View attachment 72149
I have a preliminary check of what the Kizilelma PT3 drone is likely to have installed.
Engine:
Ivchenko Progress AI322-30F Technical specifications:
Type: Two-stage low-bypass turbofan
Length: 1,960 mm
Diameter: 640 mm
Weight: 440 kg (without afterburner), 560 kg (with afterburner)
Thrust:
2,500 kgf (24.5 kN) without afterburner
4,200 kgf (41.2 kN) with afterburner
Bypass ratio: 1.19:1
Pressure ratio: 15.43:1
Fuel consumption:
0.66 kg/kgf/h without afterburner
1.9 kg/kgf/h with afterburner
Thrust-to-weight ratio:
5.68 (without afterburner)
7.5 (with afterburner)
Expected thrust ratio in the Kizilelma PT3 drone with AI322-30F engine: 0.7
Will be replaced in the long term with the TEI TF-6000/10000 engine with a thrust ratio of 0.8
Kizilelma C with double engine, which is probably planned as the final version of the drone, would probably have a thrust ratio of 1.2-1.3
Radar: MURAD 200A AESA radar
Technical specifications:
Frequency band: X-Band
Transmit/receive modules: Over 1000 individual modules
Power per module: Standard 20 W, maximum 30 W
Total pulse power: 23 kW as standard, maximum 34.5 kW
Cooling: Liquid-cooled
Functions:
Air-to-air modes: long-range search, multi-target tracking, interphase guidance, weather detection, aerial combat maneuvers
Air-to-ground modes: strip SAR, point SAR, terrain mapping, moving ground target detection and tracking, maritime search and ISAR, air-to-ground ranging, Doppler beam sharpening, automatic altitude determination
Additional capabilities:
Multifunctional radar with simultaneous air-to-air and air-to-ground operations
Non-cooperative target identification
Automatic target recognition
Interference immunity
Electronic support and attack capabilities
Electro Optical Sensor System (ETOS):
ASELSAN TOYGUN 100 ETOS
Technical Specifications:
HD MWIR thermal vision: utilizes a high-resolution MWIR detector with a resolution of 1280x1024 pixels.
Laser rangefinder and target illuminator: Operates at a wavelength of 1064 nm and a range of up to 35 km. Complies with NATO standard STANAG 3733.
Multiple target tracking: Ability to track multiple targets simultaneously.
Automatic target recognition: Enables automatic identification of targets.
Laser dot tracking: Can detect and track targets marked by other platforms.
Compatibility: Suitable for air-to-air and air-to-ground operations.
Operating temperature range: -40°C to +70°C.
Infrared search and tracking system (IRST): ASELSAN KARAT 100
Technical specifications:
The KARAT 100 is an infrared search and tracking system (IRST) developed by ASELSAN for manned and unmanned combat aircraft, helicopters and unmanned aerial vehicles. It enables the passive detection and tracking of airborne targets using infrared technology.
Detector resolution: 640 x 512 pixels with 15 µm pixel size
Wavelength range: Long-wave infrared (LWIR)
Fields of view:
Narrow: 4.0° x 3.2° (horizontal x vertical)
Wide: 8.0° x 6.4° (horizontal x vertical)
Volume scan duration: ≤ 30 seconds
Communication/video interface: Fiber Ethernet
Power supply: 28 VDC according to MIL-STD-704F
Operating temperature range: -46°C to +70°C
Storage temperature range: -54°C to +71°C
Cooling: Liquid cooling
Superior detection range for modern fighter aircraft
Faceted design to reduce the radar cross-section
Customizable search volume
Automatic target detection and tracking in the search area
Single and multiple target tracking
Alignment with the platform's line of sight
Narrow and wide fields of view
Angular position information for detected targets
Passive range estimation for detected targets
Digital video output
Advanced image processing
Precise stabilization
Distributed Aperture System (DAS):
ASELSAN DAS
Technical specifications:
ASELSAN DAS is an advanced infrared sensor system that provides 360-degree all-round visibility for aircraft. It enables simultaneous detection and tracking of threats from all directions, including aircraft, missiles and drones.
Key features of the ASELSAN DAS:
All-round visibility: the system utilizes multiple infrared sensors strategically positioned around the aircraft to provide complete 360-degree coverage.
Threat detection: It detects and tracks potential threats in real time, enabling early warning and response.
Situational awareness: Integration with the cockpit display provides pilots with enhanced situational awareness, supporting decision making in critical situations.
Integration: The DAS can be seamlessly integrated into existing avionics systems and works with other sensor systems to provide comprehensive threat analysis.
Application: It is suitable for various platforms, including fighter aircraft, helicopters and unmanned aerial vehicles (UAVs).
The ASELSAN DAS contributes significantly to increasing the survivability and effectiveness of aircraft in complex operational scenarios.
Missile Approach Warning System (MAWS):
ASELSAN IRIS 100
Technical specifications:
The İRİS-100 is a Missile Approach Warning System (MAWS) developed by ASELSAN and specially designed for use on aircraft. It is used for the early detection and tracking of infrared-guided missile threats and thus increases the survivability of airplanes and helicopters.
Main features of the İRİS-100:
Detection in the UV range: the system detects the exhaust jets of approaching missiles in the "solar blind" UV band, resulting in lower jamming sensitivity.
High sensitivity: Enables the detection of threats over long distances.
Early threat warning: Declares and tracks threats as early as the launch phase of the missile.
Visual and acoustic warnings: Informs the pilot of detected threats both visually and audibly.
High probability of detection: Provides reliable identification of threats.
Precise angle determination: Provides accurate information about the direction of arrival of the threat.
Multiple target tracking: Can detect, track and declare multiple threats simultaneously.
Fast response time: Short declaration time enables timely activation of countermeasures.
Low false alarm rate: Minimizes the number of false alarms.
Flexible system configuration: Can be equipped with 4 to 6 sensors; spherical coverage is achieved with 6 sensors.
High reliability: Has a high mean time between failure (MTBF).
Spectral range: Solar Blind UV
Field of view:
With 4 sensors: ±45° elevation x 360° azimuth
With 6 sensors: Full spherical coverage
Communication interface: MIL-STD-1553 / RS-422
Power consumption: Less than 14 W per sensor unit
Operating temperature: -40°C to +71°C (according to MIL-STD-810E)
Storage temperature: -55°C to +85°C (according to MIL-STD-810E)
Cooling: No special requirements
The İRİS-100 has been extensively tested and has proven itself in use. It is suitable for various airborne platforms and provides effective protection against infrared-guided missile threats.