Su-27
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The Su-27SK aircraft was created on the basis of the Su-27, one of the best fighters in its class; mass-produced in Komsomolsk-on-Amur.The Su-27SK aircraft is a highly maneuverable fighter designed to gain air supremacy, as well as to strike ground targets with unguided ASPs.
Flight performance
Takeoff weight: |
|
Maximum landing weight, kg | 21000 |
Maximum landing weight, kg | 23000 |
Maximum fuel supply in internal tanks, kg | 9400 |
Maximum payload weight, kg | 4430 |
Practical ceiling (without hangers), km | 18.5 |
Maximum flight speed near the ground (without hangers), km/h | 1400 |
Maximum number M (without hangers) | 2.35 |
Maximum operational overload | nine |
Maximum flight range (with missiles 2xR-27R1, 2xR-73E with launch at halfway): |
|
Maximum flight duration, h | 4.5 |
Takeoff run at normal takeoff weight, m | 450 |
Run length at normal landing weight (with brake parachute), m | 620 |
Aircraft dimensions: |
|
Number of crew members | one |
Power point | |
Number and type of engines | 2xAL-31F |
Thrust: |
|
Main avionics | |
1. Weapons control system: | |
1.1. Radar sighting system | |
1.2. Optoelectronic sighting system with a helmet-mounted target designation system | |
1.3. Single display system | |
1.4. State identification system interrogator | |
1.5. Weapon control system | |
2. Remote control system | |
3. Responder of the state identification system | |
4. Antenna-feeder system | |
5. Piloting and navigation system consisting of: | |
5.1. Navigation system consisting of: | |
5.1.1. Digital computer | |
5.1.2. Information complex of vertical and course | |
5.1.3. Radio engineering system of short-range navigation (RSBN) | |
5.1.4. Automatic radio compass | |
5.2. Automatic control system | |
5.3. Information complex of altitude and speed parameters | |
6. Satellite navigation system | |
7. Marker radio | |
8. Electronic countermeasures | |
8.1. Exposure warning station | |
8.2. Chaff and LTC reset device | |
8.3. Active interference station (in a container) | |
9. Complex of communication facilities, including | |
9.1. Communicated radio station MV-UHF range | |
9.2. Communicated radio station MV-UHF range | |
9.3. Communication radio station HF band | |
9.4. Telecode communication terminal equipment | |
10. Onboard automated control system | |
10.1. Generalized built-in control and crew warning system | |
10.2. Flight information recording equipment with operational storage | |
10.3. Airborne emergency warning equipment | |
10.4. Alarm system | |
10.5. Flight registration device | |
11. Aircraft transponder | |
Resources | |
Aircraft resource: | |
- appointed, h | 2000 |
- before the first overhaul, h | 1000 |
- service life, years | twenty |
Resource of the engine and remote box of units: | |
- before the first overhaul, h | 300 |
- assigned resource, h | 900 |
*May vary depending on the configuration of the equipment installed at the request of the customer
Armament
1. Cannon armament | Built-in gun mount 30 mm, 150 rounds of ammunition |
2. Air-to-air guided missiles | R-27R1(ER1) R-27T1(ET1) R-73E |
3. Unguided projectiles | S-8KOM, S-8OM, S-8BM S-13T, S-13OF S-25OFM-PU |
4. Air bombs of caliber, kg | 100, 250, 500 |
5. Disposable bomb cassettes | RBC-500 |
6. Outboard fuel tanks | not installed |
7. Number of suspension points | 10 |
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