Small wind power systems and component components Durability technologies: Composites - nacelle, blades, corrosion protection Stability technology: and wind speed control (electrical) + tail folding (mechanical) High-efficiency system: Direct-drive PMSG - slotless, blades, coefficient of power (Cp): 0.429 MPPT (Maximum Power Point Tracker) : Maximum power following control Web monitoring: Real-time monitoring Easy to maintain and install Quality Assurance: More than 3 years System certification: New and renewable energy facility certification, new product (NEP), excellent product designation by the Public Procurement Service - Korea's first Element parts certification: generator, inverter-CE, blade static load test, demonstration test completed Annual average wind speed of 4.5m/s or more

Features NO MELT, NO DRIP (50/50 Nylon Cotton) Moisture control system for comfort and breathability Elbow protector insertable PALS webbing on lower sleeves for scalability Reliable components (YKK military zipper, etc.) Composition Sleeves: Nylon 50%, Cotton 50% Body: Functionalized Polyester Size 95 ~ 115 Colors MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

A world well know Aviation Ground Support Equipment (AGSE) in support of military and commercial aircraft

InterGravity Technologies has developed a Type-III Composite Overwrapped Pressure Vessel (COPV) optimized for high-performance small spacecraft propulsion systems. The tank is designed with an aluminum alloy liner for impermeability and a carbon fiber/epoxy composite overwrap for high strength-to-weight ratio. The system is tailored for green propellant storage (C₂H₆, N₂O), offering an exceptionally lightweight yet robust solution for orbital transfer vehicles and CubeSat-class platforms. Technical Specifications - Type : Type-III COPV (Al liner + CFRP wrap) - Volume : 5.3 liters - MEOP : 75 bar - Proof : 230 bar - Burst : 250 bar - Dry Mass : < 1.0 kg

- Inspection robot control and damage assessment for robot operators. - Pre-inspection information creation for inspection planning. - A 3D user interface for inspection robot status monitoring. - Damage assessment and result report generation capabilities.

InterGravity Technologies has developed a 20 Newton-class bipropellant thruster designed for orbital transfer vehicles (OTVs), lunar hoppers, and micro-spacecraft requiring high efficiency, reliability, and reusability. The thruster operates with green propellants (C₂H₆, N₂O), providing both environmental compatibility and storability advantages. Key Features -Thrust Level : 20N -Specific Impulse : > 295s in vacuum

A cost-effective and reliable EO/IR solution designed for unmanned platforms, combining compact design with strong performance. The system integrates QVGA/VGA-class infrared sensors and 2–20 megapixel EO cameras, providing versatile options to meet different operational requirements. o Infrared (IR) Sensor: QVGA/VGA resolution, optimized for detection and recognition in short-to-mid range surveillance o Electro-Optical (EO) Module: 2MP–20MP visible light cameras with high-resolution imaging, adaptable to multiple mission profiles o Design Philosophy: Lightweight, compact, and robust for integration into unmanned aerial vehicles (UAVs), unmanned surface vehicles (USVs), and ground robotics o Key Value: Balances price competitiveness, system reliability, and modular scalability for mass deployment

Taesang manufactures Fixed Wing Aircraft using advanced closed die forging technology with SMS Group equipment. This process ensures precision, consistency, and superior quality for critical aerospace applications