This Control Actuation System (CAS) is a guidance system for unmanned flying objects. It consists of three MPS fin actuators that each independently position an aerodynamic fin. The maximum angle of incidence is ±8°, which allows the device to carry out highly precise dynamic manoeuvres. The miniature fin actuators that make up this Control Actuation System are manufactured by MPS Microsystems and were designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, these fin actuators meet strict requirements in terms of performance, weight - less than 100 g - and dimensions. To reduce the length of this actuator, MPS Microsystems used part of the screw length as the motor axis. This screw is equipped with a very compact 4-point contact bearing that simultaneously absorbs axial and radial loads. The angular play on the aileron axis is less than 0.1° rms. This actuator meets the storage and vibration requirements of military equipment.

The nose wheel assembly refers to the complete integrated unit consisting of the wheel, tire, axle, bearings, and associated structural components. In some configurations, it also includes steering mechanisms, shock absorbers (oleo strut), and braking systems (for specific aircraft types). The assembly is engineered for durability, precision, and reliability, enabling the aircraft to safely absorb impact forces during landing and provide accurate steering during taxiing.

A cost-effective and reliable EO/IR solution designed for unmanned platforms, combining compact design with strong performance. The system integrates QVGA/VGA-class infrared sensors and 2–20 megapixel EO cameras, providing versatile options to meet different operational requirements. o Infrared (IR) Sensor: QVGA/VGA resolution, optimized for detection and recognition in short-to-mid range surveillance o Electro-Optical (EO) Module: 2MP–20MP visible light cameras with high-resolution imaging, adaptable to multiple mission profiles o Design Philosophy: Lightweight, compact, and robust for integration into unmanned aerial vehicles (UAVs), unmanned surface vehicles (USVs), and ground robotics o Key Value: Balances price competitiveness, system reliability, and modular scalability for mass deployment

Kia developed Granbird Bare Chassis Vehicle based on long-accumulated technology and infrastructure for commercial vehicles. This Granbird Bare Chassis vehicle can be easily modified as specialized vehicles on the basis of diverse customer requirements.

In order to guarantee the quality required by customers based on excellent quality and productivity, we practice close quality control through SQ and IATF16949 certifications and devote ourselves to put all of our capabilities so that we would earn customers’ recognition.

The ECL2000 is a small cell developed for the U.S. CBRS market, providing seamless private network service in indoor environments such as homes or offices.

An Angle of Attack (AOA) indicator is a flight instrument that shows a pilot the angle between the aircraft's wing and the oncoming air, providing a crucial safety margin by warning of an approaching aerodynamic stall. Unlike airspeed. A Vertical Speed Indicator (VSI), also known as a Rate of Climb and Descent Indicator (RCDI) is an instrument which indicates the rate of climb or descent of an aircraft. These devices are installed and compatible with F-16 series aircraft and KAI's T-50/FA-50 series aircraft.

The ENS4000(Sub-6 5G Outdoor base station) is designed for outdoor services in the n79 (4.7GHz) band, providing coverage on the kilometer scale and enabling seamless private 5G service even in outdoor environments.