The device consists of a power supply, dedicated Iridium and GNSS antenna, BLE, three configurable inputs/outputs, RS232, and CANbus in an environmentally sealed enclosure. Includes an Iridium Short Burst Data (SBD) modem that allows remote devices to send and receive satellite messages from anywhere in the world.

Taesang manufactures Engine-Ring Parts using advanced profiled ring rolling technology with SMS Group equipment. This process ensures efficiency, price competitiveness, and reliable quality for demanding aerospace applications

Liquid Measurement Systems (LMS) engineers and manufactures commercial and military grade Digital Fuel Quantity Indicators to exact specifications. We integrate the latest technologies in delivering digital devices that our customers know they can trust.

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.

Receives vibration signals from an accelerometer installed on the aircraft engine and monitors engine vibration. Processes real-time vibration signals and converts them into IPS AVG units for output. Developed for localization, achieving 50% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x2 UART(RS-422/485) - x2 Accelerometer sensor - Sample rate : Up to 5,000Hz - Size : 220 x 206 x 52 (mm) - Weight : 1.75Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 10W)

Customized Market Research answers questions about an overseas market including market trends and size, customary distribution and promotion practices, market entry requirements, regulations, product standards and registration, key competitors and potential agents, distributors, or strategic partners. Rural America's Intelligence Service for Exporters (RAISE) helps rural businesses identify new markets, find industry-specific market intelligence, or identify potential business partners in a country.

The Improved Fire Control System (IFCS) PNU / Universal Fire Control System (UFCS) UPNU family represents a true state-of-the-art system approach. Its design features permit ready adaptation and/or optimization to any current or future weapon system or sensor requiring precision pointing and positioning. The PNU / UPNU and its variants point the way for the future direction of the land navigation systems. Utilizing advanced sensors, electronics, software and aiding (GPS and odometer), the PNU / UPNU family delivers precisely what the Army of tomorrow needs — a system designed to remain operationally effective and affordable to support well into the future. Features High-performance RLG-34 ring laser gyros Common architecture and components (Paladin, PIM, Firefinder, IPADS) Embedded 12-channel Selective Availability Anti-Spoofing Module (SAASM) Impervious to jamming (inertial mode) Resistant to jamming (GPS-aided mode) Combat-proven Embedded Built-In Test (BIT) High reliability MTBF, low mean time to repair (MTTR) No periodic calibration required Applications Multiple Launch Rocket System (MLRS) High-Mobility Artillery Rocket System (HIMARS) Pointing and position location

- When flying in information, azimuth information about the attitude and position of the lead aircraft is provided to pilots of surrounding aircraft in the formation - Light Intensity : 6 cd (Beam Spread : 60) - NVIS Green A/IR per MIL-STD-3009