Military · Test Equipment · Ammunition & handling equipment · Maintenance tooling & fixture · Fluid servicing equipment · AGSE Components .

Engine Parts, Overhaul

TESCAN SOLARIS X 2 extends FIB physical failure analysis capabilities to large-area applications, making deep cross-sectioning of advanced packaging devices, displays, MEMS, and optoelectronic devices more efficient. Featuring the new generation Mistral™ Xe Plasma FIB column, SOLARIS X 2 offers increased maximum ion beam current and a sharper ion beam profile across the full range, with significantly reduced beam tails. This allows operators to use higher milling and polishing currents, achieving superior surface quality comparable to conventional Plasma FIB, but with greater speed and precision.

The EMC-102 EDECU is configured as a common supervisory engine control for both T700-GE-701C/D and T700- GE-401C applications. Slated for use by the Army on current fielded models of Black Hawk helicopters, the control is configured with modern electronics, allowing for a more reliable alternative to the present Black Hawk control. The control unit is also compatible with the AH-64 Apache. The control is qualified to the latest Army requirements for superior operability in adverse environments.

The SBC6511 Rugged Single Board Computer(SBC) from Abaco Systems features the new high performance, highly integrated Intel® Xeon® E processor (‘Coffee Lake Refresh’). Powered by Intel® Xeon® W processors, offering robust computational power. • Supports up to 64 GB DDR4 SDRAM with ECC and up to 256 GB (or in some variants up to 480 GB) NVMe SSD storage • Offers high-throughput networking: Dual 40 GbE data-plane (KR4 “fat pipes”) • Features the Xilinx® Zynq® UltraScale+™ MPSoC FPGA (ZU7EG) for enhanced security

Digital mission engineering tools connect every stage of the engineering product lifecycle, from initial design to operation. They enable reality-based 3D simulation across multi-domain environments such as air, space, land, and sea by incorporating high-resolution terrain, satellite orbits, RF and radar systems, and sensor environments to accurately replicate real mission conditions. With accurate dynamics-based physical models at the core, these tools provide quantitative analysis of relative positioning between systems, changes in altitude and attitude, line-of-sight availability, and communication link status. Users can predict and evaluate mission elements such as sensor operations, communication links, platform maneuvers, and orbit optimization through scenario-based simulations.

Primarily used in medium-sized and large satellites, it provides high torque performance and momentum conservation. By localizing the Control Moment Gyro controller, which had previously been imported for Korea’s domestic satellite industry, Lumir has gained a competitive advantage in both performance and cost.

Three hydration ports Two side sleeve Internal hydration bladder pocket PALS webbing for MOLLE attachment Removable shoulder straps Drag handle Removable internal storage zipper pocket Removable beavertail Antimicrobial/FR treated padded spacer mesh Cubic Liters : 10.49L Dim. : 16" H x 8" W x 5" D Composition Material : 500D Cordura® + ARAMID / PV® Color : MC (MultiCam) BMC (Black MultiCam) BK (Black) RG (Ranger Green) CYT (Coyote Brown)