Proximity Device for target detection Optic Device for target detection

The fully redundant DA 30-HT-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 position sensor features a three channel design (for 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.

The TAC-450 FOG offers exceptional performance in bias stability, scale factor, and angle random walk, and is available in nine configurations to solve the most challenging design projects. The TAC-450 FOG is ideal for air, land, or maritime stabilization and pointing applications. Due to its versatility, and accurate, reliable output, it can also be utilized in navigation, guidance, and control systems. Highlights Designed for maximum ease of integration with housed or unhoused (for OEM configurations) options Available in nine configurations to solve the most challenging design projects Exceptional performance in bias stability, scale factor, and angle random walk 1-, 2-, or 3-axis configuration, each employing the world’s smallest precision FOG Technology Details Photonic Integrated Chip Technology EMCORE’s photonic integrated chip (PIC) technology* reimagines FOG technology by replacing individual fiber components with an innovative integrated planar optic chip. This results in a FOG with PIC Inside™ that’s reliable and robust. With three of these integrated photonic gyros at its core, the TAC-450-360 IMU provides the safe, accurate performance autonomous platforms demand.

Lumir is the first Korean company to successfully develop and manufacture this onboard equipment, delivering superior performance and significant cost savings compared to competitors’ products. By integrating non-volatile NAND flash devices into the image data handling unit, storage capacity has been significantly increased, with data retention maintained even when the power is off.The image data handling unit of the satellite is a core device that receives high-speed, large-capacity data output from Earth observation sensors mounted on the satellite—such as SAR or optical cameras—then compresses and stores the data in real time, while also performing encryption and encoding for transmission to ground stations. Lumir has successfully developed and manufactured this satellite-mounted device domestically in Korea for the first time, breaking reliance on imported technologies. This achievement secures Lumir’s competitiveness by delivering superior performance and significant cost savings compared to foreign products.

• Openable sleeves • Expandable sleeves • Convoluted conduits • Heat shrink tubing & sleeves • Heats shrink boots • Specific sleeves

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.

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)

ㅇKey Features RF Front-End - Frequency : C-Band - Tx Power : +27 dBm(0.5 W) , Rx Range : -10 ∼ -100 dBm - Rx Sensitivity : -95 dBm@2 MHz Baseband & Modem - Downlink : 2.4 Mbps / Uplink: 8 kbps - QPSK waveform and CTC Forward Error Correction Anti-Jamming / Anti-Spoofing / Video CODEC - Anti-Jamming Capability using DSSS - Anti-Spoofing Capability by AES-256/ ARIA-256 Encryption - Support H.264 / up to 1920x1080x30f Interface - 10/100 Base-T Ethernet x1, RS-422 x1, RS-232 x2 - 3G-SDI Digital Video IN/OUT Interface - Limited Discrete I/O (1PPS/sync_in, reset_in, status_out) ㅇQuality and Certification - MIL-STD-810G - MIL-STD-461F