UAVS UVM-R1 / R2
Multipurpose Use
Unmanned Aerial Vehicle
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General InformationKIS renowned capabilities include all life cycle phases of its systems. It has an organizational and technological structure in all stages after the emergence of the system idea, research and product development, production and after-sales activities. Our Research and Development capabilities in affiliation with engineering teams from ODTU (Middle East Technical University) include the complete design and development of UAV systems, aerial platforms and ground components with their subsystems. In addition to that, our activities are carried out according to the relevant military and civilian standards.
Fully in-house Tailor-Made Designed UAV systems are manufactured with their subsystems and components, integrated and offered to service after passing the detailed testing and quality control stages. In our production activities, modern machines and equipment are used for high technology production. 3 and 5-axis advanced CNC machines, automatic assembly machines, autoclaves wide enough to produce long parts such as wings, composite furnaces and high precision measuring devices of various sizes are among the important equipment in our production area.
KIS envisions and has inspiration to build the most advanced technological systems on the global stage by advancing unmanned aerial systems. In line with their principles, we strive to ensure as independent, Turkey-centric a technology stack as possible. We further attempt to dovetail emerging high technology with mission-critical functions to offer our armed forces systems that are reliable, integrated, and complete.
Approvals
These products meet the requirements of the European Community Directives EU Regulations 2019/947 and 2019/945 set out the framework for the safe operation of drones in the European skies.
Specifications
TECHNICAL SPECIFICATION OF UAVS UVM-2E
1.1 The UAV UVM-2E is designed to deliver a container with a payload weighing up to 3 kg. to the coordinate specified by the operator or from the video image from the on-board, thermal night time and daytime video camera.
GENERAL R1-R2
Aerial Vehicle Technical Specifications
Number of Rotors 4
Propeller Specifications 32x11
Ammunition Capacity Attack : 2 x 60mm / 1 x 82 mm
Data and Video Link 30 km
Autopilot YES
Flight Time 30 min with 3.5 kg payload
Cruise Speed 35 km/h
Max Speed 60 km/h
Flight Range More than 15 km (Radius)
Length (With Propeller) 2012 mm
Length (Without Propeller) 1200 mm
Rotor Diameter 812 mm
Wind Resistance 13 m/s
Battery 4 x 24V 22AH (LiPo Battery)
Charger 2 x FAST Charger with 4 slots total
Max. Altitude 6000 m MSL Max
Payload 10 kg
MTOW 32 kg
Max. Climb rate 3 m/s
Max. Descent rate 3 m/s
Max wind resistence 35 km/h
Operational range >15 km
Practical ceiling 1000 m
Endurance 30 min with 2kg payload
Onboard power supply 48 V - 24 V - 12 V - 5 V
Temperature range -40°, + 60 ° C
Base takeoff and landing area 3m x 3m
Take off and landing Fully Autonomous
Portable GCS YES
Dustproof and waterproof YES
IP65 Rugged Case YES
GPS Anti-Jamming - Anti-Spoofing Options
GPS Anti-Jamming - Anti-Spoofing Option Tualaj Anty / 4100 / 8200
Camera Systems
Daytime Camera with Zoom (R1) 10X Optic Zoom 3x Digital Zoom 30x Hybrid Zoom0X Zoom
Day time Camera Daytime Camera with Zoom (R2) 3840x2160 (ch1) / 1920x1080 (ch2) Optical Zoom (R2) 14X Optical Zoom Thermal Camera (R2) 704x576 Thermal / -20 to +550 C Measuring Range Recording (R1-R2) 2K (R1) 4K (R2)
Ground Station Ruggedized System YES
Tracker Antenna 360 YES Battery YES
Keyboard Stainless Steel + Trackball
Mission Control & AUTO Pilot
Software Specifications
Automatic Take Off & Landing YES
Automatic Return To Base YES
Blind Flight Control without GPS YES
Fleet Flight Feature Optional
Video Log & Transmit At Line Of Sight YES
Interactive Mission & Flight Planner YES
Inertial Navigation OPTIONAL
Mission Cancel/Modify YES