It is a system that performs missions such as monitoring, surveillance and reconnaissance by ejecting and launching a foldable fixed-wing drone from the canister(tube) launcher. It is equipped with EO/IR Cameras (Electro-Optical / Infra-Red), which are mission equipment for reconnaissance, so that effective day and night image information can be collected. The gathered image information is transmitted to the ground control system (GCS) in real time while detecting and tracking the target by applying AI-based image processing technology. The foldable fixed-wing UAV has a simple structure and light weight, so it can be stored and transported in the canister launcher, and can be operated immediately so that it can be operated without time delay, and if necessary, the air vehicle can be retrieved and re-used by using a net-type recovery system.

Green Optics possess proprietary CVD-based Zinc Sulfide (ZnS) production technology for defense and industrial multi-wavelength optical materials. We have core technological capabilities to manufacture high-quality ZnS products tailored to meet diverse customer requirements. ZnS Material Optical Performance and Processing ZnS materials produced through CVD processes provide high transmittance exceeding 70% in the SWIR wavelength range (8-12 μm). When these materials undergo additional Hot Isostatic Pressing (HIP) treatment, the crystal structure undergoes recrystallization, improving transmission characteristics to achieve over 70% transmittance in the visible (VIS) wavelength range of 0.45-0.8 μm. This process extends the application range of optical materials previously limited to SWIR and LWIR bands, delivering superior optical performance across multi-wavelength regions from VIS to LWIR. Material Specifications: - STD-ZnS (Standard ZnS Material): Manufactured via CVD process, exhibits transmittance exceeding 70% in LWIR wavelengths (8-12 μm) with high physical hardness (Knoop hardness: 210 kgf/mm²). - MS-ZnS (Multispectral ZnS): Converted from STD-ZnS through HIP processing, extends wavelength range into the visible spectrum. While crystal structure recrystallization during this process reduces hardness somewhat (approximately 150 kgf/mm²), it still meets MIL specifications. This dual-processing approach enables comprehensive wavelength coverage while maintaining military-grade durability standards.

A rotating component designed to accelerate and direct airflow gas within the engine.

The radar that Raytheon Missiles & Defense is building for the U.S. Army has long been known as the Lower Tier Air and Missile Defense Sensor (LTAMDS). Now, ...

The first step toward armed helicopters The Bomb Rack Unit (BRU) is a device installed on a helicopter’s Stub-wing to mount various armaments such as rocket launchers and air-to-ground missiles, and it consists of a Pylon Unit and a Bomb Rack Unit. CTLA’s Bomb Rack Unit is equipped with a Boresight function that allows vertical (up/down) and horizontal (left/right) angle adjustments, and a solenoid-actuated free-fall weapon release (Jettison) method is applied. CTLA’s Bomb Rack Unit has passed the system tests for the Light Armed Helicopter (LAH) and received suitability certification, and it is currently in mass production.

The Fuel Heater is engine-mounted with fluid connections to both the engine fuel supply system and the engine lube oil system. The heater provides fuel heating for fuel de-icing, using engine lube oil flow during aircraft cold start and cold operation periods. REPAIR PROGRAM • Triumph has the expertise only the OEM can offer • OEM repairs are more dependable, increase MTBF and cost less long-term • Repair price is all inclusive • TAT 45 days approx

Korean Commander’s Panoramic Sight Specification MODEL: SRBM-1702-60 APPLICATION: K1A1 KCPS SIZE: Φ163.8(I.D)/Φ233.5(O.D)85.6L NO. OF RINGS: 60RINGS TYPE: BORE ROTATING: CW/CCW MASS PRODUCTION ITEM (2009~ )

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.