NVS, Night Vision Scope is designed for individual soldiers and law enforcement personnel which has been already in operation all around the world. This device gives soldiers and law enforcement the versatility they need to engage in operations with optimum efficiency.

Collects data from various sensors within the aircraft system, converts it into the required format, and transmits it to the mission computer or flight control computer. Converts control commands received from the mission computer or flight control computer and relays them to sensors and other peripheral devices. Supports system control functions, monitors the status of key systems, and provides feedback. Achieves 70% cost competitiveness compared to equivalent-performance products. - x2 MIL-STD-1553B - x2 UART (RS-422/485) - x24 Analog input interfaces - x8 Analog output interfaces - x64 Discrete input interfaces - x40 Discrete output interfaces - Size : 270 x 270 x 62.2mm - Weight : 2.5Kg - Power : MIL-STD-704F (28VDC, 10W) - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G

Nara Space’s first standard nanosatellite for Earth observation constellations with 7 optical bands and 1.5 m GSD. Launched November 2023 to the 525 km of the orbit, it has 2 years Mission Lifetime.

PELICAN-D LW is a 640x512 elements, 15μm pitch, Type-2 SuperLattice (T2SL) technology based 2D Long Wave Infrared (LWIR) digital IDCA. The new ROIC outputs digital signal, similarly to SCD’s previous digital detectors: Sebastian-320, Sebastian-480, Sebastian-640, Pelican-D, Hercules, and Blackbird. Pelican-D LW is available in the same configurations as the standard (MW) Pelican-D, with a large variety of cold shield apertures and cooler types. The proximity board provides the FPA timing and sensitive power supplies. Camera-Link interface highly simplifies the integration of the detector to the system.

Various line up, high torque frameless motor capable of precise speed and position control. Application areas are Collaborative robots, Dog Horse robots.

The 20W X-band BUC is a satellite ground transport terminal that includes a receive rejection filter and performs IF-to-X-band upconversion using an internal reference frequency. It features dustproof, moisture-proof, and waterproof protection, along with self-diagnostic functions such as fan and temperature alarms. The unit provides a total gain of over 50 dB and supports a wide bandwidth of 500 MHz. Its frequency stability is maintained within 0.35 ppm.

This system product is a product that directly supplies and heats lubricant oil for smooth operation of the main engine cylinder’s metallic and mechanical movement. Lubricator, a product that supplies lubrication directly to the main engine cylinder liner, can control injection timing and consumption using an electronic control method that responds to the movement of the main engine piston. The alpha lubricator system is based on an algorithm controlling the cylinder oil dosage proportionally to the sulphur content in the fuel and, fuel consumption on particular load of engine. Minimum cylinder oil dosage is required to provide an adequate oil film and detergency properties. Everllence and WIN GD engines are currently applying the second generation Lubricator type, the Everllence type is Mk-I and the WIN GD type is Mk-ε (Epsilon).

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.