The AMT-206-1 composite tail rotor blade is a direct replacement for Bell 206A and 206B series helicopter tail rotor blades. Now fitted with a new style of feathering bearings manufactured by KAMATICS. These bearings provide a longer life expectancy, with a patented lining that provides lighter pedal loads and a higher level of chemical resistance, compared to that of the standard fabric Teflon-lined bearings. The AMT-206-1 tail rotor blade has a non-symmetrical airfoil section and incorporates a swept tip. The T/R Blade is primarily fabricated from uni-directional Graphite (carbon fiber) and Aramid (Kevlar™) continuous fibers suspended in an epoxy matrix and is fitted with a nickel abrasion strip on the leading edge. The abrasion strip is bonded on using a urethane adhesive. The AMT-206-1 composite tail rotor blades have a 30% cost advantage, twice the lifespan, higher strength and thrust, and a substantial noise reduction, making them safer and ideal for helicopter operators flying in noise-sensitive areas like national parks and built-up areas.

The operation of robotic inspection systems in an industrial environment requires a reliable control station. The second generation integrated control station -ICS 2- gives operators an all-in-one tool. Supplied in a rugged hardshell case (Pelicase®), embedded components such as a 21.5-inch touchscreen, high-performance PC or joystick can be selected according to industry standards. It also boasts a 10-year spare parts guarantee as well as extreme robustness and reliability even in harsh environments. Simplicity and ease of operation were key when developing ICS 2. The operator connects the robotic platform with one single cable and using the integrated joystick, operation is simple and self-explanatory.

Digital mission engineering tools connect every stage of the engineering product lifecycle, from initial design to operation. They enable reality-based 3D simulation across multi-domain environments such as air, space, land, and sea by incorporating high-resolution terrain, satellite orbits, RF and radar systems, and sensor environments to accurately replicate real mission conditions. With accurate dynamics-based physical models at the core, these tools provide quantitative analysis of relative positioning between systems, changes in altitude and attitude, line-of-sight availability, and communication link status. Users can predict and evaluate mission elements such as sensor operations, communication links, platform maneuvers, and orbit optimization through scenario-based simulations.

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.

We are an EASA-certified APU manufacturer. To date, we have installed more than 7,000 PBS APUs. This APU includes completely new combustion chamber, new control unit allowing allow non-operating altitude up to 8,000 m AMSL. Redesigned fuel system. Continuous operation for 6 hours. Exceptional reliability. Start up to 6,000 m

Based on our state-of-the-art facilities, the semi-conductor machinery component sector manufatctures parts including Chamber assembly, and Main Frame Assembly.

It supports both daytime and nighttime monitoring, making it highly versatile in various missions. The drone is optimized for portability, allowing operators to carry and deploy it with ease. Its compact design ensures rapid response capabilities while maintaining reliable performance in the field.

This is the UAV launchers capable of launching the fixed-wing UAVs even on mountainous terrain, field, ships without sufficient runways to take off. It is designed to be the most powerful and easy to operate to take off the fixed-wing type UAVs of various specifications(Take-off weight, Take-off speed, and allowable G-force) into the air. It provides an interface that standardizes the shuttle for any type of unmanned aviation vehicle, and is easy to mount and to avoid take-off interference. A specially designed and manufactured hydraulic actuator is used to fully cope with the take-off weight of the aircraft, and a proprietary accumulator to allow a wide range of launch speed control. And multiple pulleys are equipped to ensure acceleration performance.