- Minimizing the station's door opening and closing time to support drones' quick entry and exit. - Structural design to minimize noise and vibration when opening and closing the door - Design and implementation of an interface for interaction between an automatic door system and a drone. - Automatically opening and closing door system - Automatic detection of drones through cameras and sensors, and safe storage and charging functions

The APA-10 is a hybrid GPU equipped with diesel engine for continuous power and batteries for engine starting mode. Lightweight and maneuverable, the unit is perfect for indoor and outdoor use. Its relatively small size and extreme agility allow bringing the rectifier to any desired position. The elegant casing is made out of composite material, providing it long life and comfort to the user. The intuitive interface is user-friendly, making the GPU easy to control. Equipped with a highly durable chassis and mechanical braking system, this GPU is well prepared for heavy-duty and harsh conditions. The Ultra Green Power Solution Battery and Diesel engine driven GPU series APA is designed to reduce CO2 emissions with its unique technical characteristics.

< Frequency Range > ● 2500 ~ 6000 MHz < Output Power (W) > ● 35 < Gain (db) > ● 46 < Power Supply (V) > ● 30 < Current (A) > ● 10 < Dimension > ● 175.3 x 91.4 x 28 (mm)

EO/IR Payload System EOTS (Electro-Optical Tracking System) is an electronic optical image tracking device that identifies danger and emergency situations on the battlefield, monitors and tracks tragets, and calculates their coordinates, and is an essential equipment for drones that can be used in both military and private sectors. M1 and M2 were developed to use a common mount that connects to the drone by keeping the size of the gimbal assembly the same at 4 inches. M1 can be recognized at a maximum of 0.2km for humans during the day and at night, and M2, which operates in adverse conditions at night, can be recognized at up to 1.0km for tanks in the form of IR continuous zoom.

Near-field Ranges calculate Far-field pattern based on amplitudes and phase samples in radiating near-field region mathematically. Near-field Ranges have various testing configurations-planar, cylindrical and spherical. Planar Near-field range is suitable for directional antennas. Cylindrical Near-field range is suitable for antennas with wide side/back lobes and fan beam antennas. Spherical Near-field Range is suitable for any type of antennas. You can choose reasonably defending your conditions. MTG has many experience supplying Far-field ranges as well as Near-field ranges. MTG work with many companies including munitions industries, laboratories, telecommunication corporations, and antenna corporations. We can provide a series of positioner, probes and Near-field measurement software.

This cable assembly is applied to various precision and high-function facilities and equipment such as armored vehicles, warships/ship, medical equipment, and communication equipment to perform power connection and electronic signal connection functions. Military cable assemblies are vital for the defense and aerospace industries. Cable assemblies must be built with high-performing materials and components that withstand harsh conditions, such as vibrations, high temperatures, and chemical exposure.

- Application of patented expansion technology to resolve narrow space operation. - Equipped with camera function utilizing foldable mast. - Drone take-off and landing system using internal lift. - Equipped with a monitor for situational identification and a console for drone operation control.

CATIS™ is an ultra-high-resolution, small satellite imaging radar device independently developed by Lumir. It consists of three components: the radar signal transmission/reception device SCEU, an active phased array antenna SATA, and a data downlink antenna KaPA. This X-band imaging radar device is designed for small satellites weighing 150 kg, offering an ultra-high resolution of 0.3 m. It transmits wideband RF signals to the observation area while orbiting at an altitude of 500 km and receives the reflected signals to acquire Earth observation data.