Slice6 AIR, Slice6 Air BR 는 극한 시험 환경에서 아날로그 신호를 정밀하게 측정할 수 있도록 설계된 통합 데이터 수집 장비로, 크기, 무게, 전력(SWaP)에 최적화되어 제한된 공간과 질량 조건에서도 효과적으로 운용할 수 있습니다. 각 모듈은 마이크로프로세서, 이더넷 스위치, 신호 조정 회로, 비휘발성 메모리를 포함하고 있습니다. 독립형, 네트워크형, 기존 시스템 통합형 등 다양한 운용 방식에 대응하며, IRIG 포맷 기반 실시간 스트리밍과 이중 저장 기능을 통해 실시간 모니터링과 백업을 동시에 수행할 수 있습니다. Ethernet-based data acquisition unit (DAU) for flight test and ground shock test. SLICE6 AIR, SLICE6 AIR BR is a complete data acquisition unit for measuring analog signals in extreme test environments. Optimized for size, weight, and power (SWaP), SLICE6 AIR is ideal for applications with tight size and mass constraints. Each module features a microprocessor, Ethernet switch, signal conditioning, and non-volatile memory. The versatile SLICE6 AIR can be used standalone, networked for high channel count tests, or integrated into existing Ethernet-based flight test instrumentation. Real-time streaming in IRIG formats and dual store-in-place recording enables both real-time monitoring and redundant back-up of data on a single device.

Engine Start Begins with ATS. The Air Turbine Starter (ATS) is a key component of an aircraft's secondary power system, driven by Bleed Air supplied from the Auxiliary Power Unit (APU) to accelerate the engine up to approximately 8,900 RPM, enabling engine start. Through the in-house development and localization of the ATS, we have incorporated power generation, optimal design of the shear section with consideration of failure, Containment functionality, as well as lubrication and power transmission systems. In addition, we have secured manufacturing and assembly technologies and continue development aimed at successful operation and the establishment of a mass production system.

A device that filters outside air through a filter of a positive pressure device during chemical warfare

1) Fabrication - possible Dismension : ~ D 1200 mm - Surface Errors PV < 79 nm RMS < 12 nm Roughness < 2 nm(Typical < 1nm) 2) Lightweight - lightweight Ratio : up to 82.5 % - Rib Thickness : ~ 2 mm - Face Sheet : ~ 7 mm - Lightweight Design & Fabrication

Slightly smaller than the DCL120, the Model DCL110 red dot sight is designed and developed for the mid-size machine guns including armored vehicles, tanks and helicopters. Its wide lens (85x55mm) allows operators to have fast target acquisition and transition with both eyes open and make them easier to track moving targets from a natural firing position. Ballistic drop compensation ensures the red dot reticle is always on the target for the first round accuracy. Unique Features icon3Integrated recoil compensator retains sight picture on fast moving targets icon3Adapted a wide lens (85x55mm) makes easier to track moving targets. icon3Suitable for platform mounted weapons on armored vehicles, helicopters and boats icon3Compatible with night vision device icon3Different trajectory compensator per NATO 12.7 mm, NATO 7.62 mm and Cannon NATO 20

Technology research that needs to be developed/secured to efficiently train future combat pilots ETS must have the ability to provide a realistic training environment in which pilots can immerse themselves in training through the use of simulations and CGFs within a real platform. The advantage of ETS is that it provides trainees with a training experience that is close to the real thing and reduces overall system operating costs by replacing real systems and consumables with simulations. Developed countries are already continuing to attempt to apply various core technologies to increase the efficiency of ETS. Hangil C&C Co., Ltd. is the only ETS development company in Korea, and is striving to develop cutting-edge ETS by combining years of research and development experience and its core technologies.

To guarantee maximum safety and reliability, our DA 30 features a brushless motor and a contactless wear-free position sensor. This means maximum service life with the greatest‐possible power delivery and its design prevents electromagnetic emissions (EMI) caused by brush sparking. The housing made of saltwater‐resistant aluminum is HART‐coat treated, meets the IP‐67 standard for water and dust sealing and provides an integrated Sub‐D connector (MIL spec. circular connector or cable gland on request). Brackets integrated in the housing for horizontal and vertical assembly. 8‐fold, ball‐bearing supported, steel gear train, drive shaft with ANSI multi‐tooth. The DA 30 series can be equipped with a standard PWM input (Pulse Width Modulation) that has two different interfaces: a differential, galvanic isolated interface (Opto‐Coupler) and a single‐ended interface with CMOS levels that is also used to program the servo parameters. It includes analog position feedback to detect the drive shaft position. A differential RS‐422 PWM interface can be chosen instead of the opto‐coupled interface. The DA 30 with digital serial command interface (RS‐485) receives its commands via a CRC secured protocol. It can return not only the shaft position in digital format, but also several diagnostic data such as the level of the supply voltage, current consumption and the temperature of the motor and electronics in digital form (optionally also the humidity within the actuator case). These kind of diagnostic capabilities help to determine the health state of the actuators before, during and after deployment.

The mighty Hitec SG33BLT Series servo actuators operate on DroneCAN (formerly UAVCAN), CAN 2.0 A/B, RS485, PWM and TTL command protocols, and feature brushless motors, magnetic encoders, and hardened steel gears. They are also environmentally sealed with an IP67 waterproof case rating. The SG33BLT Series was initially developed for the automotive industry requiring minimal support equipment and wiring, saving unnecessary installation complexity, cost and weight. This same functionality is now enjoying widespread adoption of CAN and DroneCAN systems within the UAV environment. With options for both 9~15-volt and 18~32-volt operations, and DB9SUB, Circular, & Gland Cable connectivity, the SG33BLT Actuator Series is sure to have a solution for your needs. #UAV #UAS #UAM #UGV #UUV #USV