterburner, kgf 112,000
     - at full power, kgf 8,000
Avionics
     1. Attack and navigation system
          1.1 Onboard computer
          1.2. On-board digital device
          1.3. Laser target illuminator and rangefinder
          1.4. Doppler navigator
          1.5. Sight tube
          1.6. Digital mapping system
          1.7. Television signals switching unit
          1.8. HUD
          1.9. Air-to-radar missile guidance with Luch display
          1.10. Attitude and heading reference system
          1.11. Short range radio navigation and landing system
          1.12. Short range radio navigation system
          1.13. Long range radio navigation system
          1.14. Air data system
          1.15. Automatic direction finder
          1.16. Aircraft responder
          1.17. Control signal generation equipment
          1.18. Information input system
     2. GPS system
     3. Weapons control system
     4. Autopilot system
    5. Radio altimeter
    6. Communications radio transceiver
    7. IFF transponder
    8. Marker radio receiver
    9. Combat performance monitoring system
    10. Flight recorder  
    11. Defence
         11.1. Radar warning receiver
         11.2. Radio jamming transmitter (in pod)
         11.3. Infrared and passive jamming device
     12. Sensors (in pod)
     13. Kh-25MR missile (pod) guidance system
     14. Infrared imaging system (in pod)
     15. Kopyo search and track radar system
     16. Power supply and CEJ pod
     17. CEJ blocks for Kh-31A
Limits
Airframe limit:
- SLL, hours 2,000
- service life, years 20

Su-22М3

Sukhoi Su-22m3
The upgraded supersonic fighter-bomber Su-22M3 is designed for destruction of ground and surface naval targets in daytime and at night under favourable and adverse weather conditions, as well as for air combat and comprehensive reconnaissance missions



Armaments
1. Guns Two 30mm guns, with 80 rds each
2. Guided air-to-surface missiles Kh-23M,
Kh-25MR (ML, MP),
Kh-29L,
Kh-28
3. Guided air-to-air missiles R-60 (R-60M)
4. Unguided missiles S-5,
S-8,
S-24,
S-25
5. Bombs, calibre, kg 100, 250, 500
6. Cluster bombs RBK-100
RBK-250
RBK-500
7. Incendiary bombs ZB-500
8. Small-size cargo pods KMGU
9. External fuel tanks PTB-800 (840 l),
PTB-1150 (1160 l)
10. Suspension points 10


Aircraft performance
Takeoff weight:
- normal (without external ordnance or stores, with full integral tankage), kg 15,590
- maximum, kg 19,640
Maximum internal fuel, kg 3,770
Maximum ordnance, kg 4,000
Service ceiling (without external ordnance or stores), km 14.2
Maximum flight speed at sea level (without external ordnance or stores), km/h 1,350
Maximum flight speed at high altitude (without external ordnance or stores), km/h 1,900
g limit (operational) 7
Maximum flight range (with external tanks and 1 tn ordnance):
- at sea level, km 1,300
- at height, km 2,100
Takeoff run at maximum takeoff weight, m 1,600
Landing run at normal landing weight (with braking parachute), m 950
Aircraft dimensions:
- length, m 18.91
- wingspan, m 10.02 (13.68)
- height, m 5.01
Crew 1
Powerplant
Number and type of engines 1 x R-29BS-300
Thrust:
- in afterburner, kgf 11,500
- in full power, kgf 800
Avionics
1. Navigation and flight equipment
1.1.Navigation
1.1.1. Attitude and heading reference system
1.1.2. Doppler navigator
1.1.3. Short range radio navigation and landing system
1.2.Automatic direction finder
1.3. Radio altimeter
1.4. Air data system
1.5. Angle-of-attack and g-load indicator
1.6. Autopilot system
2. Aiming equipment
2.1. Aircraft gun bombsight
2.2. Laser rangefinder and target illuminator
2.3. Control equipment for X-23M rockets (in pod)
2.4. Air-to-surface missile guidance set
3. Radio equipment
3.1. Communications transceiver
3.2. IFF transponder
3.3. Aircraft responder
4. Defence
4.1. Radar warning receiver
4.2. Radio jamming transmitter (in pod)
4.3. Passive jamming device
5. Sensors (in pod)
6. GPS system
Limits
Airframe limit:
- SLL, hours 2,000
- service life, years 20


Pesawat Tempur

Pesawat tempur adalah pesawat militer yang dirancang untuk menyerang pesawat lain di udara. Berbeda dengan pesawat pengebom, yang dirancang untuk menyerang target di permukaan. Pesawat tempur relatif lebih kecil, cepat, dan lincah. Pesawat tempur awalnya dikembangkan pada Perang Dunia I untuk menghadapi pesawat pengebom dan balon udara yang mulai lazim digunakan untuk melakukan serangan darat dan pengintaian. Pesawat tempur pertama awalnya berupa pesawat sayap ganda kayu yang diberi senapan mesin ringan. Pada Perang Dunia II, pesawat tempur lebih banyak dibuat dari logam, bersayap tunggal, dan menggunakan senapan mesin yang tertanam pada sayap. Setelah Perang Dunia II, mesin turbojet mulai menggantikan mesin piston, dan peluru kendali mulai digunakan untuk menggantikan senapan mesin sebagai senjata utama. Klasifikasi pesawat tempur dibuat berdasarkan generasi. Penggunaan generasi ini awalnya digunakan petinggi pertahanan di Rusia, yang menyebut F-22 Raptor Amerika Serikat sebagai pesawat tempur "generasi kelima". Pesawat tempur adalah pesawat yang digunakan untuk perang di udara. Umumnya pesawat tempur berbentuk ramping, dapat bergerak lincah, membawa canon (senapan mesin) serta rudal dan bom, berkecepatan tinggi, dilengkapi dengan perlengkapan avionik yang lebih banyak daripada pesawat sipil/penumpang seperti radar yang mampu mendeteksi lawan dalam jarak jauh serta mengunci sasaran lawan. Terlebih lagi dilengkapi dengan peralatan pengecoh dan pengacau radar, sampai berkemampuan "siluman" (stealth).
Pada awalnya manusia menggunakan layang-layang untuk menakuti-nakuti musuh serta memberikan informasi tentang posisi baik kawan maupun lawan atau bahkan menakut-nakuti musuh. Kebiasaan ini dilakukan oleh bangsa Cina kuno. Kemudian pada layang layang dilengkapi dengan manusia untuk mengetahui secara detail posisi lawan. Penemuan balon udara dan Zeppelin juga mewarnai perkembangan pesawat militer. Digunakan mulai dari sekedar pengintaian dan digunakan sebagai pembom untuk mengebom posisi musuh. Tercatat diantaranya adalah Jerman yang memanfaatkan zeppelin untuk membom Inggris dalam Perang Dunia I. Dalam perjalanannya dibuat pesawat-pesawat dan dikembangkan untuk kepentingan peperangan dan pertempuran khususnya pertempuran udara.

Berdasarkan era

  1. Era Perang Dunia I (1911-1935)
  2. Era Perang Dunia II (1939-1945)
  3. Era pesawat Jet (1950-1970)
  4. Era Penyempurnaan Teknologi (1970-sekarang)

Berdasarkan fungsi

  1. Pesawat Burusergap
  2. Pesawat Serang Darat (Attack)
  3. Pesawat Intai
  4. Pesawat Pembom (Bomber)
  5. Pesawat Tempur Latih
  6. Pesawat Tempur Anti Gerilya (COIN)
  7. Pesawat Tempur Multifungsi

Berdasarkan kasat/tidak kasat radar

  1. Pesawat Tempur Konvensional
  2. Pesawat tempur siluman
Contoh Pesawat Tempur (Fighters):

  • JF-17 Thunder, China / Pakistan
  • Chengdu J-20, China
  • Chengdu J-10, China
  • SAC J-31, China
  • SAC J-8 Finback, China
  • Eurofighter Typhoon, European Union
  • Dassault Rafale, France
  • Dassault Mirage 2000 B/C, France
  • Dassault Mirage F1, France
  • HAL Tejas, India
  • IAI Lavi, Israel
  • IAI Kfir, Israel
  • Mikoyan MiG 1.42 (1.44) MFI, Russia
  • Mikoyan MiG-31 Foxhound, Russia
  • Mikoyan MiG-29 Fulcrum, Russia
  • Mikoyan MiG-25 Foxbat, Russia
  • Mikoyan MiG-23 Flogger, Russia
  • Sukhoi PAK FA, Russia
  • Sukhoi S-37 Berkut, Russia
  • Sukhoi Su-27 Flanker, Russia
  • Yakovlev Yak-141 Freestyle, Russia
  • Atlas Cheetah, South Africa
  • Saab JAS 39 Gripen, Sweden
  • Saab 37 Viggen, Sweden
  • AIDC F-CK-1 Ching Kuo, Taiwan
  • Panavia Tornado ADV, United Kingdom / Germany / Italy
  • British Aerospace Sea Harrier, United Kingdom
  • Lockheed Martin F-35, USA
  • Lockheed Martin / Boeing F-22 Raptor, USA
  • Boeing F/A-18E/F Super Hornet, USA
  • Boeing F/A-18A/C Hornet, USA
  • Lockheed Martin F-16 Fighting Falcon, USA
  • McDonnell Douglas F-15 Eagle, USA
  • Grumman F-14 Tomcat, USA
  • Northrop F-5E Tiger II, USA
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