Active phased array fire control radar (AESA) for aircraft A fire control multi-function radar (MFR) that can simultaneously detect, identify, and track multiple targets, including in the air and on the ground, and has SAR and NCTR functions. Aircraft (fighter)-mounted AESA radar is a core sensor for fighter jets to perform day/night/all-weather multiple missions. It operates in multiple modes such as air-to-air/air-to-ground/air-to-sea/support mode, and acquires ground images and air/ground in electronic warfare situations. It is essential mission equipment for fighter jets that detects/tracks multiple targets and supports guided missile guidance and gun shooting.

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.

The SWIR & NIR 25-250mm f/5.5 (NFOV) f/4.0 (WFOV) continuous zoom lens is a first to market low-Size, Weight, and Power (SWaP), compact lens, for the newly introduced 5μm SXGA, as well as for 10μm SXGA, and 15μm VGA SWIR detectors. The SWIR & NIR zoom lens employs a unique mechanical and optical design, resulting in an all-around smaller and lighter unit with only 860gr in weight, and 224mm in length, making it approximately 60% lighter than similar existing SWIR lenses. The SWIR lens is also chromatically corrected to support a broader short-wave IR wavelength regime from 0.7-1.7μm and operates with minimal distortion. The SWIR & NIR 25-250mm f/5.5 (NFOV) f/4.0 (WFOV) continuous zoom lens presents an unrivaled combination of SWaP capabilities, detection range exceeding 26km. Product features: • Continuous zoom in the 0.7-1.7μm SWIR regime • Designed for 5μm, 10μm SXGA & 15μm VGA SWIR detectors • Lightweight (<860 gr) • Detection range >26 km • Enables laser-line detection

Hydraulic top bracing is an attenuation device installed between the main engine and the hull of the ship to reduce thermal expansion and vibration from the main engine to natural frequencies. The operating principle is an automatic control operating system through in/out and on/off the operating range of the hydraulic top bracing according to the rpm of the main engine. The number of hydraulic cylinders per engine is typically 2, 4, 6 depending on the type of engine, up to 8 are installed if necessary, and 1~2 of control panels are installed.

- 1 axis Fiber Optic Gyroscope - Bias Repeatability (over temp. range): ≤ 1.0º /hr (1σ, RMS) - Angle Random Walk: 0.035º /√hr (typical, 1σ) - Power Consumption: 1.3 W @ 25℃ (<2.4 W, @ -40℃) - Input Voltage: + 5 V - Weight: 165 g (0.36 lbs)

Processor - 64-bit Quad Core PowerPC QorIQT2080 up to 1.2GHz - 6 DMIPS/MHz per core (up to 28,800 DMIPS@1.2GHz) - 128b AltiVecSIMD unit (up to 38.4 GFLOPs@1.2GHz) Memory - 4GB soldered 64-bit DDR3L SDRAM with ECC - 256MB 16-bit NOR flash - 64GB SATA NAND SSD - 512KB NvRAM Form Factor - 6U VME - Conduction-Cooled, Air-cooled support

Designed and manufactured to ensure flawless connection between precision striking functions, even in extreme temperatures, varying altitudes, and impact environments.