The SC-HPCRTM is a Rear Transition Module (RTM) designed to extend the I/O functionality of the HPC2812 high-performance computing board. It can be mounted on the rear side of the VPX backplane to enhance system connectivity and I/O flexibility. Since the HPC2812 board consists of two computing nodes, the SC-HPCRTM provides dedicated interfaces for each node, including Ethernet, USB, MMCX, and Mini-HDMI ports, ensuring optimal data communication and display output performance in mission-critical embedded systems.

FRAZIER AVIATION develops customized short- and long-term program packages that fit our Customers individual sustainment requirements and budget limitations. We are committed to crafting tailored spares and repair solutions that meet the distinct demands of each client. Military Aviation Program Sustainment (MAPS) * Tailored Customer agreements * Consisting of high turn structures * Manufactured at economies of scale * Cost effective, value added * Just-In-Time (JIT) deliveries Frazier Aviation Sustaining the Warfighter

InterGravity Technologies has developed a Type-III Composite Overwrapped Pressure Vessel (COPV) optimized for high-performance small spacecraft propulsion systems. The tank is designed with an aluminum alloy liner for impermeability and a carbon fiber/epoxy composite overwrap for high strength-to-weight ratio. The system is tailored for green propellant storage (C₂H₆, N₂O), offering an exceptionally lightweight yet robust solution for orbital transfer vehicles and CubeSat-class platforms. Technical Specifications - Type : Type-III COPV (Al liner + CFRP wrap) - Volume : 5.3 liters - MEOP : 75 bar - Proof : 230 bar - Burst : 250 bar - Dry Mass : < 1.0 kg

A cost-effective and reliable EO/IR solution designed for unmanned platforms, combining compact design with strong performance. The system integrates QVGA/VGA-class infrared sensors and 2–20 megapixel EO cameras, providing versatile options to meet different operational requirements. o Infrared (IR) Sensor: QVGA/VGA resolution, optimized for detection and recognition in short-to-mid range surveillance o Electro-Optical (EO) Module: 2MP–20MP visible light cameras with high-resolution imaging, adaptable to multiple mission profiles o Design Philosophy: Lightweight, compact, and robust for integration into unmanned aerial vehicles (UAVs), unmanned surface vehicles (USVs), and ground robotics o Key Value: Balances price competitiveness, system reliability, and modular scalability for mass deployment

Specification Array Format : 1280 × 1024 Pixel pitch : 10㎛ Spectral range : 0.9㎛ ~ 1.7㎛ (SWIR) Operability : ≥ 99.5% Quantum Efficiency : 70% @ 1550nm Application Near-infrared Imaging Imaging Spectroscopy Surveillance Medical Science and Biology Astronomy and Scientific Material inspection Food inspection Forgery detection

The Integrated Weather Observation System (IWOS®) is the compact, wireless, rugged weather station that can be customized to any customers’ specific needs. This system can replace legacy weather stations that require hardline power or extensive infrastructure for permanent installation. It integrates up to eight environmental sensing modules with optional satellite communication in a package that fits into a single case and weighs less than 25 lb. In addition to its portability, performance, and professional-grade construction, the modular design of the IWOS lends itself to higher accuracy, higher availability, and a lower lifecycle cost thanks to its easily replaceable and serviceable modules.

Ultra-High Accuracy MEMS Certus Evo features some of the highest accuracy MEMS accelerometers and gyroscopes currently available. Certus Evo’s inertial performance exceeds some FOG IMUs and is up to 100x smaller and 10x cheaper. Certus Evo is put through Advanced Navigation’s intensive calibration process to provide consistently accurate data over an extended temperature range of -40°C to 85°C. AI-Based Algorithm Certus Evo features Advanced Navigation’s revolutionary AI neural network sensor fusion algorithm. It was designed for control applications and has a high level of health monitoring and instability prevention to ensure stable and reliable data. Dual Antenna RTK GNSS Certus Evo contains a dual frequency RTK GNSS receiver that provides up to 1 cm accuracy positioning and supports all of the current and future satellite navigation systems, including GPS, GLONASS, GALILEO, BeiDou and QZSS. Dual antenna heading provides high accuracy heading that is not impacted by magnetic interference and has no motion requirements. Time Synchronization Certus Evo contains a GNSS disciplined oscillator that can act as the primary time source within a distributed time system, enabling access to ultra-accurate system time using PTP or NTP network time sync. Certus also has a high-accuracy 1PPS and frequency output. Multi Protocol Support Certus Evo features multiple interfaces including Ethernet, CAN, RS232, RS422 and GPIOs. Certus supports all the industry standard protocols including NMEA 0183, NMEA 2000, TSS, PASHR, Simrad as well as a wide variety of proprietary protocols. It features a rich web UI and 256GB of internal logging.

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.