In response to USAF IPSAFE contract and developed as part of the LSI’s MACK-5A solution for the modernization of the ACES II Ejection Seat Survival System, the QUAD FIRE™ is LSI’s newest innovative addition to its survival accessory line. This unique survival tool contains four fire starting devices: an arc lighter, a ferro rod and striker, a fresnel lense, and wind/waterproof matches, plus Pyro Putty™ Fireball Tinder.

Relief Valve ensures high flow rate compared to competitor market designs. Climb/Dive Valve is a pressure equalizing solution for enclosed volumes that experience pressure differential levels between the internal and external pressure values of the system. Ball Valve is very commonly used on UAV and land systems. It is available with high torque and low torque actuation. Materials, sizes, end connects customizable.

Large Area Display Head Unit is included in avionics equipments used in the cockpit of an aircraft. Its wide screen vision development implements Full Glass Cockpit in aircraft. It also provides processing with more efficient yet less complicated circumstance with maximum 4 external input video signals Options that can be provided are - 20"x8" LCD Glass, LCD Module and Entire LAD system unit

A Very High Resolution (0.75 m GSD) and Wide-Field of View (24 km swath) optical payload under development. Designed for microsatellite integration, Chouette combines sub-meter detail with wide-area coverage, a unique balance that expands the scope of commercial EO applications beyond what current systems offer.

Next-generation wheeled military vehicles are essential to secure maneuverability and survivability for efficient power operation even in the worst weather and terrain conditions, so we have developed a run-flat product with pure domestic technology that can drive to a safe zone where tires can be repaired and replaced with quality that meets the standards of the United States and NATO (North Atlantic Treaty Organization) while ensuring stable steering and driving performance by applying our unique design in the event of tire pressure loss due to tire damage. Based on this, we produce and supply run-flat-related products to wheeled military vehicle manufacturers.

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.

CATIS™ is an ultra-high-resolution, small satellite imaging radar device independently developed by Lumir. It consists of three components: the radar signal transmission/reception device SCEU, an active phased array antenna SATA, and a data downlink antenna KaPA. This X-band imaging radar device is designed for small satellites weighing 150 kg, offering an ultra-high resolution of 0.3 m. It transmits wideband RF signals to the observation area while orbiting at an altitude of 500 km and receives the reflected signals to acquire Earth observation data.

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.