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Wednesday, September 15, 2010

Su-30MK / Su-30 MK2 TNI AU

Su-30MK


Su-30MK basic performances
Engines type 2 x АL-31F
Thrust, kgf 2 x 12500
Length, m 21.9
Wing span, m 14.7
Height, m 6.4
Takeoff weight, kg:
normal 24900
max. 34500
limit 38800
Fuel capacity, kg 9640
Combat load, kg 8000
Max. speed, km/h:
at altitude 2120
sea level 1350
Max. Mach 2
Operational ceiling, m 17300
Limit load factor 9
Range, km:
without refueling 3000
with one refueling  5200
Takeoff run (at normal takeoff weight), m 550
Landing roll (with brake parachute), m 750



Double-seat fighter.

The Su-30MK multipurpose double-seat fighter is a modification of Su-27SK produced serially since 1999.
The fighter is designed to gain air superiority through manned and unmanned aircraft destroying by guided missiles in medium range engagements and dogfights; sea and ground targets destroying by all kinds of weapons first of all by high precision ones while individual and group operations in all weather conditions. Besides the fighter can be operated to perform aerial reconnaissance while naval and land operations as well as while flight crews training to operate the aircraft and to launch weapons. The second pilot helps to reduce the first pilot’s load while combat missions with long-range weapon application, at nights, and long flights with in-flight refueling as well.
Su-30MK has the following peculiarities:
  • modified weapon control system with extended capabilities to destroy ground and sea targets;
  • new cockpit indication system on the base of multifunctional LCD indicators;
  • upgraded navigation and communication system;
  • upgraded EW system;
  • great nomenclature of air-to-air and air-to-surface weapons mounted on 12 hard-points;
  • in-flight refueling system;
  • reinforced airframe and landing gear construction that allows aircraft operation with full fuel tanks and maximal combat load at takeoff weight up to 38.8 tons.
The Su-30MK weapon control system provides detection, tracking and destroying air, ground and sea targets in all weather conditions by day and night.
It comprises two basic parts:
  • air-to-air weapon control system consisting of sight radar system, Optoelectronic sighting system and HUD, and additional capability of the Kh-31A anti-ship missiles launch;
  • air-to-surface weapon control system allowing great nomenclature of high-precision weapon launch to destroy ground targets, and all sight data reflection on 4 MFD on control panels in the cockpits.
The Su-30MK radar can be operated in air-to-air and air-to-surface modes. It ensures air and ground targets detection in all weather conditions by day and night.
Optoelectronic sighting system includes optical location sighting system and helmet mounted target designator. The Su-30MK optical location sighting system represents a combination of IR-direction finder and a laser rangу finder, and it is used to detect and track air targets by its radiation in forward and back hemispheres, to range air and ground targets with the help of laser beam and to illuminate ground targets and destroy them by air-to-surface guided missiles with semi-active laser seekers.
The Su-30MK weapon comprises the GSh-301 airborne quick-fire 30-mm caliber cannon with 150 cartridge round; missiles and bombs mounted on 12 hard-points under the wing and fuselage. Air-to-air missiles include the R-27R1 (R-27ER1) guided medium-range missiles with semi-active seekers, 2 R-27Т1 (R-27EТ1) medium-range missiles with heat seekers, the RVV-AE medium range missiles with active radar seekers, the R-73E dogfight missiles with heat seekers.
The Su-30MK air-to-surface weapon comprises up to 6 Kh-31P anti-radiation missiles with passive radar seekers, up to 6 Kh-31A anti-ship missiles with active radar seekers, up to 6 Kh-29Т (Kh-29ТЕ) short-range missiles with TV-seekers or Kh-29L with semi-active laser seekers, two Kh-59МE medium-range missiles with TV-commanded seekers and up to 6 КАB-500Kr or 3 КАB-1500Kr guided bombs with TV-correlated seekers.
The Su-30MK unguided weapon can include up to 8 bombs (cluster bombs, incendiary tanks) of 500 kg caliber, up to 28 bombs of 250 kg caliber, up to 32 bombs of 100 kg caliber, and up to 80 unguided missiles of S-8 type (in four B-8М1 units), 20 S-13 rockets (in 4 B-13L units), 4 S-25-ОFМ rockets.
Additional materials about this theme:

Su-30MK2


Su-30MK2 basic specifications
Engines type 2 х AL-31F
Thrust, kgf 2 х 12500
Length, m 21,9
Wing span, m 14,7
Height, m 6,4
Max takeoff weight, kg:
- max 34500
- limit 38000
Max internal fuel capacity, kg 9720
Max payload, kg 8000
Max speed, km/h:
- at high altitude 2100
- at sea level 1400
Max Mach number 2
Service ceiling, m 17300
Max g-load 9
Range, km:
- without in-flight refuelling 3000
- with one in-flight refuelling 5600
Run with the normal takeoff weight, m 550
Roll with the drag chute deployed, m 750



Double-seat fighter.

The Su-30MK2 multi-role fighter is designed to gain air superiority through killing hostile manned and unmanned aircraft with guided missiles in medium-range engagements and dogfights, and surface (ground and sea) targets destroying with all types of weapon, first of all with high precision weapon in individual and group operations in all-weather conditions. The aircraft can be used for training flying personnel to hone their flying and fighting skills.
The back-seater reduces the pilot's workload in long-range PGM encounters, in nighttime operations and on protracted missions with in-flight refuelling.
The main features of the Su-30MK2 fighter are the following:
  • an improved fire control system boasting enhanced surface-target capabilities;
  • an advanced cockpit management system;
  • an improved navigation and communications suite;
  • more sophisticated self-defense electronic countermeasures (ECM) suite;
  • an expanded air-to-air and air-to-surface weapons suite with the ordnance mounted externally on 12 hardpoints;
  • an in-flight refueling system;
  • reinforced airframe and landing gear provide for the aircraft operation with max combat load and fuel capacity with take-off weight up to 38 tones.
The fire control system of Su-30MK2 provides for detection, tracking and hitting by onboard weapons aerial and surface targets round the clock and in any weather.
The fire control system comprises two major subsystems:
  • fire control subsystem for air-to-air weapon includes radar sighting system, optronic sight system, and head-up display system;
  • fire control subsystem for air-to-surface weapon provides for the use of a wide spectrum of air-to-surface high-precision weapons, and for the indication of targets designation, flight and navigation data on four 4-х multifunction displays located on the cockpits’ instrument panels.
The mainstay of the cockpit management system are four colour multifunction liquid crystal displays (LCD) and head up-display (in the fore cockpit only). These displays show all required digital and visual target designation, flight and navigation data as well as data on the aircraft systems status. Along with the multifunction LCDs, the instrument panel houses traditional electromechanical instruments, which act mostly as backups.

The radar used on Su-30MK2 in the air-to-air engagement ensures the following:
  • searching for aerial targets;
  • detected targets identification;
  • attacking the targets with medium- and short-range missiles featuring different guidance;
  • searching for, locking on and tracking a visual target in dogfights.
In the air-to-surface mode, the radar ensures the following:
  • all-weather acquisition and positioning of radio-contrast surface targets;
  • surface targets designation data supply to provide the Kh-31A, Kh-35E, and Kh-59MK air-to-ship missiles application.
Optical-electronic sighting system comprising the Optical location station and Helmet-mounted target designation system (HMS). The Optical location station (OLS) of Su-30MK2 is a combination of an infrared search and track system (IRST) and a laser rangefinder/target designator .It is designed to track aerial targets both in the front and rear hemispheres using their infrared signature. It also can be used for the laser ranging of aerial and surface targets as well as for illuminating surface targets by the laser beam for air-to-surface missiles with semi-active laser homing heads application.
The Su-30MK2 weapon suite includes the built-in GSh-301 30-mm automatic single-barrel high-rate-of-fire cannon with ammunition load of 150 rounds, missiles, rockets and bombs mounted externally on 12 hardpoints under wings and fuselage.
The air-to-air weapon suite includes medium-range missiles of the R-27 type – R-27T1, R-27ET1 heat-seeking missiles, R-27R1, R-27ER1 semi-active radar-homing missiles, R-27P1 and R-27EP1 missiles; RVV-AE medium-range active radar-homing missiles; and R-73E short-range heat-seeking missiles.
The Su-30MK2 fighter has wide range of guided and unguided weapons used to destroy surface targets.
The air-to-surface guided weapon of the Su-30MK2 fighter consists of the Kh-59ME, Kh-35E and Kh-59MK missiles; the Kh-31A medium-range high-speed anti-ship active radar-homing missiles; the Kh-31P medium-range antiradar passive radar-homing missiles; Kh-29T, Kh-29TE TV-homing missiles or Kh-29L laser-homing short-range missiles; KAB-1500Kr TV-homing bomb and KAB-500Kr (KAB-500-OD) guided bombs.
The unguided air-to-surface weapons include bombs of 500-kg, 250-kg, and 100-kg caliber, cluster bombs, incendiary tanks, and S-8, S-13, and S-25-OFM rockets as well.
Additional materials about this theme:

KNAAPO

Su-27SKM TNI AU


 
Su-27SK basic specifications
Engines type 2 х AL-31F
Thrust, kgf 2 х 12500
Length, m 21.9
Wing span, m 14.7
Height, m 5.9
Max takeoff weight, kg
33000
Max payload, kg
8000
Max internal fuel capacity, kg
9400
Max sea-level speed, km/h 1400
Max Mach number 2.15
Service ceiling, m 17750
Max g-load
9
Flight range at the cruising altitude, km: 3530
Run with the normal takeoff weight, m 450
Roll with the drag chute deployed, m 700

 

Single-seat multirole fighter.

The Su-27SKM single-seat multi-role fighter is a derivative of the Su-27SK fighter.
The fighter is designed to destroy aerial targets in free air and against the background of land; and surface (ground and sea) targets with guided and unguided weapons at day and night under the all-weather conditions.
The main features of the Su-27SKM fighter are the following:
  • an improved fire control system boasting enhanced surface-target capabilities;
  • an advanced cockpit management system;
  • an improved navigation and communications suite;
  • more sophisticated self-defense electronic countermeasures (ECM) suite;
  • an expanded air-to-air and air-to-surface weapons suite with the ordnance mounted externally on 10 hardpoints;
  • an in-flight refueling system.
The fire control system of Su-27SKM provides for detection, tracking and hitting by onboard weapons aerial and surface targets round the clock and in any weather. The fire control system ensures the application of wider range (in comparison with the Su-27SK fighter) of weapon including the RVV-AE medium-range air-to-air active radar-homing missiles, and air-to-ground high-precision guided weapon with different types of guidance. The fire control system of Su-27SKM comprises two major subsystems: the first subsystem for air-to-air weapons and the second one for air-to-surface weapons.
The mainstays of the cockpit management system are two colour multifunction liquid crystal displays (LCD), colour multifunction display panel with push-buttons, and head up-display. These displays show all required digital and visual target designation, flight and navigation data as well as data on the aircraft systems status. Along with the multifunction LCDs, the instrument panel houses traditional electromechanical instruments, which act mostly as backups.
The radar used on Su-27SKM in the air-to-air engagement ensures the following:
  • searching for aerial targets;
  • detected targets identification;
  • attacking the targets with medium- and short-range missiles featuring different guidance;
  • searching for, locking on and tracking a visual target in dogfights.
In the air-to-surface mode the radar ensures the following:
  • all-weather acquisition and positioning of radio-contrast surface targets;
  • surface targets designation data supply to provide the Kh-31A air-to-ship missile application.
Optical location station (OLS) is a combination of an infrared search and track system (IRST) and a laser rangefinder/target designator. It is designed to track aerial targets by their IR radiation. It also can be used for the laser ranging of aerial and surface targets as well as for illuminating surface targets by the laser beam for air-to-surface semi-active laser-homing missiles application.
Helmet mounted target designation system feeds target designation data to the missiles' homing heads when the pilot turns his head towards the area where any target is expected to be detected.
The Su-27SKM weapon suite includes the built-in GSh-301 30-mm automatic single-barrel cannon, missiles, rockets and bombs mounted externally on 10 hardpoints under wings and fuselage.
The air-to-air weapon suite includes medium-range missiles of the R-27 type – R-27T1, R-27ET1 heat-seeking missiles, R-27R1, R-27ER1 semi-active radar-homing missiles; RVV-AE medium-range active radar-homing missiles; and R-73E short-range heat-seeking missiles.
The Su-27SKM fighter has wide range of guided and unguided weapons used to destroy surface targets.
The air-to-surface guided weapon of the Su-27SKM fighter consists of the Kh-31A medium-range high-speed anti-ship active radar-homing missiles, the Kh-31P medium-range antiradar passive radar-homing missiles, Kh-29T, Kh-29TE TV-homing missiles or Kh-29L semi-active laser-homing short-range missiles; and KAB-500Kr, KAB-500-OD, and one KAB-1500Kr TV-homing bombs.
The unguided air-to-surface weapons include bombs of 500-kg, 250-kg, and 100-kg caliber, cluster bombs, incendiary tanks, and S-8, S-13, and S-25-OFM rockets as well.

KNPOO

Su-27SK TNI AU


 
Su-27SK basic specifications
Engines type 2 х AL-31F
Thrust, kgf 2 х 12500
Length, m 21.9
Wing span, m 14.7
Height, m 5.9
Max takeoff weight, kg
30450
Max internal fuel capacity, kg 9400
Max sea-level speed, km/h 1400
Max Mach number 2.35
Service ceiling, m 18500
Max g-load
9
Flight range at the cruising altitude, km: 3530
Run with the normal takeoff weight, m 450
Roll with the drag chute deployed, m 620

 

Single-seat fighter.

The Su-27SK single-seat multi-role fighter is an export version of the Su-27 fighter that has been serially produced since 1991.
The fighter is designed to gain air superiority through destroying hostile manned and unmanned aircraft with guided missiles in medium-range engagements and dogfights in individual and group operations; and surface (ground and sea) targets destroying with all types of weapon, first of all with high precision weapon (guided missile and bombs) in all-weather conditions.
The main features of Su-27SK are the following:
  • high maneuverability provided by high thrust-to-weight ratio, the aircraft perfect aerodynamics, and Fly-by-wire system used for the aircraft longitudinal control;
  • large flight range due to the aircraft perfect aerodynamics, the power plant high effectiveness, and the inner fuel tanks capacity;
  • integrated weapon control system consists of two independent complementary channels – radar sighting system and optronic sight system with HMS;
  • up-to-date navigation system, communication suite, and ECM suite;
  • an expanded weapons suite (air-to-air guided missiles and bombs, and air-to-surface rockets) with the ordnance mounted externally on 10 hardpoints.
The Su-27SK weapon control system provides for aerial, surface and sea targets designation, tracking and destroying with the air weapon in round-the-clock all-weather conditions. It comprises two main subsystems: radar sighting system and optronic sight system.
Flight and navigation data is indicated on the MFD and HUD, and on the other cockpit instruments as well.
The radar used in Su-27SK is of pulse-Doppler type, it ensures aerial targets searching and tracking in air and against a ground/sea background at 100 km distance. The radar can simultaneously track and prioritize 10 aerial targets, and attack the most dangerous one.
The Su-27SK optronic sighting system comprises Optical-Electronic Location System and HMS (Helmet mounted system). Optical-Electronic Location System is a combination of an infrared search and track system (IRST) and a laser rangefinder/target designator, used to track aerial targets both in the front and rear hemispheres using their infrared signature, and the targets laser ranging.
The Su-27SK aircraft weapons suite includes the built-in GSh-301 30-mm automatic single-barrel high-rate-of-fire cannon with 150 rounds ammunition load; and missiles, rockets and bomb ordnance suspended on 10 hard points located under the wings and fuselage.
Su-27SK can carry up to six R-27R1 (R-27ER1) air-to-air medium-range missiles with semi-active radar homing heads, up to two R-27T1 (R-27ET1) heat-seeking medium-range missiles, and up to six RVV-AE medium-range active radar-homing missiles and six R-73E short-range heat-seeking missiles.
The aircraft weapons suite includes a wide range of different types of weapon to destroy surface (sea) targets. The weapon suite can include bombs of 500, 250 or 100-kg caliber, cluster bombs, incendiary tanks, and the S-8 rockets (in four B-8M1 pods), the S-13 rockets (in four B-13L pods), and the S-25-OFM rockets.
 KNAAPO

Su-30MK2 TNI AU


 
Su-30MK2 basic specifications
Engines type 2 х AL-31F
Thrust, kgf 2 х 12500
Length, m 21,9
Wing span, m 14,7
Height, m 6,4
Max takeoff weight, kg:

- max
34500
- limit
38000
Max internal fuel capacity, kg
9720
Max payload, kg
8000
Max speed, km/h:

- at high altitude
2100
- at sea level
1400
Max Mach number 2
Service ceiling, m 17300
Max g-load
9
Range, km:

- without in-flight refuelling
3000
- with one in-flight refuelling
5600
Run with the normal takeoff weight, m 550
Roll with the drag chute deployed, m 750

 

Double-seat fighter.

The Su-30MK2 multi-role fighter is designed to gain air superiority through killing hostile manned and unmanned aircraft with guided missiles in medium-range engagements and dogfights, and surface (ground and sea) targets destroying with all types of weapon, first of all with high precision weapon in individual and group operations in all-weather conditions. The aircraft can be used for training flying personnel to hone their flying and fighting skills.
The back-seater reduces the pilot's workload in long-range PGM encounters, in nighttime operations and on protracted missions with in-flight refuelling.
The main features of the Su-30MK2 fighter are the following:
  • an improved fire control system boasting enhanced surface-target capabilities;
  • an advanced cockpit management system;
  • an improved navigation and communications suite;
  • more sophisticated self-defense electronic countermeasures (ECM) suite;
  • an expanded air-to-air and air-to-surface weapons suite with the ordnance mounted externally on 12 hardpoints;
  • an in-flight refueling system;
  • reinforced airframe and landing gear provide for the aircraft operation with max combat load and fuel capacity with take-off weight up to 38 tones.
The fire control system of Su-30MK2 provides for detection, tracking and hitting by onboard weapons aerial and surface targets round the clock and in any weather.
The fire control system comprises two major subsystems:
  • fire control subsystem for air-to-air weapon includes radar sighting system, optronic sight system, and head-up display system;
  • fire control subsystem for air-to-surface weapon provides for the use of a wide spectrum of air-to-surface high-precision weapons, and for the indication of targets designation, flight and navigation data on four 4-х multifunction displays located on the cockpits’ instrument panels.
The mainstay of the cockpit management system are four colour multifunction liquid crystal displays (LCD) and head up-display (in the fore cockpit only). These displays show all required digital and visual target designation, flight and navigation data as well as data on the aircraft systems status. Along with the multifunction LCDs, the instrument panel houses traditional electromechanical instruments, which act mostly as backups.

The radar used on Su-30MK2 in the air-to-air engagement ensures the following:
  • searching for aerial targets;
  • detected targets identification;
  • attacking the targets with medium- and short-range missiles featuring different guidance;
  • searching for, locking on and tracking a visual target in dogfights.
In the air-to-surface mode, the radar ensures the following:
  • all-weather acquisition and positioning of radio-contrast surface targets;
  • surface targets designation data supply to provide the Kh-31A, Kh-35E, and Kh-59MK air-to-ship missiles application.
Optical-electronic sighting system comprising the Optical location station and Helmet-mounted target designation system (HMS). The Optical location station (OLS) of Su-30MK2 is a combination of an infrared search and track system (IRST) and a laser rangefinder/target designator .It is designed to track aerial targets both in the front and rear hemispheres using their infrared signature. It also can be used for the laser ranging of aerial and surface targets as well as for illuminating surface targets by the laser beam for air-to-surface missiles with semi-active laser homing heads application.
The Su-30MK2 weapon suite includes the built-in GSh-301 30-mm automatic single-barrel high-rate-of-fire cannon with ammunition load of 150 rounds, missiles, rockets and bombs mounted externally on 12 hardpoints under wings and fuselage.
The air-to-air weapon suite includes medium-range missiles of the R-27 type – R-27T1, R-27ET1 heat-seeking missiles, R-27R1, R-27ER1 semi-active radar-homing missiles, R-27P1 and R-27EP1 missiles; RVV-AE medium-range active radar-homing missiles; and R-73E short-range heat-seeking missiles.
The Su-30MK2 fighter has wide range of guided and unguided weapons used to destroy surface targets.
The air-to-surface guided weapon of the Su-30MK2 fighter consists of the Kh-59ME, Kh-35E and Kh-59MK missiles; the Kh-31A medium-range high-speed anti-ship active radar-homing missiles; the Kh-31P medium-range antiradar passive radar-homing missiles; Kh-29T, Kh-29TE TV-homing missiles or Kh-29L laser-homing short-range missiles; KAB-1500Kr TV-homing bomb and KAB-500Kr (KAB-500-OD) guided bombs.
The unguided air-to-surface weapons include bombs of 500-kg, 250-kg, and 100-kg caliber, cluster bombs, incendiary tanks, and S-8, S-13, and S-25-OFM rockets as well.

KNPAAPO

Su-30MK2 TNI AU

Su-30MK2


Su-30MK2 spesifikasi dasar
Mesin tipe 2 х AL-31F
Thrust, kgf 2 х 12500
Panjang, m 21,9
Wing span, m 14,7
Tinggi, 6,4 m
Max berat lepas landas, kg:
- Maks 34500
- Limit 38000

Max kapasitas bahan bakar internal, kg 9720
Max payload, kg 8000
Max kecepatan, km / h:
- Pada ketinggian tinggi 2100
- Di permukaan laut 1400
Max Mach nomor 2
Layanan langit-langit, m 17300
Max g-load9
Range, km:
- Tanpa pengisian bahan bakar dalam penerbangan
3000
- Dengan satu dalam penerbangan pengisian bahan bakar
5600
Jalankan dengan berat lepas landas normal, m 550
Roll dengan parasut drag dikerahkan, m 750


Double-kursi tempur.

Pesawat tempur multi-peran Su-30MK2 dirancang untuk mendapatkan keunggulan udara melalui bermusuhan membunuh berawak dan pesawat tak berawak dengan peluru kendali dalam pertempuran jarak menengah dan dogfights, dan permukaan (tanah dan laut) menghancurkan target dengan semua jenis senjata, pertama-tama dengan senjata presisi tinggi dalam individu dan operasi kelompok dalam kondisi semua cuaca. Pesawat ini dapat digunakan untuk pelatihan personil terbang untuk mengasah mereka terbang dan berkelahi keterampilan.

Bagian belakang-seater mengurangi beban kerja pilot dalam pertemuan PGM jangka panjang, dalam operasi malam hari dan misi berlarut-larut dengan pengisian bahan bakar dalam penerbangan.

Fitur utama dari pesawat tempur Su-30MK2 adalah sebagai berikut:

* Sistem pengendalian kebakaran meningkatkan membual peningkatan kemampuan permukaan-target;
* Sistem canggih kokpit manajemen;
* Navigasi yang ditingkatkan dan suite komunikasi;
* Lebih canggih pertahanan diri penanggulangan elektronik (ECM) suite;
* Udara diperluas-ke-udara dan udara-ke-permukaan suite senjata dengan persenjataan yang dipasang secara eksternal pada tanggal 12 cantelan;
* Sebuah in-flight sistem pengisian bahan bakar;
* Badan pesawat diperkuat dan landing gear menyediakan untuk operasi pesawat dengan beban max tempur dan kapasitas bahan bakar dengan take-off berat badan sampai dengan 38 nada.

Kontrol kebakaran sistem Su-30MK2 menyediakan untuk deteksi, pelacakan dan memukul dengan senjata onboard target udara dan permukaan sepanjang waktu dan dalam cuaca apapun.

Sistem pengendalian kebakaran terdiri dari dua subsistem utama:

api subsistem kontrol * untuk senjata udara-ke-udara termasuk sistem radar penampakan, sistem penglihatan optronic, dan sistem head up display;
api subsistem kontrol * untuk senjata udara-ke-permukaan menyediakan untuk penggunaan spektrum yang luas dari udara-ke-permukaan senjata presisi tinggi, dan untuk indikasi sasaran, tujuan dan data penerbangan navigasi di empat menampilkan multifungsi 4-х terletak pada panel instrumen cockpits '.

Andalan dari sistem manajemen kokpit empat warna multifungsi liquid crystal display (LCD) dan kepala up-display (di kokpit kedepan saja). Ini menampilkan tampilkan semua diperlukan target penunjukan digital dan visual, penerbangan dan navigasi data serta data mengenai status pesawat sistem. Seiring dengan LCD multifungsi, rumah-rumah panel instrumen instrumen elektromekanis tradisional, yang bertindak terutama sebagai backup.



Radar digunakan pada Su-30MK2 di keterlibatan udara-ke-udara memastikan sebagai berikut:

* Mencari target udara;
* Terdeteksi identifikasi target;
* Menyerang target dengan rudal jarak pendek menengah dan menampilkan panduan yang berbeda;
* Mencari, pengunci pada dan pelacakan target visual di dogfights.

Dalam mode udara-ke-permukaan, radar memastikan berikut:

* Semua-cuaca akuisisi dan positioning target permukaan radio-contrast;
* Permukaan data penetapan target pasokan untuk menyediakan Kh-31A, Kh-35E, dan Kh-59MK udara-ke-kapal aplikasi rudal.

Optik-elektronik penampakan sistem yang terdiri dari stasiun Optical lokasi dan Helm-sistem target sebutan mount (HMS). Lokasi Optical stasiun (OLS) Su-30MK2 adalah kombinasi dari pencarian inframerah dan sistem track (IRST) dan laser rangefinder / target penanda. Hal ini dirancang untuk melacak target udara baik di depan dan belahan belakang menggunakan inframerah tanda tangan mereka . Hal ini juga dapat digunakan untuk laser mulai dari target udara dan permukaan serta untuk menerangi target permukaan oleh sinar laser untuk peluru kendali udara-ke-permukaan dengan laser homing semi-aktif aplikasi kepala.

Suite senjata Su-30MK2 termasuk built-in GSH-301 30-mm automatic single-barrel tinggi tingkat-meriam-api dengan beban amunisi dari 150 putaran, rudal, roket dan bom yang dipasang secara eksternal pada tanggal 12 cantelan dibawah sayap dan pesawat .

Suite senjata udara-ke-udara termasuk rudal jarak menengah dari jenis-27 R - R-27T1, R-27ET1 rudal pencari panas, R-27R1, R-27ER1 radar-rudal homing semi-aktif, R-27P1 dan rudal R-27EP1; RVV-AE rudal jarak menengah radar-homing aktif, dan R-73E jarak pendek rudal pencari panas.

Pesawat tempur Su-30MK2 memiliki berbagai senjata dipandu dan terarah digunakan untuk menghancurkan target permukaan.

Udara-ke-permukaan senjata dipandu pesawat tempur Su-30MK2 terdiri dari Kh-59ME, Kh-35E dan Kh-59MK rudal, sedangkan jarak menengah Kh-31A berkecepatan tinggi anti-kapal rudal radar-homing aktif, sedangkan Kh-31p jarak menengah antiradar radar-homing rudal pasif; Kh-29T, TV-homing rudal Kh-29TE atau Kh-29L laser-homing rudal jarak pendek; bom TV-homing KAB-1500Kr dan-KAB 500Kr (KAB- 500-OD) bom dipandu.

KNAAPO/INDEFECE

SUKHOI 30MK TNI AU


Berikut adalah spesifikasi dan foto Su-30MK yg dimiliki  TNI AU



Su-30MK dasar kinerja
Double-kursi tempur
Mesin tipe 2 x АL-31F
Thrust, kgf 2 x 12.500
Panjang, m 21,9
Wing span, m 14,7
Tinggi, 6,4 m

Lepas landas berat badan, kg:
24.900 normal
maks. 34.500
batas 38.800

Bahan bakar kapasitas, 9.640 kg
Combat beban, 8.000 kg

Max. kecepatan, km / h:
di ketinggian 2120
permukaan laut 1350
Max. Mach 2
Operasional langit-langit, m 17300
Batas beban faktor 9

Rentang, km:
tanpa pengisian bahan bakar 3.000
dengan satu pengisian bahan bakar 5.200
Lepas landas berjalan (di berat lepas landas normal), 550 m
Landing roll (dengan rem parasut), 750 m

Deskripsi

Double-kursi tempur.

Pesawat tempur Su-30MK double-kursi multiguna merupakan modifikasi dari Su-27SK diproduksi serial sejak tahun 1999.

tempur ini dirancang untuk mendapatkan keunggulan udara melalui pesawat berawak dan tak berawak menghancurkan oleh peluru kendali jarak menengah di Pertunangan dan dogfights; laut dan menghancurkan target darat oleh semua jenis senjata pertama-tama dengan presisi yang tinggi sedangkan individu dan kelompok operasi di segala kondisi cuaca . Selain pesawat tempur yang dapat dioperasikan untuk melakukan pengintaian udara sedangkan laut dan operasi tanah serta awak pesawat, sementara pelatihan untuk mengoperasikan pesawat dan untuk memulai senjata. Pilot kedua membantu mengurangi beban pilot pertama, sementara pertempuran misi dengan aplikasi senjata jarak jauh, di malam hari, dan penerbangan panjang dengan in-flight pengisian juga.

Su-30MK memiliki kekhasan sebagai berikut:
senjata sistem kontrol diubah dengan kemampuan diperpanjang untuk menghancurkan target darat dan laut;
kokpit baru indikasi sistem dasar indikator LCD multifungsi;
upgrade navigasi dan sistem komunikasi;
EW upgrade sistem;
tata nama besar udara-ke-udara dan senjata udara-ke-permukaan yang dipasang di 12 poin keras;
in-flight sistem pengisian bahan bakar;
diperkuat kerangka pesawat dan pendaratan peralatan konstruksi yang memungkinkan pengoperasian pesawat dengan tangki bahan bakar penuh dan beban berat memerangi maksimal pada lepas landas hingga 38,8 ton.

Sistem kontrol senjata Su-30MK menyediakan deteksi, pelacakan dan menghancurkan udara, darat dan target laut di segala kondisi cuaca siang dan malam.

Ini terdiri dari dua bagian dasar:
senjata udara-ke-udara sistem pengendalian yang terdiri dari sistem penglihatan radar, optoelektronik sistem dan HUD penglihatan, dan kemampuan tambahan terhadap rudal anti-kapal Kh-31A memulai;
udara-ke-permukaan senjata sistem kontrol yang memungkinkan tata-nama besar meluncurkan senjata presisi tinggi untuk menghancurkan target darat, dan semua melihat refleksi data pada tanggal 4 MFD pada panel kontrol dalam cockpits.

Radar Su-30MK dapat dioperasikan di udara-ke-udara dan mode udara-ke-permukaan. Ini memastikan udara dan tanah deteksi target di segala kondisi cuaca siang dan malam.

optoelektronik meliputi sistem pengamatan lokasi sistem pengamatan optik dan helm mount designator target. Sistem peninjauan lokasi Su-30MK optik merupakan kombinasi dari pencari IR-arah dan pencari rangу laser, dan digunakan untuk mendeteksi dan melacak target udara dengan radiasi di depan dan belahan kembali, untuk rentang target udara dan tanah dengan bantuan dari sinar laser dan untuk menerangi target tanah dan menghancurkan mereka dengan udara-ke-permukaan dengan peluru kendali pencari laser semi-aktif.

Senjata Su-30MK terdiri dari GSH-301-api cepat udara 30-mm kaliber meriam dengan 150 putaran kartrid; rudal dan bom yang dipasang di 12 hard-poin di bawah sayap dan badan pesawat. Udara-ke-udara termasuk rudal R-27R1 (R-27ER1) dipandu rudal jarak sedang dengan pencari semi-aktif, 2 R-27Т1 (R-27EТ1) jarak menengah dengan rudal pencari panas, RVV-AE kisaran menengah rudal dengan radar pencari aktif, rudal R-73E pertempuran udara dengan pencari panas.

Senjata udara-ke-permukaan Su-30MK terdiri sampai dengan 6 rudal anti-radiasi Kh-31p dengan pencari radar pasif, sampai 6 Kh-31A rudal anti-kapal dengan radar pencari aktif, sampai dengan 6 Kh-29Т (Kh- 29ТЕ) rudal jarak pendek dengan TV-pencari atau Kh-29L dengan pencari laser semi-aktif, dua Kh-59МE rudal jarak sedang dengan pencari TV-diperintahkan dan hingga 6 КАB-500Kr atau 3 bom dipandu КАB-1500Kr dengan TV -berkorelasi pencari.

Senjata Su-30MK terarah dapat mencakup hingga 8 bom (bom cluster, tank pembakar) kaliber 500 kg, sampai dengan 28 bom kaliber 250 kg, hingga 32 bom kaliber 100 kg, dan sampai 80 rudal terarah S ketik empat unit B-8М1 (-8), 20 S-13 roket (di 4 unit B-13L), 4 roket S-25-ОFМ.

Sejarah

Biro Desain mulai bekerja untuk mengembangkan sebuah pesawat Su-30-berbasis untuk Angkatan Udara India pada tahun 1995. AF Barkovsky diangkat desainer kepala proyek ini. Pada 30 November 1996 perjanjian antar pemerintah dibuat untuk pembangunan bertahap dan pengiriman ke India dari 8 Su-30K dua-kursi pesawat tempur dan 32 Su-30MKI multi-peran dua-kursi pejuang. Pesawat dijadwalkan untuk pengiriman di beberapa kiriman, dengan peningkatan secara bertahap dari avionik, powerplant dan senjata. Kontraktor umum, sesuai dengan resolusi pemerintah, adalah:
- Untuk pengembangan pesawat: Biro Desain Sukhoi OJSC (sekarang JSC),
- Untuk produksi pesawat: Pesawat Irkutsk Asosiasi Produksi (IAPA, sekarang Irkut Corporation).

Dua prototip dibangun oleh Biro Desain di 1995-1998. Prototipe pertama, Su-30I-1, didasarkan pada versi Su-30 produksi, prototipe selesai pada musim semi 1997. Penerbangan pertama dilakukan oleh pilot uji V.Yu. Averyanov pada tanggal 1 Juli 1997. Pada bulan Juli 1997, Biro Desain meluncurkan program untuk menguji pesawat bersama-sama dengan SPFC Angkatan Udara.

Pesawat telah diproduksi di Irkutsk sejak tahun 2000. Pesawat pra-produksi pertama penerbangan diuji di pabrik oleh V.Yu. Averyanov pada 26 November 2000. Tiga pertama pra-produksi Su-30MKIs diserahkan kepada Biro Desain dan telah digunakan bersama dengan prototipe dalam program bersama-pengujian dengan SPFC dari Angkatan Udara.

Sesuai dengan persyaratan dalam kontrak, pesawat-pesawat Su-30MKI itu harus diuji dan disampaikan dalam 3 tahap. Pengiriman pertama dari 10 Su-30MKIs kepada Nasabah terjadi pada tahun 2002; tahap kedua dari 12 pesawat terbang, pada tahun 2003. Pada tahun 2004, Su-30K dan Su-30MKI pesawat telah dimasukkan ke dalam layanan dengan dua skuadron dari Angkatan Udara India.

Su-30MKI yang khas fitur:
- Untuk pertama kalinya di dunia, sebuah pesawat produksi memiliki daya dorong mesin dengan kontrol vektor (AL-31FP, dikembangkan oleh RDC dinamai A. Lyulka), dan sistem remote control diintegrasikan ke dalam sebuah loop kendali tunggal. Secara bersama-sama, ini menyajikan Su-30MKI sangat yg dpt digerakkan;
- Untuk pertama kalinya dalam sejarah Biro Design, pesawat fitur integrasi skala besar sistem avionik asal asing dan domestik.
Su-30MKI memiliki "internasional" portofolio avionik, termasuk seperti halnya sistem dan unit dibuat oleh 14 perusahaan asing dari 6 negara di dunia.
- Untuk pertama kalinya di dunia, sebuah pesawat produksi memiliki radar dengan PAA ("Bar" yang dikembangkan oleh Institut Riset Ilmiah Teknologi Instrumentasi). Selain itu, pesawat memiliki kursi ejeksi baru, K-36D-3.5, dan sejumlah sistem inovatif lainnya berasal dari dalam negeri.
- Garis ADO-up telah ditingkatkan secara signifikan dengan penambahan udara RVV-Aye-udara ke-peluru kendali, Kh-29L/T/TYe, Kh-31A / P, Kh-59M udara-ke-tanah rudal, dan-KAB-1500 500 dan bom dipandu KAB.

Program Su-30MKI memiliki untuk pertama kalinya dalam sejarah Rusia memamerkan model baru bagi kerjasama militer-teknis menggabungkan semua jenis kerja sama jangka panjang saat ini dipraktekkan di dunia seperti:
- Pengiriman pengiriman pertama produk dalam versi awal (Su-30K),
- R & D bersama untuk menghasilkan versi upgrade (Su-30MKI),
- Pemberian pelanggan lisensi untuk memproduksi dengan penggantian komponen berikutnya buatan Rusia dengan yang asal asing (pada bulan Desember 2000, kontrak ditandatangani untuk menjual ke India lisensi untuk memproduksi 140 pesawat Su-30MKI dari kelompok tujuan akhir),
- Peningkatan kemampuan pesawat dari pengiriman pertama status teknis kelompok tujuan akhir,
- Menyiapkan sebuah layanan kerjasama teknis untuk aftersales pemeliharaan peralatan yang disediakan,
- Menggunakan ekspor «tempat berpijak» untuk memperluas ke pasar regional (di tahun 2003, kontrak dibuat untuk memasok pesawat Su-30MKM ke Malaysia).
Sumber: KnAAPO , dan Sukhoi   
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Perbedaan Antara Su-27 SK dan Su-27 SKM


su 27skm
Mulai tahun 2002 Su-27 SK dikirim ke pabrik KnAAPO (Komsomolsk-on-Amur Aircraft Production Association) untuk berubah wujud menjadi Su-27 SKM. Beberapa peningkatan kemampuan dilakukan pada Su-27 SK sehingga menjadi Su-27 SKM. Antara lain meliputi beberapa hal. Pertama perbaikan dan peningkatan sistem kontrol tembakan. Su-27 SKM tidak lagi hanya berkemampuan air to air, tetapi juga air to ground. su 27skmKedua, mengganti panel-panel kuno dikokpit dengan avionik layar kaca berupa tiga MLD (Multifunction Liquid-crystal Displays) serta HUD (Head-Up Displays) Ketiga, peningkatan sistem navigasi yang terintegrasi dengan sistem satelit GLONASS dan NAVSTAR. Keempat, penggunaan RWR (Radar Warning System) untuk memandu rudal antiradiasi KH31P. Peningkatan IRST (Infrared Search and Track Devise) dengan penjejak laser untuk melepaskan rudal laser-beam riding juga dilakukan.
Kelima, peningkatan kemampuan bawa senjata sehingga Su-27 SKM dilengkapi rudal air to air RVV-AE active radar homing, rudal air to ground Kh-29T(TE), Kh-29L, Kh-31P, Kh-31A, serta bom berpemandu KAB-500Kr dan KAB-1500Kr. Semua persenjataan ini dibawa dalam 10 cantelan (external stores). Untuk konfigurasi combat load, persenjataan Su-27 SKM mencakup 6 rudal RVV-AE, empat rudal air to ground atau empat bom berpemandu masing-masing 500 Kg atau satu bom berpemandu dengan bobot 1.500Kg. Su-27 SKM juga tetap membawa beragam persenjataan (rudal maupun roket) yang diaplikasikan pada Su-27 SK.
Keenam, peningkatan yang cukup signifikan pada Su-27 SKM adalah dilengkapinya pesawat dengan alat pengisian bahan bakar di udara (refuelling system). Dengan adanya perangkat ini SU-27 SKM yang berkursi tunggal itu bisa terbang lebih lama lagi dan menjelajah lebih jauh.
Sumber: Angkasa edisi 1 Oktober 2008

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