Our LiDAR uses a custom-designed laser that separates 1064 nm and 532 nm wavelengths from a single source, with two dedicated receivers capturing each set of data independently. Inside the system, the linear laser beam is refracted at a 10-degree angle through a prism to enable circular scanning. An RF module is also integrated for real-time equipment status monitoring. From circuit board design to component selection, every part of this system was developed in-house by multiple institutions. As a result, we have successfully eliminated reliance on foreign technology.

InterGravity Technologies has developed a Type-III Composite Overwrapped Pressure Vessel (COPV) optimized for high-performance small spacecraft propulsion systems. The tank is designed with an aluminum alloy liner for impermeability and a carbon fiber/epoxy composite overwrap for high strength-to-weight ratio. The system is tailored for green propellant storage (C₂H₆, N₂O), offering an exceptionally lightweight yet robust solution for orbital transfer vehicles and CubeSat-class platforms. Technical Specifications - Type : Type-III COPV (Al liner + CFRP wrap) - Volume : 5.3 liters - MEOP : 75 bar - Proof : 230 bar - Burst : 250 bar - Dry Mass : < 1.0 kg

◾ Drive Motor : Electric motor installed in the Explosive Ordnance Disposal (EOD) Robot to supply power for driving. ◾ Flipper Motor : Electric motor that supplies power for driving the flipper of the Explosive Ordnance Disposal (EOD) Robot.

A VGA (640×480) LWIR (8–12 µm) uncooled micro-bolometer module with 12 µm pixel pitch and NETD ≤ 50 mK, paired with an F1.0, 10.7 mm EFL lens delivering H42° / V31.5° / D52.5° FOV. It streams at 30 Hz in either UVC (USB-C, 5 V) or GMSL1 (FAKRA, 12 V), with power consumption < 1.9 W. The compact, lightweight housing (30×30×58.9 mm for UVC; 30×30×70.9 mm with FAKRA for GMSL1; IP65; −40 °C to 85 °C) makes it well-suited for autonomous vehicles, UAVs, and security systems, providing reliable day/night thermal perception of pedestrians, animals, and objects in adverse weather.

Wing shells, side shells and fuselage sections are usually made of carbon fibre composites and glued together during the production process. With many components, a groove or an open edge remains after the bonding process, which must be filled or sealed. A modified two-component epoxy resin is often mixed and then applied manually. This often entails long production times and complex quality controls. Equally high material costs due to the processing of materials from cartridges. ViscoTec defies short pot life and materials that are difficult to handle: Thanks to a coherent overall system from material removal to material application, this process can be automated. The two components are taken separately from cartridges, hobbocks or drums and fed via hose lines to a two-component dosing system. Only at the very end of the process they are mixed in a static mixing tube and applied to the substrate (e.g. via a nozzle). The process is controlled and monitored by pressure sensors.

GE's T901 Engine for ITEPA test cell is not a combat mission. In combat, there is no time for an unproven design. With more than 100 million flight hours of ...

Nas-52 or Night Attachable Sight gives law enforcement and military personnel the versatility in operations through attaching simple night vision device prefixed to daytime sight which makes available to engage in surveillance or to acquire targets regardless of ambient light conditions. NAS-52 is a clip-on system designed to mount in front of any kinds of daytime riflescope, and it gives daytime riflescope the night vision capability. Sniper or designated shooter using daytime scope will significantly need this performance for night time operation.