NarSha is a dedicated small satellite for monitoring methane (CH₄) emissions, a key contributor to the climate crisis. It is the first satellite of its kind in South Korea to be developed and led by a private company. The launch of NarSha-1 is targeted for the fourth quarter of 2026.

Type : Axial (6P) Size(L,W,H mm) : 330 × 283 × 310 Weight(kg) : 54 N. Speed(rpm) : 2500 N. Torque(Nm) : 385 N. Power(kW) : 100

The L Series comes with frames in various lengths to accommodate a variety of module combinations. The frames range from a basic frame with just 2 side rails and 2 end caps, to more complex versions with jackscrews, backshells, cable clamps, etc.

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.

Quapason™ is a high-performance vibratory gyroscope from Safran Electronics & Defense, combining the compactness of MEMS with the reliability of Fiber-Optic Gyroscopes (FOG). It delivers exceptional robustness, ultra-low noise, and high signal stability, making it ideal for stabilization and inertial navigation in harsh environments. Used in weapon turret stabilization, avionics, and artificial horizons, it has surpassed 140,000 units delivered, proving its reliability and precision across civil and military applications.

CATIS™ is an ultra-high-resolution, small satellite imaging radar device independently developed by Lumir. It consists of three components: the radar signal transmission/reception device SCEU, an active phased array antenna SATA, and a data downlink antenna KaPA. This X-band imaging radar device is designed for small satellites weighing 150 kg, offering an ultra-high resolution of 0.3 m. It transmits wideband RF signals to the observation area while orbiting at an altitude of 500 km and receives the reflected signals to acquire Earth observation data.

· Wide-area situational awareness through omni-directional cameras and EO/IR sensors · Seamless remote control enabled by LEO satellite communication and USV teaming operation · Multi mission capabilities by interchangeable mission modules such as UUV, UAV and compact rocket modules

Auto Assembly Jig For : Wing Bottom Panel A320 Project 50m (L) x 1.1m (W) x 3.6m (H )