With a peak torque of >200Nm / 1770 lbf-in and a rated torque of 80Nm / 708 lbf-in, the fully redundant DA 58-D is the strongest, electromechanical, fully integrated (actuator control electronics, position sensing, motor and drivetrain in one housing) actuator in the market. Besides the well-proven redundant RS 485 interface, the DA 58-D also features a redundant CAN bus interface. The DA 58-D has been developed for applications with the highest reliability demands. The redundant – two channel – design of the actuator allows continuous operation even if one of the two channels has failed. All major components such as the electric motors, control and communication electronics, and power supply are available twice (redundant). The actuator features a triple-redundant position sensor (2 out of 3 voting). Additionally there are several sensors integrated to provide diagnostic information such as current consumption, supply voltage levels and temperature readings. All major components of the actuator are continuously diagnosed by the microcontrollers of the actuator and its health status can be read via the redundant RS485 / CAN interface.

The CAS-500(Compact Advanced Satellite), phase #1 project is the project in which KAI aims to develop a CAS500-1 by operating a joint design team with Korea Aerospace Research Institute(KARI) and to transfer the government’s satellite development technology to the industries. Then, KAI initiates the development of the CAS500-2 project and establish the industry-led development as well as mass-production infrastructure.

24-7 non-stop operating RADAR for ceaseless aerial surveillance and early trajectory detection. Design and Manufacture - Antenna Housing - Driving Unit

Between Earth and space: stratosphere-compatible, solar-powered high-altitude aircraft, known as HAPs (High Altitude Platforms), offer a sustainable alternative to satellites for Earth observation and communication. They are reusable, cost-effective and flexible in use. The DLR joint project HAP-alpha is developing such a technology demonstrator and is endeavoring to establish a complete system capable of permanent operation. The aim is for DLR to build up comprehensive expertise for the development of high-performance, high-flying solar aircraft and to play an active role in shaping the legal framework. In summer 2025, the HAP-alpha successfully passed a ground vibration test.

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.

SAIT CIRUS has been fortunate to receive generous funding from the Canada Foundation for Innovation (CFI), Natural Sciences and Engineering Research Council of Canada (NSERC), and Prairies Canada to support the development of our research centre and supporting applied research projects. Our research centre features a diverse and advanced fleet of remotely piloted aircraft, sensors, survey equipment, data processing and modeling software, and hardware. Some of our remotely piloted systems are the only ones in North America, making CIRUS a leading research centre on the continent.

The Ophir® SupIR 80-1200mm MWIR f/5.5 and SupIR 60-1200mm MWIR f/4 lenses are designed for 15 µm 640x512 and SXGA 10 µm pitch FPA (focal plan arrays) cooled MWIR detectors, respectively, providing detection ranges exceeding 28 km. Key Features: - High performance IR continuous zoom lens - Compatibility with 10 µm SXGA/HD and 15 µm 640x512 cameras - Maintains accurate LOS & focus through the full zoom range - Designed for extended range observation & C-UAS systems - Detection range exceeds 26 km