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.

Designed to support U.S. DoD modernization strategies, REDCOM Sigma is a complete software-based Command & Control solution with voice, video, chat, and conferencing. REDCOM Sigma® increases the warfighter’s operational flexibility while reducing size, weight, and power (SWaP) requirements at the tactical edge. REDCOM Sigma is based on open standards with a focus on interoperability, flexibility, and ease of use, and is listed on the DoDIN Approved Products List (APL). REDCOM Sigma was selected by the U.S. Army’s Program Executive Office Command, Control Communications-Tactical for network modernization at the tactical edge. Sigma is being deployed to multiple programs within the U.S. Army at the battalion level and below.

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

Key Features - Frequency Range: 8.5 - 10GHz - RX Noise Figure: 3.0dB - RX Small Signal Gain: 21 dB - TX Small Signal Gain: 27dB - TX High Pout: 39dBm - TX High PAE: 37% Chip size: 2.9x2.5x0.1mm  

Servo control is performed to remotely drive the armament device of the unmanned search vehicle and shoot at a moving target. - PMSM 4-axis servo control - Built-in regeneration function - Self-inspection and protection function

Gas-to-liquid heat exchangers, also known as air-to-water or water-to-air heat exchangers, are critical in high-performance environments where efficient thermal management determines reliability and output. They are widely used in applications such as engine charge air cooling, exhaust gas heat recovery, avionics thermal control, cryogenic fluid conditioning, and high-temperature gas handling.

This Ka-band antenna and data transmission device incorporates electronic beam steering antenna technology and software-defined radio technology as part of the Ka-band downlink system for satellites. It serves as a key component of data downlink systems within the satellite payload, supporting high-speed data transmission. The device enables system optimization through miniaturization, lightweight design, and single-unit modularization.

The AB-U10 is a 10 kg-class vectored-thrust eVTOL. With a wingspan of 1.8 meters, it features a maximum take-off weight (MTOW) of 10 kg, a range of over 10 km, a payload capacity of 2 kg, and a maximum speed of 160 km/h. The AB-U10 is a lightweight mission aircraft specifically designed for anti-drone operations, equipped with an integrated net gun system.