Drones can also be remotely controlled using a control system for real-time route changes, mission aborts, emergency returns, and area patrol commands. Furthermore, based on their precise attitude control and location recognition capabilities, they can define and perform tasks such as recognizing specific objects and precisely landing at designated locations.

The flagship VS-210 represents a landmark achievement in Korea’s urban air mobility development. As the nation’s first domestically designed and manufactured piloted eVTOL aircraft to successfully perform an urban air mobility flight, the VS-210 showcases V-Space’s technological leadership in advanced electric aviation. Built with lightweight composite structures and a high-power electric propulsion system, it delivers quiet, zero-emission, and eco-friendly operation while demonstrating remarkable flight stability and control. Through its successful demonstration flights, the VS-210 has become a symbolic platform proving Korea’s readiness for the next generation of sustainable urban aviation. Under the slogan “Touchable Future,” V-Space continues to lead innovation in electric propulsion, integrated system design, and future UAM certification readiness.

Spring probes are designed to optimize performance in high reliability, multicycle applications. Smiths Interconnect’s spring probes are compliant which makes them ideal for blind mate applications as they self correct for x, y, z, rotational and angular misalignment of the target. Offered in compressed heights less than 2 mm and utilized on pitches as tight as 0.4 mm, they are well suited for high density, board-to-board, battery contact and high frequency applications. Mixed signals and functionality can be designed into a single connector.

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

- Installed on the fuselage or tail to provide flash lighting in a location that does not impede the visibility of position lights - The reflector rotates in an arc. - Flash Rate : 40 to 100 times per minute [cycle] - Effective Intensity : FAA FAR 29.1401 - SAE ARP 5825A

The QRS116 is a compact angular rate sensor ideally suited for applications in tactical, aerospace and mission-critical instrumentation. The QRS116 features exceptionally low noise, fast start-up, and a simple electrical interface, the QRS116 has no moving parts ensuring long service life and high MTBF. System Performance PARAMETERS SPECIFICATIONS Standard Ranges ±100°/sec Input Voltage + 5 Vdc ±5% regulation Short Term Bias Stability (100 sec at const. temp) 3 deg/hr Output Noise ( DC to 100 Hz) ≤ 0.002°/√Hz* * Values Indicated are for ±100°/sec. Range Features Exceptional Bias Stability Unprecedented Low Angle Random Walk Values Superior Vibration Performance Compact Industry-Standard Package (Same as QRS11) Rugged, Compact Package Integrates easily Applications Tank Turret Stabilization Defense Fixed Wing Defense Helicopter Unmanned Aerial Vehicles UGV – Unmanned Ground Vehicle Platform Stabilization Camera Stabilization Antenna Stabilization ROV – Remotely Operated Vehicle

EFFECTIVE RANGE : 600 m RIFLING : 1:7" Twist, 6 Groove R/H MAGAZINE CAPACITY : 30 rounds

- Interior/Exterior lighting control device - Input Power : 28 VDC - MIL-STD-461 - MIL-STD-704 - RTCA/DO-160 Section 25