Each SCU can interface with up to eight (8) fuel probes with temperature detection and/or fuel probes with compensators. It will process capacitive and resistive readings to determine the fuel heights for each probe and transmit the calculated fuel volume to the cockpit.

The VPX6-C6 which provides a full 6U OpenVPX(VITA65) is a Single Board Computer(SBC) that combines the power, versatility, cost-effectiveness of the 8th generation Intel mobile one-chip processor solution with the reliability. VPX6-C6 is based on the Intel i7-8665UE CPU that has quad cores running at 1.7GHz and providing a 32Gbytes of highbandwidth DDR4 SDRAM. Intel i7 processor includes an integrated Intel UHD 620 graphics engine, providing discrete GPU performance with OpenGL for graphics-intensive applications. For storage application VPX6-C6 provides the built-in 80GB SLC NVMe SSD solution via PCIe x4 lanes as well as the external SATA expansion through VPX site. The VPX6-C6 satisfies the demanding applications ranging from tactical aircraft to armoured vehicles to rugged industrial systems, with its rich complement of features and I/O including Intel Graphics, Integrated Platform Management Interface, Gigabit Ethernet, DIO, Serial channels, USB ports and more.

Mixed Signal Oscilloscope (4) Analog Channels, 10M record length, Certificate of Traceable Calibration Standard

The SCVPX-SSGM (Synchronous Signal Generation Module) generates synchronization signals to coordinate the operation and timing of various radar system components. It can generate synchronization signals using an internal clock, receive an external clock, or regenerate synchronization signals from external sources to maintain precise timing cycles. A device driver program is required for configuration and operation, and the Linux driver can be downloaded from Seedcore’s product page. Drivers for other operating systems can be developed upon request. This module is deployed in the L-SAM multi-function radar system, providing precise timing synchronization across mission-critical subsystems.

NO MELT, NO DRIP (50/50 NYLON COTTON) Incorporated ventilation system and COOLMAX & Mesh fabrics to ensure comfort and breathability Multi-pattern round processing for free movement Velcro® webbing for MOLLE attachment to support scalability Chest and sleeve side pockets to improve storage convenience Use MIL-SPEC threads and YKK zippers Composition Material : NYLON 50% / COTTON 50%, COOLMAX, MESH Size : 95~115 Colors MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)

BAE Systems has acted as the manufacturer and systems integrator of the Bradley program for over 30 years, including conducting various upgrades based on customer needs and mission requirements. The newest Bradleys feature the latest digitized electronics for optimum situational awareness, network connectivity, and communication within the ABCT. Over the life of the Bradley program, there have been several survivability upgrades, including installation of underbelly protection and the Bradley Urban Survivability Kits (BUSK), further enhancing the safety of one of the most survivable vehicles in the fleet.

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)

The ASN-157 was developed to meet the ongoing need for helicopters with reduced size and weight avionics. The ASN-157 system has an accuracy of 0.15 percent of total velocity, weighs less than 13 lbs., consists of one line-replaceable unit, and has a predicted mean time between failure of over 7,300 hours.