Our products serve the clients in military and aerospace industries, who require high performance with strength and ability to perform at extreme temperatures and pressures.

Our firm offers end-to-end GaN production capabilities, including fabrication, packaging, test, and failure analysis to meet custom requirements. To enable customer designs, a process design kit (PDK) is available with a design manual, sample layouts, and a non-linear device model. Options available include fabrication of customer-designed wafers (“PDK foundry service”) or custom design by TransEON and fabrication according to customer specs (“NRE foundry service”). For either option, volume levels available include pilot/engineering runs, multi-project wafers (MPWs), or full production runs.

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.

Engine Parts, Overhaul

Product Information Frequency signal generator for small target detection High-frequency resolution design and frequency conversion function using DDS method main performance Frequency: Ku-Band ~ Ka-Band Very Small Size, Pulse Mode Output Level: -5dBm min Spurious: -30dBc min Harmonic: -40dBc min Phase Noise: High Performance Frequency Sensibility: 50ppm max Port isolation: 50dBc Min Applicable fields Applicable to ultra-small guided weapon tower system and small radar system

Designed for existing in-service EGI upgrade and compatibility with open architecture requirements. Perfectly suited for military helicopters, aircraft, fighter jets and UAVs, the BlackNauteTM Embedded GNSS and Time INS (EGTI) sets the new standard for resilient navigation performance.

This Control Actuation System (CAS) is a guidance system for unmanned flying objects. It consists of three MPS fin actuators that each independently position an aerodynamic fin. The maximum angle of incidence is ±8°, which allows the device to carry out highly precise dynamic manoeuvres. The miniature fin actuators that make up this Control Actuation System are manufactured by MPS Microsystems and were designed based on customer specifications. Designed to guide a very small object and disposing of an extremely limited space, these fin actuators meet strict requirements in terms of performance, weight - less than 100 g - and dimensions. To reduce the length of this actuator, MPS Microsystems used part of the screw length as the motor axis. This screw is equipped with a very compact 4-point contact bearing that simultaneously absorbs axial and radial loads. The angular play on the aileron axis is less than 0.1° rms. This actuator meets the storage and vibration requirements of military equipment.

Development of an integrated support system for total life cycle management of weapon systems