The first step toward armed helicopters The Bomb Rack Unit (BRU) is a device installed on a helicopter’s Stub-wing to mount various armaments such as rocket launchers and air-to-ground missiles, and it consists of a Pylon Unit and a Bomb Rack Unit. CTLA’s Bomb Rack Unit is equipped with a Boresight function that allows vertical (up/down) and horizontal (left/right) angle adjustments, and a solenoid-actuated free-fall weapon release (Jettison) method is applied. CTLA’s Bomb Rack Unit has passed the system tests for the Light Armed Helicopter (LAH) and received suitability certification, and it is currently in mass production.

We has built a global partnership with accumulated technology to produce/supply major structures to Boeing and Airbus. By manufacturing large-scale composites that make the fuselarge of an aircraft, automated production technology applying robot concepts, non-destructive inspection technology and flow production line, etc. we are competing with advanced aircraft manufacturers with the best technology, quality and productivity by developing advanced technologies and equipment.

The APG-63(V)3 AESA radar provides powerful, adaptable radar technology, proven performance, and tactical flexibility that F-15 pilots can rely on. Available for F-15C and F-15E aircraft, it continues a tradition of innovative, highly reliable technology. Superior situational awareness is a key benefit of this all-weather, multimode radar.

Deep Reinforcement Learning and Knowledge-based Autonomous Maneuver/Engagement AI Pilot System - Air-to-air WVR, BFM/ACM autonomous maneuver/engagement AI pilot - Expandable to BVR engagement and mission performance * Terms: WVR (Within Visual Range), BFM (Basic fighter maneuvers), ACM (Air Combat Maneuvering), BVR (Beyond Visual Range)

The Military Satellite Communication System-II is a basic communication system that uses the military's own satellites operating in geostationary orbit to ensure mobility and survivability through dedicated satellite communication terminals without the help of any infrastructure on land, sea, or air in the ROK Armed Forces' operational area, including the Korean Peninsula. The Military Satellite Communication System-II is a basic communication system that uses the military's own satellites operating in geostationary orbit to ensure mobility and survivability through dedicated satellite communication terminals without the help of any infrastructure on land, sea, or air in the ROK Armed Forces' operational area, including the Korean Peninsula. We supply various types of satellite communication terminal equipment and major component modules that can transmit and receive large amounts of data in real time without regional restrictions using military satellites to system/system companies. Among the main modules of various satellite communication terminal equipment of system/system manufacturers, we supply modems and subscriber matching devices Military Satellite Communication System-II High-speed basic link, anti-electronic warfare link, and low-speed basic link of all satellite terminals 7 types of modems and 7 types of subscriber devices for interworking provide large-capacity data transmission, anti-electronic warfare capabilities, and multi-channel links

D-100-C repair & Bleeding

EMCORE’s SDI170 IMU is designed as a performance-compatible inertial system that is form, fit, and functional with a legacy RLG-based IMU product, but with superior overall performance, versatility, and a significantly higher MTBF (Mean Time Before Failure) rating over ruggedized environments. The tactical performance of the SDI170 IMU is based on EMCORE’s mature, proven, dependable and accurate quartz MEMS inertial sensor technology in our SDI500 tactical-grade IMU. EMCORE’s quartz technology enables repeatable high-volume production of precisely machined sensor structures combined with the inherent large signal output and thermal stability of quartz materials. The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

With a peak torque of >200Nm / 1770 lbf-in and a rated torque of 80Nm / 708 lbf-in, the fully redundant DA 58-D is the strongest, electromechanical, fully integrated (actuator control electronics, position sensing, motor and drivetrain in one housing) actuator in the market. Besides the well-proven redundant RS 485 interface, the DA 58-D also features a redundant CAN bus interface. The DA 58-D has been developed for applications with the highest reliability demands. The redundant – two channel – design of the actuator allows continuous operation even if one of the two channels has failed. All major components such as the electric motors, control and communication electronics, and power supply are available twice (redundant). The actuator features a triple-redundant position sensor (2 out of 3 voting). Additionally there are several sensors integrated to provide diagnostic information such as current consumption, supply voltage levels and temperature readings. All major components of the actuator are continuously diagnosed by the microcontrollers of the actuator and its health status can be read via the redundant RS485 / CAN interface.