ARMSNET
Military Equipment Database
Initializing 0%

ŞİMŞEK Turkish Unmanned Aerial Vehicle (UAV)

ŞİMŞEK

Tactical Unmanned Aerial Vehicle (UAV)
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
ŞİMŞEK Turkish Unmanned Aerial Vehicle (UAV)
Designation
ŞİMŞEK
Alternate Designation
ŞİMŞEK
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Turkish Aerospace
Date of Introduction
2012
Description

The ŞİMŞEK Turkish Unmanned Aerial Vehicle (UAV) is engineered to fulfill the requirements of high-speed target drone operations that simulate enemy aircraft and missiles. This system is applicable for air-to-air, ground-to-air, and anti-aircraft gunnery and missile system training. Key specifications include: - An open architecture design that allows for modifications in accordance with user specifications. - An operational endurance of 45 minutes. - A maximum speed in excess of 350 knots. - A mission altitude range from 50 feet (15 meters) to 25,000 feet (7,600 meters) above sea level. - A 120 km Line of Sight (LOS) Data Link Range utilizing a Ground Control Station (GCS). - Capability for launch via catapult or release from aircraft wings. - A parachute recovery system suitable for both terrestrial and maritime environments. - The ability to take off and be operated from naval platforms. - A structure manufactured using advanced composite materials. - Compliance with military standards. - Full autonomous flight capabilities, inclusive of take-off and landing, facilitated by an indigenous Flight Control System and Autopilot System integrated with the GCS. - Preprogrammed flight abilities that enable waypoint assignments and modifications during or prior to flight. - Return Home and Fail-Safe Modes for automatic recovery to a predetermined point of return. - Recording and playback functionalities for real-time coded digital flight data telemetry. - Digital mapping capabilities featuring dynamic movement options. - A Passive Radar Cross Section Augmenter using a Luneberg Lens. - An Active Radar Cross Section Augmenter. - A Miss Distance Indicator (MDI). - An Infrared Signature Augmenter (Hot Nose). - An Automatic Identification System (AIS). - A Smoke Generator. This comprehensive system is designed to enhance training and simulation for diverse military applications, demonstrating advanced technological capabilities and operational effectiveness.

Air & Air Defense Specifications
Max Speed 648.2 km/h
Range 700.0 km
Endurance 50.00 hrs
Service Ceiling 7620 m
Wingspan 1.60 m
Payload Capacity 17 kg
System
Alternate Designation ŞİMŞEK
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Turkish Aerospace
Payload Capacity 17 kg
Features **Features:** - Fully Autonomous Flight - Take-off from Launcher or Airborne Carrier - Parachute Recovery System - Reconfigurable Payload Options Based on Mission Requirements - Electronic Warfare Precautions - Pre- and In-Flight Mission Planning and Update Capabilities - Return-to-Base (RTB), Emergency, and Automatic Landing Modes - Encrypted Digital Flight Data Recording - Swarm Technologies Integrated with Artificial Intelligence (AI)
Payloads Payloads: Active and Passive Radar Cross Section Augmenter, Miss Distance Indicator (MDI), Infrared Signature Augmenter (Hot Nose), Countermeasure Delivery System with Chaff and Flare, Camera, Controlled Reception Pattern Antennas (CRPA).
Dimensions
Length 2.3 m
Height 0.7 m
Wingspan 1.6 m
Maximum Takeoff Weight 70 kg (up to 90 kg from airborne carrier)
Automotive
Engine Name INA
Engine Type INA
Engine Power INA
Maximum Speed 648.2 km/h
Datalink Range 150 km (LOS)
Maximum Range 700 km
Service Ceiling 7,620 m
Endurance 50 min
Details
Country of Origin Turkey
Category UAVs
Air > UAVs
Filter Label
Ş
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.3 m
Width
1.6 m
Height
0.7 m
Weight
70 kg
Operators (1)
Turkey
Something went wrong. Please reload the page. Reload