Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration. Processes real-time vibration signals and converts them into IPS AVG units for output. Developed for localization, achieving 50% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x2 UART(RS-422/485) - x2 Accelerometer sensor - Sample rate : Up to 5,000Hz - Size : 220 x 206 x 52 (mm) - Weight : 1.75Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 10W)

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.

Technology research that needs to be developed/secured to efficiently train future combat pilots ETS must have the ability to provide a realistic training environment in which pilots can immerse themselves in training through the use of simulations and CGFs within a real platform. The advantage of ETS is that it provides trainees with a training experience that is close to the real thing and reduces overall system operating costs by replacing real systems and consumables with simulations. Developed countries are already continuing to attempt to apply various core technologies to increase the efficiency of ETS. Hangil C&C Co., Ltd. is the only ETS development company in Korea, and is striving to develop cutting-edge ETS by combining years of research and development experience and its core technologies.

High-Density Space-grade NAND Flash memory : 1. Density : 128Gbit (2G x 8bit x 8chips) NAND Flash 2. Package Type : 54 Pin SOP (Small Outline Package) 3. Radiation : TID > 60 krad, SEL (TBD)

This system product is a product that directly supplies and heats lubricant oil for smooth operation of the main engine cylinder’s metallic and mechanical movement. Lubricator, a product that supplies lubrication directly to the main engine cylinder liner, can control injection timing and consumption using an electronic control method that responds to the movement of the main engine piston. The alpha lubricator system is based on an algorithm controlling the cylinder oil dosage proportionally to the sulphur content in the fuel and, fuel consumption on particular load of engine. Minimum cylinder oil dosage is required to provide an adequate oil film and detergency properties. Everllence and WIN GD engines are currently applying the second generation Lubricator type, the Everllence type is Mk-I and the WIN GD type is Mk-ε (Epsilon).

The CAS-500(Compact Advanced Satellite), phase #1 project is the project in which KAI aims to develop a CAS500-1 by operating a joint design team with Korea Aerospace Research Institute(KARI) and to transfer the government’s satellite development technology to the industries. Then, KAI initiates the development of the CAS500-2 project and establish the industry-led development as well as mass-production infrastructure.

The IMX-5™ includes Attitude Heading Reference System (AHRS) sensor fusion to estimate roll, pitch, and heading. Adding GNSS input to the IMX-5 enables onboard Inertial Navigation System (INS) sensor fusion for roll, pitch, heading, velocity, and position. Features Tactical Grade IMU Gyro: 1.5 °/hr Bias Instability, 0.16 °/√hr ARW Accel: 19 µg Bias Instability, 0.02 m/s/√hr VRW 0.04° Dynamic Roll/Pitch 0.13° Dynamic Heading Surface Mount Reflowable (PCB Module) Fast Integration with SDK and Example Software Data Logging (SDK and Application Software)

The engine is suitable for MALE AUVs. Available in pusher and tractor configurations. Digital interface for control and monitoring. Stable operation at high altitudes and high temperatures. Ability to run at cold temperatures below -30°C without preheating.