1. Maintenance • Depot Maintenance • Structure & Avionics Replacement, Repair, Wire Harness, Test and Inspection 2. Upgrade & Modification • Structure Upgrade and Modification • Avionics Upgrade, System Integration, Test and Inspection Highlights √ Final Assembly incl. Engine Installation √ System Integration, Test & Inspection Project Highlight : KT-100 & Light Sport Aircraft (Final Assembly), HH-60, CH-53, CH-47, F-16, P3-c, C-130H, AS-1S, MD500, NG RQ-4B ( Logistic & Ground Support)

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.

This is the UAV launchers capable of launching the fixed-wing UAVs even on mountainous terrain, field, ships without sufficient runways to take off. It is designed to be the most powerful and easy to operate to take off the fixed-wing type UAVs of various specifications(Take-off weight, Take-off speed, and allowable G-force) into the air. It provides an interface that standardizes the shuttle for any type of unmanned aviation vehicle, and is easy to mount and to avoid take-off interference. A specially designed and manufactured hydraulic actuator is used to fully cope with the take-off weight of the aircraft, and a proprietary accumulator to allow a wide range of launch speed control. And multiple pulleys are equipped to ensure acceleration performance.

ts advanced integrated optics and closed-loop Field Programmable Gate Array (FPGA) electronics deliver much higher accuracy, lower noise and greater efficiency than competing technologies. In addition, the EG-1300 can be calibrated internally for better thermal effect and has both digital and analog outputs, along with separation of the electronics from the FOG’s sensing coil assembly to accommodate the widest variety of installation parameters. Features Fully-integrated optics and electronics Advanced optics and FPGA electronics for higher accuracy, lower noise and greater efficiency Precise navigation (1 mile/hour without GPS) Fast, precise gyrocompassing to 1 milliradian Bandwidth to 500 Hz Separate electronics and sensor modules More economical than competing systems Applications Navigational grade applications Unmanned aerial vehicle (UAV) guidance Missile guidance Aeronautics and aviation Robotics

Primarily used in medium-sized and large satellites, it provides high torque performance and momentum conservation. By localizing the Control Moment Gyro controller, which had previously been imported for Korea’s domestic satellite industry, Lumir has gained a competitive advantage in both performance and cost.

Auto Assembly Jig For : Wing Bottom Panel A320 Project 50m (L) x 1.1m (W) x 3.6m (H )

Our technology and quality have been recognized internationally and regionally as we supply products manufactured based on AS9100, NADCAP special process approval to global companies lockage in domestic and overseas.