ts advanced integrated optics and closed-loop Field Programmable Gate Array (FPGA) electronics deliver much higher accuracy, lower noise and greater efficiency than competing technologies. In addition, the EG-1300 can be calibrated internally for better thermal effect and has both digital and analog outputs, along with separation of the electronics from the FOG’s sensing coil assembly to accommodate the widest variety of installation parameters. Features Fully-integrated optics and electronics Advanced optics and FPGA electronics for higher accuracy, lower noise and greater efficiency Precise navigation (1 mile/hour without GPS) Fast, precise gyrocompassing to 1 milliradian Bandwidth to 500 Hz Separate electronics and sensor modules More economical than competing systems Applications Navigational grade applications Unmanned aerial vehicle (UAV) guidance Missile guidance Aeronautics and aviation Robotics

GORE® SKYFLEX® Aerospace Materials are a portfolio of unique, commercially-available material sets, forms and sizes with a wide range of engineered properties and specifications. Gore’s tapes and gaskets are specified by leading civil and defense aircraft OEMs and solve many challenges such as sealing, abrasion, corrosion and gap filling. These materials can also withstand a wide range of temperatures.

The system is designed to maximise installation flexibility, through optional power and diagnostics data over RF (permitting the use of a single cable), and a highly reconfigurable baseplate to allow the mounting holes and connector type/ position to be tailored to the target platform. Use of Chelton’s established and field-tested GNSS Anti-Jam core firmware provides a high degree of protection against complex threat scenarios and in highly dynamic environments. A software definable core allows future upgradeable ‘Signal Intelligence Apps’ to be hosted, providing the user with situational awareness of the battlefield environment and allows feedback into mission planning activities.

EMCORE’s SDI170 IMU is designed as a performance-compatible inertial system that is form, fit, and functional with a legacy RLG-based IMU product, but with superior overall performance, versatility, and a significantly higher MTBF (Mean Time Before Failure) rating over ruggedized environments. The tactical performance of the SDI170 IMU is based on EMCORE’s mature, proven, dependable and accurate quartz MEMS inertial sensor technology in our SDI500 tactical-grade IMU. EMCORE’s quartz technology enables repeatable high-volume production of precisely machined sensor structures combined with the inherent large signal output and thermal stability of quartz materials. The SDI170 IMU is designed for demanding, mission-critical, rugged environments and ideal for continuous use applications with no wear-out components, highly linear accelerometer performance and longer life compared to competing alternatives. It is constructed with EMCORE’s latest generation quartz gyros, quartz accelerometers, and high-speed signal processing to achieve outstanding precision performance. The solid-state quartz sensors and hermetically sealed IMU construction provide reliable MTBF and a 20-year operating and storage life. Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection and flexible input power compatibility make the SDI170 IMU easy to use in a wide range of higher-order integrated commercial and defense system applications.

A connector in military or aerospace applications is a device used to join electrical wires, cables, or circuits securely, ensuring reliable signal and power transmission under harsh conditions.

From the rocket launcher to its upper assembly, the bomb rack unit, completing a full weapon system as one set. The rocket launcher is a weapon system independently designed to launch guided missiles or rockets through 7-tube and 19-tube launchers, enabling both single and multiple firings. Through its development, independence of the weapon system has been secured, and structural stability has been achieved by applying a design that considers aircraft vibration and aerodynamic effects. In addition, it is equipped with the capability to receive the system’s firing signal and ignite the rocket. Based on the successful development in 2017 of the 7-tube 2.75-inch rocket launcher assembly for helicopters, the company is now independently developing upgraded versions of the 7-tube and 19-tube rocket launcher assemblies. Through this effort, we are securing scalability for application to next-generation helicopters and UAV systems.

The GSG-8 GNSS Simulator is an advanced software-powered turnkey simulator, supporting multi-constellation, multi-frequency, and hundreds of satellite signals. With an incredible 1000 Hz iteration rate, the GSG-8 GPS Simulator is ideal for space trajectories, custom PNT signals, hardware-in-the-loop, and any type of all-in-view satellites simulation. With the GSG-8 Simulator, you can generate RF signals to simulate how your receiver device will react in the real world, under the simulation parameters that you set. Control every aspect of your simulation, including 6 Degrees of Freedom (DoF) receiver trajectories, multi-vehicle simulation, multi-path signals, jamming and spoofing, as well as atmospheric interferences. The GSG-8 is the most popular positioning, navigation, and timing test solution offered through Safran’s GSG family of Skydel-based simulators. It was developed to deliver the highest standard of Global Navigation Satellite System (GNSS) signal testing and sensor simulation performance in an easy to use, upgradable and scalable platform.

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.