AI Navigation Algorithm The Certus Mini range features Advanced Navigation’s revolutionary AI neural network sensor fusion algorithm. The algorithm was designed for control applications and has a high level of health monitoring and instability prevention to ensure stable and reliable data. High-Performance MEMS The Certus Mini range contains high performance MEMS sensors that are put through Advanced Navigation’s intensive 8 hour temperature calibration process. This provides the highest accuracy possible from this sensor class and outputs consistent accuracy over the full temperature range from -40°C to 85°C. Reliability The Certus Mini range has been designed from the ground up for mission-critical control applications where reliability is essential. Built using a safety-oriented real-time operating system, all software is designed and tested to high safety standards with fault-tolerance in mind. The Certus Mini range is designed, manufactured and tested to military standards. L1/L5 Multi Constellation RTK GNSS The Certus Mini D supports L1/L5 dual frequencies, and GPS, GLONASS, Galileo, BeiDou and NavIC constellations. Access to multiple constellations and frequencies provides enhanced accuracy, availability and performance even in difficult environments such as multi-storey urban canyons. The GNSS receiver has 10 mm position accuracy with real-time RTK or post-processed PPK. Dual Antenna Heading The Certus Mini D provides a high accuracy heading solution using two GNSS antennas. The Certus Mini D rapidly and consistently maintains an accurate heading without the need for magnetic calibration and is unaffected by magnetic interference. Additionally, the system can determine heading while stationary. This makes it well-suited to applications where there is limited, or no, positional movement.

Developed as Korea’s first hydrogen-and-battery hybrid propulsion system, this next-generation eco-friendly aircraft uses electric batteries for take-off and hydrogen fuel cells for cruise flight, achieving a new standard in sustainable aviation. Recognized as a world-first intellectual property, this model also became the first hydrogen hybrid Advanced Air Mobility (AAM) aircraft in Korea to receive Special Airworthiness Certification from the Ministry of Land, Infrastructure and Transport in 2024.

Features ● Wideband Frequency Range of 2.0~18.0GHz ● Rigid Construction with AL Brazing ● Monotonic Beam Shape, No Beam Split ● Optimized Gain Ripple and VSWR Applications ● General Purpose TX/RX Antenna ● EMC Testing ● TX/RX Antenna for EW Testing ● Wideband TX Antenna for Anechoic Chamber

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

Integrated logistics support division, a Vendor Item Tool Manager, Consumables & Special Cutting Tools, Fixed and Rotary Wing String Lighting.

Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration. Processes real-time vibration signals and converts them into IPS AVG units for output. Developed for localization, achieving 50% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x2 UART(RS-422/485) - x2 Accelerometer sensor - Sample rate : Up to 5,000Hz - Size : 220 x 206 x 52 (mm) - Weight : 1.75Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 10W)

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.

A compact EO/IR gimbal camera system designed for UAVs, unmanned surface vehicles, and defense platforms. The system integrates a QVGA/VGA-class LWIR thermal imager and a high-resolution EO camera within a stabilized gimbal, ensuring reliable performance in diverse environmental conditions. Optimized for ISR (Intelligence, Surveillance, Reconnaissance) missions, the system provides detection, recognition, and identification (DRI) capabilities with low-SWaP (Size, Weight, and Power) characteristics.