L14F type liquid level switches

Monitors abnormal engine operation based on digital and analog signals from the aircraft engine. It calculates engine life indices and detects engine malfunctions for generate a Pilot Fault List (PFL), which will stored in memory. When an engine failure is detected, it provides warning for display on the Central Maintenance Panel (CMP). Developed as a replacement for obsolete, achieving 60% cost competitiveness compared to equivalent products. - x1 MIL-STD-1553B - x16 Discrete Inout - x14 Discrete Output - x3 Analog Input - x1 RS-232 - Size: 283 x 265 x 89 (mm) - Weight : 4.1Kg - Environment : MIL-STD-810G - EMI/EMC : MIL-STD-461G - Power : MIL-STD-704F (28VDC, 25W)

Ultra-High Accuracy MEMS Motus features some of the highest accuracy MEMS accelerometers and gyroscopes currently available. Motus’s inertial performance exceeds some FOG IMUs and is up to 100x smaller and 10x cheaper. Motus is put through Advanced Navigation’s intensive calibration process to provide consistently accurate data over an extended temperature range of -40°C to 85°C. Miniature Package Never before has such high inertial performance been available in such a small package. Motus consumes just over 1 cubic inch in volume and weighs only 26 grams. This makes it ideal for weight and size sensitive applications. Motus is available in an OEM package suitable for integration into larger products or an enclosed package for external and standalone use. Advanced Signal Processing Motus samples its sensors synchronously at 1000Hz through six individual 24-bit differential ADCs which minimizes noise as well as providing optimal thermal calibration and performance characteristics. 14 separate heavily filtered regulated power supplies ensure that each sensor and ADC is operating off the cleanest possible power supply. Reliability Motus has been designed from the ground up for mission critical control applications where reliability is very important. It is built on top of a safety oriented real time operating system and all software is designed and tested to safety standards with fault tolerance in mind. The hardware is designed and manufactured to mil standards. High Update Rate Motus outputs temperature calibrated sensor data at 1000Hz as well as filtered attitude at the same rate. This allows for control of dynamically unstable platforms.

Supported by a rugged internal combustion engine compatible with heavy fuels, Reliant delivers over 10 hours of persistent ISR without runways, launchers, or recovery gear. Designed for high-wind, high-altitude, and denied environments, Reliant excels where legacy platforms fall short. Dual swappable payload bays support ISR, SIGINT, or EW missions, while onboard edge AI processing enabled by NVIDIA Jetson Orin NX modules delivers real-time threat detection and adaptive rerouting, even without connectivity. The platform can be deployed by a two-person team in under 10 minutes using a compact 10×10-meter footprint for launch and recovery from rooftops, vehicles, ships, or remote terrain. With an IP55-rated, all-weather design and reliable GNSS-denied navigation, Reliant gives operators the flexibility and resilience required to operate in complex, contested battlespaces.

The DA 15‐N is our smallest and lightest full brushless actuator. Its brushless motor and contactless, wear-free position sensing system makes the DA 15‐N immune to wear, vibrations and shock loads. It has especially been designed for usage in harsh environments and for safety-critical applications that require an actuator with high endurance. The conductive aluminum case and the shielded connection cable are reducing the susceptibility to any kind to EMI/RFI noise to the absolute minimum. The servo features position, temperature and current feedback as a standard and is fully programmable.

An Angle of Attack (AOA) indicator is a flight instrument that shows a pilot the angle between the aircraft's wing and the oncoming air, providing a crucial safety margin by warning of an approaching aerodynamic stall. Unlike airspeed. A Vertical Speed Indicator (VSI), also known as a Rate of Climb and Descent Indicator (RCDI) is an instrument which indicates the rate of climb or descent of an aircraft. These devices are installed and compatible with F-16 series aircraft and KAI's T-50/FA-50 series aircraft.

The device consists of a power supply, dedicated Iridium and GNSS antenna, BLE, three configurable inputs/outputs, RS232, and CANbus in an environmentally sealed enclosure. Includes an Iridium Short Burst Data (SBD) modem that allows remote devices to send and receive satellite messages from anywhere in the world.

V-BAT은 전투 검증을 마친 플랫폼으로, 유사한 성능의 Group 4 및 5급 대형 무인기 대비 비용과 물류 부담을 획기적으로 절감하면서, 전략 및 전술 수준의 ISR(정보 수집·감시·정찰)과 표적 획득 기능을 제공하는 기동성 중심의 운용 플랫폼입니다. 전자전 환경을 고려해 설계, 시험, 실전 배치된 V-BAT은, GNSS 차단 및 통신 간섭 상황에서도 임무 수행 효과성을 실전에서 입증한 바 있습니다. V-BAT은 미 해안경비대(Maritime UAS Services Program)의 공식 채택 플랫폼으로 선정되었으며, 미 해군의 거의 모든 함정과 해병대 전진기동부대(MEU) 전 편대에 실전 배치되었습니다. 독자적인 설계 및 제어 기술을 통해, 강풍, 혼잡한 비행 갑판, 이동 중인 함정 등에서도 4.6m x 4.6m 수준의 협소한 공간 내 이착륙이 가능합니다.