High-power laser weapons targeting objects at 0.5 ~ 4.0km distances require optical components with sub-nm wavefront error precision. Our Company has successfully developed aspherical polishing and high-power laser coating technologies for Ø300 ~ 550mm optical components through defense project experiences. measurement technology 1) Laser Induced Damage Threshold(LIDT) - The evaluation to confirm the durability of optical components is called LIDT (Laser-Induced Damage Threshold), which is defined as "the maximum amount of laser radiation incident on an optical component when the expected probability of damage is zero" (ISO 21254). In other words, it represents the maximum intensity or power of laser that an optical component can withstand, making it a critical requirement in laser weapon systems. - Our company has established LIDT measurement technology and in-house facilities developed in accordance with ISO 21254 standards. When compared with LIDT test results from domestic and international companies during laser weapon system development, we have demonstrated measurement technology and accuracy that meets or exceeds industry standards. While overseas companies require more than one month for verification processes, our company can immediately provide reliable data through our LIDT system. 2) Cavity Ring Down Spectroscopy(CRDS) - When the reflectivity is 99.997%, this may not present significant issues in low-power laser applications. However, in high-power laser components, even the 0.05% of light that passes through the optical mirror can cause problems in vulnerable parts of the system, including rear optical instruments, bonded lenses, and control cables. Therefore, measurement and evaluation methods for high-reflectivity optical mirrors are extremely important. - Currently, the transmittance and reflectance of optical components are generally measured using spectrophotometers, but measuring reflectance levels of 99.5% or higher is not possible with this method. CRDS (Cavity Ring-Down Spectroscopy) technology is required to achieve measurement resolution beyond that of spectrophotometers, and our company has established this system to measure the reflectance of various optical components. This is a critically important technology for responding to high-power laser weapon system development requirements.

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.

Military Parts

The ACTUS® CORE-1 Dot Sight is a high-performance optical device chosen as the Warrior Platform Selection Equipment by the Republic of Korea Army (ROKA). Built to MIL-SPEC standards, it meets rigorous military requirements, including extreme temperature resistance, shock testing, waterproofing, and protection against fluid contamination. Designed for durability and reliability, the CORE-1 enhances operator safety in the field, ensuring quick and precise target acquisition during critical missions.

MIL-DTL-26482 seriesⅡ has the same contact arrangement as MIL-DTL-26482 series I, and the bayonnet coupling method is applied. The connection between the contact and the wire is a crimping method, which is different from 26482-I. It provides reliable fastening with 5 guide keys. It also has excellent EMI shielding ability and can be used with various additional parts of the M85049 standard, so it is applied to aviation, space, and various high-tech precision equipment.

The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.

The SCVPX-SSGM (Synchronous Signal Generation Module) generates synchronization signals to coordinate the operation and timing of various radar system components. It can generate synchronization signals using an internal clock, receive an external clock, or regenerate synchronization signals from external sources to maintain precise timing cycles. A device driver program is required for configuration and operation, and the Linux driver can be downloaded from Seedcore’s product page. Drivers for other operating systems can be developed upon request. This module is deployed in the L-SAM multi-function radar system, providing precise timing synchronization across mission-critical subsystems.

It is designed to be suitable for difficult environments and can be applied to high torque and angle control. Applications are Missile defense, Torpedoes, Anti-drones system, Underwater drones.