Slightly smaller than the DCL120, the Model DCL110 red dot sight is designed and developed for the mid-size machine guns including armored vehicles, tanks and helicopters. Its wide lens (85x55mm) allows operators to have fast target acquisition and transition with both eyes open and make them easier to track moving targets from a natural firing position. Ballistic drop compensation ensures the red dot reticle is always on the target for the first round accuracy. Unique Features icon3Integrated recoil compensator retains sight picture on fast moving targets icon3Adapted a wide lens (85x55mm) makes easier to track moving targets. icon3Suitable for platform mounted weapons on armored vehicles, helicopters and boats icon3Compatible with night vision device icon3Different trajectory compensator per NATO 12.7 mm, NATO 7.62 mm and Cannon NATO 20

STANAG 4695 & GOSSRA* * GENERIC OPEN SOLDIER SYSTEM REFERENCE ARCHITECTURE compatible with Nett Warrior BREAK-AWAY CONNECTOR

Engine Start Begins with ATS. The Air Turbine Starter (ATS) is a key component of an aircraft's secondary power system, driven by Bleed Air supplied from the Auxiliary Power Unit (APU) to accelerate the engine up to approximately 8,900 RPM, enabling engine start. Through the in-house development and localization of the ATS, we have incorporated power generation, optimal design of the shear section with consideration of failure, Containment functionality, as well as lubrication and power transmission systems. In addition, we have secured manufacturing and assembly technologies and continue development aimed at successful operation and the establishment of a mass production system.

The reference timing is used as the standard time for many tasks linked in various fields of industry and society. Especially precisely synchronized timing information and signals are widely used to keep mobile networks synchronization and generate precise time and frequency. In addition, it is being utilized in various ways such as power protection system for power generation and load management of each power plant according to smart grid issue, military satellite communication, electronic warfare signal detection and command control communication system. Features NTP Related Content Timing Accuracy (1PPS): ± 100ns or less Providing Various Frequency Outputs According to User's Requirements GPS L1 Signal Synchronization Event Logging and Network Remote Management Available for operators ODM / OEM Supply Available Proven Stability Through Various Performances of Mobile Communication Network and Power Protection System Providing IRIG-B (TTL, SINE) Signal Input / Output Interface (selectable according to User's Requirement) Providing GPS NMEA in Message API form (N220) Providing PCIe Interface

Specification Array Format : 1280 × 1024 Pixel pitch : 10㎛ Spectral range : 0.9㎛ ~ 1.7㎛ (SWIR) Operability : ≥ 99.5% Quantum Efficiency : 70% @ 1550nm Application Near-infrared Imaging Imaging Spectroscopy Surveillance Medical Science and Biology Astronomy and Scientific Material inspection Food inspection Forgery detection

The ACTUS® ARKS11 (1–10X, 24mm FFP) Riflescope is engineered for precision and durability, meeting the demands of professional users across diverse environments. Featuring a First Focal Plane (FFP) optical design, it provides fast and accurate target acquisition at any magnification level. The illuminated reticle ensures clear and reliable aiming, even in low-light conditions such as dawn or dusk. Built for versatility and performance, the ACTUS® ARKS11 is the ultimate optic for users operating in dynamic and challenging environments.

Liquid Measurement Systems (LMS) engineers and manufactures commercial and military grade Digital Fuel Quantity Indicators to exact specifications. We integrate the latest technologies in delivering digital devices that our customers know they can trust.

Each SCU can interface with up to eight (8) fuel probes with temperature detection and/or fuel probes with compensators. It will process capacitive and resistive readings to determine the fuel heights for each probe and transmit the calculated fuel volume to the cockpit.