ICONYX™ is a high-performance tactical grade Inertial Measurement Unit (IMU) for guidance and control applications. ICONYX™ is designed to meet the most demanding environmental conditions with extreme accuracy and reliability. Proven Technology Safran proposes an IMU based on Hemispherical Resonator Gyroscope the HRG Crystal™. This technology is combat proven for 15 years and is extremely accurate, reliable, and is capable of navigating in the most contested GNSS denied environments. HRG Crystal™ Embedded Thanks to the HRG Crystal™, ICONYX™ surpasses the highest performances of its category while keeping the best in class SWaP (Size, Weight, and Power) characteristics of the market. High performance in demanding environments ICONYX™ includes 3 hemispherical resonator gyroscopes HRG Crystal ™ and 3 closed loop MEMS (Micro Electro Mechanical Systems) accelerometers in a compact package. Both Safran’s gyroscopes and Safran’s accelerometers are technological breakthrough.

The Haigh-Farr Wraparound™ is a self-contained omnidirectional antenna for cylindrical or conical shaped bodies. A single point feed is used and no external splitters, combiners or cable harnesses are required for installation. The antenna is conformal, and may be mounted flush, or on the exterior of the vehicle. Designs are available from 300 MHz to 13 GHz with typical applications including Flight Termination, GPS, Telemetry, Data Links and Transponder. Multiple antenna elements may be combined within the same physical Wraparound™, providing multi- band capability in a single, compact package. Wraparound™ antennas have been flown on vehicles from subsurface sea to space, including high-mach kinetic kill weapons, high-G projectiles and re-entry vehicles. The Wraparound™ has been qualified for use on several high performance vehicles flown on test and launch ranges throughout the United States and Europe. For high aero-heating applications an ablative heat shield may be added to the antenna for additional thermal protection.

CoaXPress enables bidirectional transmission of data transfer, camera control, power supply (PoCXP), and triggering over a single coaxial cable. This product supports the following transmission standards. Designation Bit Rate ========== ======== CXP-1 1.250 Gbps CXP-2 2.500 Gbps CXP-3 3.125 Gbps CXP-5 5.000 Gbps CXP-6 6.250 Gbps CXP-12 12.500 Gbps The CXR-4C amplifies and transmits image signals from 1/2/4-channel CoaXPress cameras to a PC frame grabber. Typically, transmission matches the distance between the camera and the device. Transmission distance depends on the coaxial cable type, and due to significant variability, specific distances are not provided.  4 CH x 1 Camera Configuration  2 CH x 2 Camera Configuration  1 CH x 4 Camera Configuration  2 CH + 1CH Camera Configuration

The SWE550S is a rugged 6U VPX fully managed Layer-2/3 Ethernet switch aligned with the SOSA profile, providing blazing-fast 25/100 GbE switching via a 3.2 Tbps fabric and flexible I/O reconfiguration. • 3.2 Tbps switch fabric delivering full wire-speed bandwidth (~2.5× typical) • Front: up to 2×100 GBASE-SR4 (MPO); Rear: up to 7×100 GBASE-SR4, SWE540A-compatible I/O • Fat-pipe ports reconfigurable into thin-pipe ports; copper ports support 25/100→10/40 Gb speed downgrade • Dual-core ARM + OpenWare™ management; built-in storage sanitization • SOSA-aligned 6U VPX form factor; air & conduction cooled; rugged Levels 1, C, E

Our LiDAR uses a custom-designed laser that separates 1064 nm and 532 nm wavelengths from a single source, with two dedicated receivers capturing each set of data independently. Inside the system, the linear laser beam is refracted at a 10-degree angle through a prism to enable circular scanning. An RF module is also integrated for real-time equipment status monitoring. From circuit board design to component selection, every part of this system was developed in-house by multiple institutions. As a result, we have successfully eliminated reliance on foreign technology.

- Interior lighting used by removing it from the upper cockpit mount - Adjust the DIM/BRT brightness by operating the knob switch - NVIS WHITE per MIL-STD-3009

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.

Twister is lightweight, rapidly deployable, and designed to provide actionable intelligence directly at the point of contact. Its agility and intuitive operation make it ideal for SOF units operating in contested or high-tempo environments. Key Features: Lightweight and packable <1-minute deployment Designed for small-unit autonomy Live video and metadata transmission Supports target acquisition and real-time threat detection