Material: SS400-540, SPPS and ALDC1-8 Application Equipment: 60mm Mortar Purpose: Training for Prectice

From the rocket launcher to its upper assembly, the bomb rack unit, completing a full weapon system as one set. The rocket launcher is a weapon system independently designed to launch guided missiles or rockets through 7-tube and 19-tube launchers, enabling both single and multiple firings. Through its development, independence of the weapon system has been secured, and structural stability has been achieved by applying a design that considers aircraft vibration and aerodynamic effects. In addition, it is equipped with the capability to receive the system’s firing signal and ignite the rocket. Based on the successful development in 2017 of the 7-tube 2.75-inch rocket launcher assembly for helicopters, the company is now independently developing upgraded versions of the 7-tube and 19-tube rocket launcher assemblies. Through this effort, we are securing scalability for application to next-generation helicopters and UAV systems.

L3Harris combines speed, innovation and flawless execution to deliver the best solutions as quickly as possible.

Continental connectors are manufactured with highest quality materials. Our contacts are machined to close tolerances as opposed to stamped and formed styles. All molding compounds are glass reinforced, flame retardant and able to withstand severe environmental and mechanical requirements. Military connector families conform to the highest Defense Supply center (DSCC) standards, which require qualification testing and continued periodic requalification under the surveillance of government representatives to maintain our Company Qualified Product Listing (QPL)

We bring all our skills and expertise to bear in product development and in-service support in order to meet our customers' needs: 3D drawings and design Aeroelasticity Thermal, CFD analysis Static and dynamic analysis Electrical/hydraulic/mechanical system design Cost-optimized design, cost-benefit analysis Parametric experiment design Optimization techniques and algorithms Multiphysics modeling Concessions management: control plan, extension of concession, design engineering office, concession justification, impact analysis (FMECA, process/design change, etc.), definition of a repair program, updating of certifications Flight physics Configuration management Design, calculation and modeling Composite or metallic parts

The HPC2812 is a rugged 6U VPX high-performance computer aligned with the compute-intensive SOSA profile, delivering top-tier processing with dual Intel® Xeon® D-2700 (Ice Lake-D) processors and flexible expansion capabilities. • Supports up to 128 GB DDR4 SDRAM with ECC and 480 GB NAND Flash (NVMe SSD) per node • Offers 2× 100 GbE (or 4× 40 GbE) data plane with RDMA, PCIe Gen 4 expansion plane, plus control and management plane support • Features the Xilinx® Zynq® UltraScale+™ MPSoC FPGA for enhanced security

STIM300 is a small, tactical grade, low weight, high performance non-GPS aided Inertial Measurement Unit. It contains 3 highly accurate MEMS gyros, 3 high stability accelerometers and 3 inclinometers. The IMU is factory calibrated and compensated over its entire operating temperature range. STIM300 is a cost-effective ITAR free solution for systems that only had FOGs as an alternative when reaching for the performance level of that STIM300 can offer. Each axis is factory calibrated for bias, sensitivity and compensated for temperature effects to provide high-accuracy measurements. The unit runs off a single +5V supply and communicates via a RS422 interface. The use of a 32-bit RISC ARM microcontroller provides flexibility in the configuration, like choice of output unit, sampling frequency, LP filter -3dB frequency and RS422 bit-rate and protocol parameters. For more advanced users, STIM277H may be put in Service Mode. In this mode all the configuration parameters can be temporarily or permanently changed by overwriting the current settings in the flash memory. Service Mode also provides the ability to perform single measurements, perform diagnostics and obtain a higher detail in the status byte.

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.