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

An optimized Plasma FIB-SEM platform with proprietary gas chemistries for high-quality delayering of the most current semiconductor devices

This system processes threat information across air, surface, and underwater domains, while providing video distribution, recording, and storage functions. It also interfaces with external equipment to enable efficient, fleet-wide operational control. - Compliant with MIL-SPEC standards (shock, vibration, temperature/humidity, EMI/EMC) - Equipped with a liquid-cooling system to protect internal components

Side shells, wing shells and fuselage structures are made of CFK, GFK, aluminium or organic sheets and get connected during production. Sealants are used to seal the connection surfaces. These are usually two-component polysulphides, which have to be applied in different geometries. Typical applications are: Fillet sealings, oversealings, interface sealings and seal caps. Due to their properties, polysulfides require very low pressure and shear handling. The compressibility of the fillers contained in the medium requires a high level of expertise and a coherent overall system from material removal to application. With manual application, long production times and high material ejection have a negative influence on the complete process. Complex quality standards are required due to the risk of human error. With the in-house developments of the vipro-DUOMIX from ViscoTec, this process can be depicted fully automatically. The individual nozzle design is also adapted to each application. The result is a controlled dosage in compliance with the specifications and at the same time the highest repeat accuracy.

ElectroAir’s mobile APA-65 -series combined units consist of frequency converter units (AC rated output power up to 45 kVA) and rectifier units (DC continuous current up to 800A). These units are intended for the ground servicing of all aircraft types with a frequency of 400Hz and voltage 115/200 V and to power on-board electrical equipment and launch aircraft/ helicopters with a voltage of 28.5 VDC. APA-65 series is designed to eliminate CO2 emissions with its unique technical characteristics. Diesel hybrid unit and battery driven unit - unit can perform the complete service of aircraft at remote parking places with diesel engine / through batteries and it is also capable to operate from the 50/60Hz, 400V, 3 phase main power supply grid as any electrical GPU, without fuel consumption and with zero operating emissions. The range of different APA configurations with no emissions allow for safer, cleaner and more practical operational conditions for operators and personnel at the location. These units are very compact in size and weight.

KAI participates in the system integration of the KSLV-II and development of its first-stage propellant tank while trying to secure the technology of Space Launch Vehicle.

- Compact size with built-in drive, position sensor, DC motor and gear box - Better durability & faster speed under similar rated load comparing to 12Lf series thanks to the bigger 17mm diameter DC motor - Position, current and speed control along with position & current feedback - Easy digital extended I/O control through 4 x Expansion I/O ports (No coding) - 27/37/50/87mm(*) stroke option (*): Each 3mm stroke can be added when adjusting the long stroke limit through Total Manager software. Rated load of 17N~70N depending on the lead angle for each stroke (Speed is inversely proportional to the rated load, so the higher the rated load, the slower the speed.) - RS-485 MODBUS-RTU protocol applied (IR open protocol is not provided) - Action feature which enables user’s motion save & run

The iGRVT-50 is InterGravity Technologies’ next-generation green-propellant orbital transfer vehicle (OTV), purpose-built for the rideshare launch ecosystem. iGRVT-50 enables small payloads (up to 15–20 kg class) to be deployed or serviced in a wide range of orbits. Key Features - Payload Capacity : Up to ~20 kg class hosted payloads - Propulsion System : 20 N green bipropellant thrusters (C₂H₆/N₂O) - Delta-V Capability : > 450 m/s - Communications : UHF, S-band TM/TC, X-band downlink