This rocket nozzle featuring conformal cooling channels and isogrid ribbing was manufactured using EOS Copper CuCP, a pure copper material optimized for additive manufacturing. The production required approximately 72 hours, taking advantage of the exceptional thermal and electrical conductivity of pure copper to meet demanding aerospace performance requirements. As one of the few companies in Korea capable of performing metal additive manufacturing with pure copper, we provide advanced technical expertise and support OEM production as well as collaborative technology development projects with various industrial partners. The showcased component was designed by nTopology and demonstrates the synergy of advanced design optimization with state-of-the-art copper additive manufacturing.

We have been designing and supplying cryogenic turbines for helium liquefaction since the late 1980s. Today we are a major supplier of turboexpanders, compressors and pumps to the world's leading manufacturers of cryogenic systems. Our cryogenic product line utilizes the unique PBS technology and know-how of dynamic gas bearings. We supply to prestigious research institutes such as CERN, Max Planck Institute or Rosendorf Research Centre. With the new HEXT/CTE300 turboexpander we will be ready for the hydrogen ecosystem

The CZ600IP is a high-performance un-cooled LWIR thermal camera engineered to deliver professional-grade imaging and system integration. With a 640x480 resolution and 12μm pixel pitch sensor, it provides exceptional clarity and detail, even in low-contrast environments. Its motorized focus and zoom control ensure smooth and accurate long-range observations, making it ideal for applications that demand both precision and flexibility. The camera’s wide temperature measurement range further enhances its utility, supporting reliable operation in industrial process monitoring, facility security, and advanced research projects.
Equipped with modern networking features, the CZ600IP supports Gigabit Ethernet connectivity, H.265/H.264 compression, and OnVif Profile S compliance, ensuring seamless integration with existing surveillance and monitoring systems. It also offers multi-streaming capabilities and advanced security protocols, allowing safe and efficient deployment in critical infrastructure. By combining robust imaging technology with flexible system compatibility, the CZ600IP stands out as a versatile solution that adapts to evolving customer needs while maintaining high reliability and accuracy.

Our products serve the clients in military and aerospace industries, who require high performance with strength and ability to perform at extreme temperatures and pressures.

The SCFAN-CTRL-10U is an internal fan control module installed inside the chassis to provide advanced cooling control and system thermal management. It integrates with FAN trays and operates through Kontron’s Power Supply Control Module (PSCM), supporting up to two 12V @ 3.5A fans and seven 12V @ 2.5A fans. This module ensures stable cooling performance and system reliability for high-density VPX-based embedded systems. It is deployed in the M-SAM-II multi-function radar system, where it provides precise and efficient cooling control for mission-critical radar operations.

- Integrated control of two zones: engine bay and crew bay - Equipped with a self-diagnostic function for key AFSS components - Capable of interfacing with the vehicle computer - Adjustable temperature setting for engine bay fire detection

FMP is built around Moog’s world-renowned military motion control technology. Options include integration of Moog’s high-performance stabilization and weapon stores management systems (SMS), providing missile firing capability to suit any mission. Missiles previously only launchable from helicopters may now be fired from ground vehicles with missile combinations able to suit any mission need from any platform.

Heat engine that converts combustion energy into mechanical energy. It consists of a compressor, combustion chamber, and turbine, and is widely used in aircraft propulsion.