The 20W X-band BUC is a satellite ground transport terminal that includes a receive rejection filter and performs IF-to-X-band upconversion using an internal reference frequency. It features dustproof, moisture-proof, and waterproof protection, along with self-diagnostic functions such as fan and temperature alarms. The unit provides a total gain of over 50 dB and supports a wide bandwidth of 500 MHz. Its frequency stability is maintained within 0.35 ppm.

[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

RF Systems designs and manufactures antennas for UAVs, guided missile seekers, and satellite systems. Through proprietary Dip Brazing process, we achieve high structural precision and RF reliability in every antenna. 1. Guided Missile Seeker Antenna 2. UAV Slot Array Antenna 3. Satellite Communication Antenna 4. Satellite Lightweight SAR Antenna 5. Satellite SAR Feed

r-TWR are digital towers which enable the remote use of air traffic services (ATS) from any location. Being at an airport, air base or at a centralised location, distance is no longer a factor. The r-TWR functions can be integrated to a traditional tower as a hybrid solution, and can support the ramp and apron management using the same information. It can also be deployed and put in place when needed. Through the use of digital camera technology and sensors, operators can effectively conduct and manage various services remotely, based on visual surveillance. This removes the need to be on-site and occupying critical space at an airport, in favour of a chosen location.

Cool comfort fit and excellent elasticity with Nylon & Span materials Enhanced breathability & moisture absorption with mesh fabrics Applied Velcro® to sleeve for patch attachment V-neck / Round-neck design Long Sleeve / Short Sleeve Composition Material : NY80/PU20 High Gauge Trichord (Nylon & Span) Size 95 ~ 115 Colors BK (Black) RG (Ranger Green) CYT (Coyote Brown)

The engine offers a take-off power of up to 180 kW (235 hp). Excellent power-to-weight ratio. Small installation dimensions. Two outpu shaft speed configurations. Stable operation at high and low temperatures.

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The CAS-500(Compact Advanced Satellite), phase #1 project is the project in which KAI aims to develop a CAS500-1 by operating a joint design team with Korea Aerospace Research Institute(KARI) and to transfer the government’s satellite development technology to the industries. Then, KAI initiates the development of the CAS500-2 project and establish the industry-led development as well as mass-production infrastructure.