Collects data from various sensors within the aircraft system, converts it into the required format, and transmits it to the mission computer or flight control computer. Converts control commands received from the mission computer or flight control computer and relays them to sensors and other peripheral devices. Supports system control functions, monitors the status of key systems, and provides feedback. Achieves 70% cost competitiveness compared to equivalent-performance products. - x2 MIL-STD-1553B - x2 UART (RS-422/485) - x24 Analog input interfaces - x8 Analog output interfaces - x64 Discrete input interfaces - x40 Discrete output interfaces - Size : 270 x 270 x 62.2mm - Weight : 2.5Kg - Power : MIL-STD-704F (28VDC, 10W) - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G

SJP’s connector components are designed and manufactured to meet the highest standards of precision and reliability across industries. Equipped with state-of-the-art CNC multi-tasking machines and extensive know-how, we deliver solutions ranging from fine threading to complex geometries. Our connectors are widely applied in electronics, medical devices, aerospace, and defense, where durability and stable connectivity are critical. Through customized design services and fast lead times, we help our clients enhance their product competitiveness.

The iGRVT-50 is InterGravity Technologies’ next-generation green-propellant orbital transfer vehicle (OTV), purpose-built for the rideshare launch ecosystem. iGRVT-50 enables small payloads (up to 15–20 kg class) to be deployed or serviced in a wide range of orbits. Key Features - Payload Capacity : Up to ~20 kg class hosted payloads - Propulsion System : 20 N green bipropellant thrusters (C₂H₆/N₂O) - Delta-V Capability : > 450 m/s - Communications : UHF, S-band TM/TC, X-band downlink

FMP is built around Moog’s world-renowned military motion control technology. Options include integration of Moog’s high-performance stabilization and weapon stores management systems (SMS), providing missile firing capability to suit any mission. Missiles previously only launchable from helicopters may now be fired from ground vehicles with missile combinations able to suit any mission need from any platform.

Featuring an ultra-compact package of less than 5 cubic inches, the TAC-440 delivers 1°/hour gyro bias with 1 mg accelerometer bias stability and very low 0.05°/√hour angle random walk (ARW) over wide temperature ranges. The breakthrough performance of the TAC-440 IMU is based on a EMCORE’s proven quartz MEMS inertial sensor technology. 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 TAC-440 is a compact IMU constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The TAC-440 IMU is designed for demanding, mission-critical, rugged environments. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection make the TAC-440 IMU easy to use in a wide range of higher order integrated system applications.

KAI participates in the system integration of the KSLV-II and development of its first-stage propellant tank while trying to secure the technology of Space Launch Vehicle.

정상적인 신호 수신을 방해하는 재밍 (Jamming)을 극복하고 안정적인 위성신호를 수신하는 안테나를 독자개발하였습니다.

Our software enables engineers to analyze and optimize their preliminary designs in the best way possible – at the whole aircraft level – which not only saves time but money as well. With its Multi-disciplinary Analysis and Optimization (MDAO) approach, you can model aircraft and their subsystems, assess performance, and generally accelerate your progress in numerous design challenges. Whatever your aircraft preliminary design goals may be, Desmo has a solution.