IMSAR's high performance multi-mode radar integration on Meta Special Aerospace's King Air provides all-weather imaging, monitoring, and surface search capabilities at long ranges and high altitudes. Contact us at 801.798.8440 or sales@imsar.com for more information.

Seedcore’s VPX Chassis Housing Assembly is designed as a structural platform for Multi-function radar signal processing systems. Featuring a robust 8U 2×5 slot VPX configuration, precision-machined aluminum construction, and excellent thermal management, it ensures high mechanical stability and optimal heat dissipation in demanding defense environments. This chassis housing is deployed in Korea’s key air defense radar systems, including the L-SAM, M-SAM, and LAMD programs, supporting mission-critical radar signal processing architectures.

- Minimizing the station's door opening and closing time to support drones' quick entry and exit. - Structural design to minimize noise and vibration when opening and closing the door - Design and implementation of an interface for interaction between an automatic door system and a drone. - Automatically opening and closing door system - Automatic detection of drones through cameras and sensors, and safe storage and charging functions

This product supports the following transmission standards. Designation Bit Rate ========== ========== CXP-1 1.250 Gbps CXP-2 2.500 Gbps CXP-3 3.125 Gbps CXP-5 5.000 Gbps CXP-6 6.250 Gbps CXP-12 12.500 Gbps The CXR-2C amplifies and transmits image signals from 1/2-channel CoaXPress cameras to a PC frame grabber. Typically, transmission matches the distance between the camera and the device. Transmission distance depends on the coaxial cable type, and due to significant variability, specific distances are not provided.

Broad range of specialized Coaxial, Triaxial and custom options for Network/Communications, Data Transfer, High Frequency/Micorwave and Inflight Entertainment Cable Demands • EMI immunity • Low Loss • light weight • Superior resistance to high temperatures and harsh environments • More flexible/Tighter bend radius

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)

- Installed on the fuselage or tail to provide flash lighting in a location that does not impede the visibility of position lights - The reflector rotates in an arc. - Flash Rate : 40 to 100 times per minute [cycle] - Effective Intensity : FAA FAR 29.1401 - SAE ARP 5825A

A distributed sensor system based on BOTDA (Brillouin Optical Time Domain Analyzer), capable of detecting structural deformation and external intrusion.