Hyundai Elevator is leveraging its expertise in elevator technology to develop infrastructure for urban air mobility (UAM). We are working on takeoff, landing, charging, and maintenance platforms that can be built on top of existing buildings, solving space constraints in congested urban environments. Our initiative is backed by their manufacturing expertise and government support, though global building codes may present a challenge in scaling the solution.

[LEO GNSS-R] Satellite : LEO RF Characteristics : GPS L1/L5, Galileo E1/E5a(option) Accuracy : Position ≤ 10m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : Sync to GPS Time Data < 1us (1PPS Accuracy < 1.5us) TTFF : Cold Start ≤ 20min / Warm Start ≤ 10min Dara Interface : MIL-STD-1553B, RS-422(Data Interface) [GEO GNSS-R] Satellite : GEO RF Characteristics : GPS L1/L2C/L5, Galileo E1 Accuracy : Position :: ≤ 30m(3DRMS), Velocity : ≤ 1m/s Raw Data Accuracy : Pseudo-Range : 1m(RMS) Carrier-Phase : 10mm(RMS) Data Output Rate : 1Hz 1PPS Accuracy : 2us(RMS)/Sync to GPS Time Data TTFF : Cold Start ≤ 45min / Warm Start ≤ 20min Dara Interface : MIL-STD-1553B EEE Parts : ITAR Free Parts

Reinforced & Non-Reinforced Seals

This product is a test-rig to test the injection and function of various fuel (diesel oil, gas) objects of the main engine. This product model is made from slide fuel valve types of traditional diesel engines to latest dual fuel gas engines GI, GI, LGIP, LGIM/X-DFM, and ammonia fuel valve engines LGIA and X-DFA types, and we are directly doing everything from design to production. In accordance with the maintenance regulations recommended by Everllence and WIN GD, it is a product that tests the normal functionality of fuel injectors of main engine after disassembling, cleaning and reassembling of fuel injection valves.

Our products are used for manufacturing interior design components for civil and military aircraft construction. Sandwich structures are used in many areas of an aircraft (storage compartments, interiors, wings) to reduce weight. In order to structurally strengthen the honeycombs or insert them, they often have to be filled during the production process. Typical materials are one- and two-component epoxy resins with a very high proportion of hollow glass spheres. These require extremely gentle handling, as they would otherwise be destroyed, which in turn would result in an increase in density. Common application patterns are beads, circles, full surfaces and egde-filling. The job is often done manually, which results in long production times and high running costs due to material waste. Lack of reproducibility is just as problematic as the health hazard often posed by these media. The ViscoTec solution: Material is continuously fed to the dosing system by removal from a large container. With the help of a robot or axis system, suitable structures can be mapped reliably. A coordinated overall system delivers a dispensing result according to specification, in which operator interaction is reduced to a minimum.

Its unique tail-sitter design enables vertical takeoff and landing while maintaining fixed-wing efficiency during flight. The drone achieves high-speed performance and extended flight distances, making it ideal for wide-area monitoring. With its advanced endurance and adaptability, GOSHAWK delivers reliable intelligence in both tactical and strategic operations.

KJF designed and fabricated passenger, service and cargo door assembly toolings for sukhoi superjet 100.

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