The ACTUS® CORE-1 Dot Sight is a high-performance optical device chosen as the Warrior Platform Selection Equipment by the Republic of Korea Army (ROKA). Built to MIL-SPEC standards, it meets rigorous military requirements, including extreme temperature resistance, shock testing, waterproofing, and protection against fluid contamination. Designed for durability and reliability, the CORE-1 enhances operator safety in the field, ensuring quick and precise target acquisition during critical missions.

The 200W High Power Amplifier is an L-band amplifier that delivers 200W output with a 60% duty cycle. It provides a gain of over 53 dB, with output flatness of 2 dB depending on the input signal level. At maximum output, it offers ACLR performance of -20 dBc. With a built-in output-stage bandpass filter (BPF), it achieves excellent harmonic suppression of -70 dBc. Built-in monitoring functions include output signal and temperature monitoring.

Dual function pressure and temperature transducer

From the rocket launcher to its upper assembly, the bomb rack unit, completing a full weapon system as one set. The rocket launcher is a weapon system independently designed to launch guided missiles or rockets through 7-tube and 19-tube launchers, enabling both single and multiple firings. Through its development, independence of the weapon system has been secured, and structural stability has been achieved by applying a design that considers aircraft vibration and aerodynamic effects. In addition, it is equipped with the capability to receive the system’s firing signal and ignite the rocket. Based on the successful development in 2017 of the 7-tube 2.75-inch rocket launcher assembly for helicopters, the company is now independently developing upgraded versions of the 7-tube and 19-tube rocket launcher assemblies. Through this effort, we are securing scalability for application to next-generation helicopters and UAV systems.

The mRO-50 Ruggedized is a breakthrough microwave optical double resonance (MODR) low SWaP-C Miniaturized Rubidium Oscillator designed to meet the latest commercial, military and aerospace requirements where time stability and power consumption are critical. It provides a one day holdover below 1µs and a retrace below 1E-10 in a form factor (50.8 x 50.8 x 20mm) that takes up only 51 cc of volume (about one-third of the volume compared to standard rubidiums) and consumes only 0.36W of power, which is about ten times less than existing solutions with similar capabilities. The mRO-50 Ruggedized Oscillator provides accurate frequency and precise time synchronization to mobile applications, such as military radio-pack systems in GNSS-degraded or denied environments. Its wide-ranging operating temperature of -40° to +80°C is also ideal for: Underwater Applications, Military Communications, Radars, Low Earth Orbit, Electronic Warfare, Airbornes & Avionics, UAV/UGV/USV/UUV

- 1 axis Fiber Optic Gyroscopes - Bias Repeatability: 0.1°/hr - Bias Stability: 0.02 °/h (1,000 sec) - Angle Random Walk: 0.005 °/√hr - Scale Factor Accuracy: 500 ppm - Operating Voltage: 5 V (1 A) - Interface: RS422 Weight: 1.0 kg EMC: MIL-STD-461E

Currently in the final stages of development. Compact engine of a simple design and small frontal diameter, fuel lubricated, equipped with a BLDC starter-generator. Excellent thrust-to-weight ratio. Pyro ignition (optional).

Digital mission engineering tools connect every stage of the engineering product lifecycle, from initial design to operation. They enable reality-based 3D simulation across multi-domain environments such as air, space, land, and sea by incorporating high-resolution terrain, satellite orbits, RF and radar systems, and sensor environments to accurately replicate real mission conditions. With accurate dynamics-based physical models at the core, these tools provide quantitative analysis of relative positioning between systems, changes in altitude and attitude, line-of-sight availability, and communication link status. Users can predict and evaluate mission elements such as sensor operations, communication links, platform maneuvers, and orbit optimization through scenario-based simulations.