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.

FLAMEMASTER has formulating and compounding capabilities for sealants, adhesives, and coatings made from polysulfides, epoxies, silicones, and rubbers, among others. The product line includes corrosion-resistant materials, mid- and lightweight sealants, electrical potting compounds, and thermal barriers.

KAI participates in the system integration of the KSLV-II and development of its first-stage propellant tank while trying to secure the technology of Space Launch Vehicle.

The main wheel assembly refers to the complete structural unit that includes the wheel, tire, axle, bearings, and in most cases, the braking system. As the primary load-bearing gear, the assembly is engineered to absorb high-impact forces during landing and provide strong braking performance during deceleration. Its design integrates durability, safety, and serviceability, making it a critical element of aircraft ground operations.

The maximum transmission distance varies based on the following frequency-related specifications. Camera Frequency Max Cable Length ================ =============== 20 ~ 60 MHz 10 m 60 ~ 80 MHz 7 m 80 ~ 85 MHz 5 m  In cases where a single PC cannot handle large amounts of image data, it becomes necessary to duplicate the image and use multiple PCs for processing. A splitter is required in such scenarios.  The CLS-30T2S amplifies and transmits image signals from a single camera to up to two PCs, supporting Base/Medium/Full configurations (10 Taps supported).  The Master side transmits RS232 and CC1~4 signals, while the Slave side replicates and transmits image signals only.

- Application of patented expansion technology to resolve narrow space operation. - Equipped with camera function utilizing foldable mast. - Drone take-off and landing system using internal lift. - Equipped with a monitor for situational identification and a console for drone operation control.

PELICAN-D JT is a MWIR detector for missile applications. The FPA is InSb based, having digital Readout Integrated Circuit (ROIC) in a format of 640 x 512 with 15μm pitch. Pelican-D JT has a unique structure of Dewar which enables very fast cool down time and hence quick mission readiness using Joule-Thomson (JT) cooler. Due to the low heat load on the focal plane, the detector achieves long mission duration. The Detector can be supplied with a proximity board which provides Camera Link interface to the customer system. This highly simplifies the integration of the detector to the system.

Type : Axial (3P) Size(Ø, mm) : 310 × 109 Weight(kg) : 37 N. Speed(rpm) : 2100 N. Torque(Nm) : 450 N. Power(kW) : 100