[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

- A red light mounted on the left side of the aircraft to indicate the aircraft's location - A green light mounted on the right side of the aircraft to indicate the aircraft's location - These lights indicate the aircraft's position, flight direction, and attitude - Visible/IR Mode, Steady/Flash Mode - Light Intensity : FAA FAR 29.1391 ~ 29.1395 - SAE ARP 5825A

The Harxon JH001 and JH003 antennas are purpose-built for UAVs operating in environments with jamming and spoofying, offering superior anti-jamming capabilities far beyond ordionary helix antennas. Leveraging advanced beamforming technology and pre-multiple filtering, these antennas significantly enhance signal quality by effectively suppressing out-of-band noise and mitigating multipath interference. This ensures robust, high-precision centimeter-level positioning, making them ideal for critical UAV applications.

aviation fuel refueling cart : Mobile refueling cart that can easily refuel light aircraft and helicopters Sump recovery system : Collect the drained/sumped aviation fuel from the aviation fuel refueling system, easily sample and test it, and then decide whether to drain it or return it to the system. Aviation fuel refueling system : The aviation fuel refueling system is compactly constructed with a skid for easy use and installation.

An optimized Plasma FIB-SEM platform with proprietary gas chemistries for high-quality delayering of the most current semiconductor devices

Hyundai Rotem's UGV has adapted the top-notch autonomous driving technoolgies from Hyundai Motor Group, capable of search and reconnaissance missions as well as munition transport. Fielded in real operation after approval by the ROK Army in 2021, its technologies were also appreciated in major events such as National Armed Forces Day and Combined Joint Live Fire Exercise.

From the rocket launcher to its upper assembly, the bomb rack unit, completing a full weapon system as one set. The rocket launcher is a weapon system independently designed to launch guided missiles or rockets through 7-tube and 19-tube launchers, enabling both single and multiple firings. Through its development, independence of the weapon system has been secured, and structural stability has been achieved by applying a design that considers aircraft vibration and aerodynamic effects. In addition, it is equipped with the capability to receive the system’s firing signal and ignite the rocket. Based on the successful development in 2017 of the 7-tube 2.75-inch rocket launcher assembly for helicopters, the company is now independently developing upgraded versions of the 7-tube and 19-tube rocket launcher assemblies. Through this effort, we are securing scalability for application to next-generation helicopters and UAV systems.

The new Super-TAC IMU integrates three fiber optic gyros that exceed tactical grade performance with three high-accuracy Micro-Electro-Mechanical Systems (MEMS) accelerometers and state-of-the-art support electronics in a single small, lightweight package. This solution addresses the need for superior inertial performance in a tactical- grade package, critical for operation in GPS denied and contested environments. The Super-TAC IMU measures change in velocity and angle, utilizing a configurable variable synchronous data link control (SDLC) digital serial bus. The Super-TAC is configured to offer customers the best value solution when designing new systems as well as provide the flexibility to upgrade existing platforms. The Super-TAC IMU employs state-of-the-art optics with fewer components, providing significant performance and reliability improvements across standard military environments. Background Emcore, located in Budd Lake, NJ has been designing, developing and producing inertial components, sensors and navigation systems for Space, Ground, and Avionic applications for over 35 years. Emcore has been developing Fiber Optic Gyros (FOGs) since the early 1990s, producing and delivering IMU products with performance ranging from tactical to strategic grade PERFORMANCE GYRO PERFORMANCE Bias Stability < 0.05 °/hr. (1σ) Angle Random Walk ( ARW) ≤ 0.01 °/√hr. (1σ) Scale Factor Repeatability ≤ 100 ppm (1σ) Scale Factor Linearity ≤ 50 ppm (1σ) Angular Rate Range 1,000 °/sec Acceleration Range 100,000 °/sec2 ACCELEROMETER PERFORMANCE Range ± 25 g Bias Variation ≤ 50 μg (1σ) Scale Factor Stability ≤ 300 ppm (1σ) SYSTEM PERFORMANCE Bandwidth (adjustable) 800 Hz (gyros) 150 Hz (accelerometers) MTBF >25,000 hr.