SAT-PRE establish emergency communication networks for communication-disrupted areas during natural disasters and catastrophes. SAT-PRE ensures communications between commands in deepest operational areas and also between team members. it maximized communication success in adverse terrain, weather and other terrible conditions. The rate of transfer success is over 90%. The implementation of various communication methods such as voice PTT, automatic location reporting, and specialized transmission and reception using satellites as we reflects the latest technology based on Iridium 2nd generation satellites. The mission control center's CL-700 receives information transmitted from the operational area SAT-PRE in real time for up to 1,000 units and shares on-site situations by linking with other systems.

High reliability KA series MIL-DTL-55302 compliant connectors offer signal contacts designed for demanding defense, commercial aerospace and space applications. The 2 and 3 row series are compliant to MIL-DTL-55302 and offer flexibility not available with other interconnects. The 4 and 5 row versions are also available and offer up to 490 contacts.

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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.

Next-generation satellite multi-band terminal system development project

An AI-powered geospatial intelligence platform that allows users to interact with satellite imagery through natural language. By integrating LLMs with advanced image processing and object detection, SatCHAT makes EO data accessible to non-experts, enabling real-time infrastructure monitoring, event detection, and automated reporting. This lowers the barrier for industries to leverage satellite insights.

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.

Monitors abnormal engine operation based on digital and analog signals from the aircraft engine. It calculates engine life indices and detects engine malfunctions for generate a Pilot Fault List (PFL), which will stored in memory. When an engine failure is detected, it provides warning for display on the Central Maintenance Panel (CMP). Developed as a replacement for obsolete, achieving 60% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x16 Discrete Inout - x14 Discrete Output - x3 Analog Input - x1 RS-232 - Size: 283 x 265 x 89 (mm) - Weight : 4.1Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 25W)