Safran Engineering Services was selected by Honeywell for the STC development for multiple rotorcrafts. Safran Engineering Services took responsibility as the design authority for the design, development, integration, installation, testing, tech pubs and STC approval under FAA, EASA and TC agencies.

Woori DS Co., Ltd. has developed firmware for a cooling and heating air conditioning system that performs all controls, fault diagnosis and communication for heating and cooling control and positive pressure control inside an armored vehicle, and developed an inverter control device capable of controlling communication with the armored vehicle body system and monitoring error situations. We are developing products based on the best technology and competitiveness to satisfy customer requirements for electrical equipment required for armored vehicles. In addition, we have developed an air conditioning system blower durability test device that can test the durability of air conditioning blowers, and we have secured test and evaluation technology for blower durability by checking blower errors and performing cycle management. By continuously securing innovative technologies in the defense industry, we are expanding our electronic device development business to deliver new value and impress customers with the highest quality and trust from product design, development, and mass production.

KJF designed and fabricated passenger, service and cargo door assembly toolings for sukhoi superjet 100.

With more than 3,000 EO/IR sensors on order or delivered, the Star SAFIRE® series provides the longest range performance in its class.

Hydraulic top bracing is an attenuation device installed between the main engine and the hull of the ship to reduce thermal expansion and vibration from the main engine to natural frequencies. The operating principle is an automatic control operating system through in/out and on/off the operating range of the hydraulic top bracing according to the rpm of the main engine. The number of hydraulic cylinders per engine is typically 2, 4, 6 depending on the type of engine, up to 8 are installed if necessary, and 1~2 of control panels are installed.

The Ku-band Amplifier Module is a low-power amplifier designed to amplify the LO (Local Oscillator) frequency in the Ku-band. It provides a gain of at least 17 dB and an output level of 13 dBm or higher. The module includes a built-in monitoring function for output signal detection.

GAIN CRITICAL CLARITY WITH SATELLITE TASKING Task ICEYE SAR satellites to access groundbreaking data on any location on Earth – day or night and in any weather. The process is simple and images are usually delivered within 24 to 48 hours of your initial request. ORDERING SAR DATA – MADE SIMPLE We believe access to reliable and timely SAR Earth observation data should be available to all, so we provide access options designed to meet your specific mission needs and collection timeframes. The process begins with defining your area of interest, revisit frequency and other parameters. The first images are usually acquired, downlinked, decoded and processed within 24 hours of the initial request and delivered within 8 hours after that.

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.