Quadro expands the capabilities of Exolaunch's microsatellite separation systems with a four-point offering tailored to match the Arrow 150 satellite with masses up to 250 kg. It is currently the only separation system which is qualified to fly the Arrow 150 platform on the SpaceX Transporter missions. Quadro was crowned the most innovative separation system in Europe by winning the Innovation in Space Award 2023 at the European Space Summit, celebrating its unique blend of flight-proven technology and cutting edge four-point design securing access to orbit for the next generation of microsatellite buses.

The SCXMC-SFPDP is a high-speed optical communication card that operates through the XMC interface of the SBC. It is designed to transmit and receive large volumes of data between the SBC and other devices in real time. Unlike Ethernet, which can be difficult to synchronize, the SCXMC-SFPDP uses optical communication with synchronization signals, enabling precise and high-speed data transfer. It offers low response latency (<40 µs) and supports four transmit/receive channels at 3.125 Gbps per channel. A device driver program is required for operation, and the Linux driver can be downloaded from Seedcore’s product page. Drivers for other operating systems can be developed upon request. This module is deployed in the L-SAM multi-function radar system to ensure reliable real-time data transmission between mission-critical subsystems.

· Cannon laying : Automatic/Semiautomatic /Manual(within 10 secon)ds · Elevation : 45 ~ 85°(driving speed 10°/sec) · Deflection angle : 360°infinite (driving speed 20°/sec) · Sighting Error : Max 3 mil(1σ) · Navigation System : Send location/orientation information

The fully redundant DA 30-HT-D has been developed for applications with the highest reliability demands. The redundant – two channel – design of the actuator allows continuous operation even if one of the two channels has failed. All major components such as the electric motors, control and communication electronics, and power supply are available twice (redundant). The position sensor features a three channel design (for 2 out of 3 voting). Additionally, there are several sensors integrated to provide diagnostic information such as current consumption, supply voltage levels and temperature readings. All major components of the actuator are continuously diagnosed by the microcontrollers of the actuator and its health status can be read via the redundant RS485.

Haigh-Farr designs support hardware to work hand-in-hand with our solutions to maximize performance. Our support hardware utilizes the same well-proven construction as the antennas they support. Power Dividers, Combiners, Hybrids & Diplexers

It is especially suited for demanding applications, which require reliable performance, such as missile seeker gimbal stabilization, where small size and low power consumption is required, while in a low cost design that is also ideally suited for high volume commercial applications. System Performance PARAMETERS SPECIFICATIONS Standard Ranges ±100°/sec, ±200°/sec, ±400°/sec Input Voltage + and - 5.0 Vdc Bandwidth 110 Hz Output Noise < 005°/sec/√Hz Scale Factor Accuracy ±1% Nominal Features Dual Axis Capabilities in Small Form Factor Miniature Size: Only 25gm.(1.05” x 0.71” diameter) Hermetically Sealed In Stainless Steel Cylinder High Reliability DC Input/High-Level DC Analog Output Low Cost Applications Tank Turret Stabilization Missile Targeting Platform Stabilization Antenna Stabilization Camera Stabilization Spacecraft

NVS, Night Vision Scope is designed for individual soldiers and law enforcement personnel which has been already in operation all around the world. This device gives soldiers and law enforcement the versatility they need to engage in operations with optimum efficiency.

- Seamless integration with all CAD models - Specialized for UAM and eVTOL design - Supports analysis of complex aerodynamic phenomena - Accurate prediction of airflow under subsonic and supersonic flight conditions - Detailed analysis of boundary-layer flow separation and viscous effects