The structural design and interpretation technology uses a computer interpretation method to predict and design the design factors, properties and strength needed for the development of launcher platforms to satisfy stable missile firing conditions.
The operating unit and position controller controls the launcher position and direction so that the missile command and control unit can rapidly fire within a given operating time.
The firing design technology requires special material application and key element part design to protect the missile under any external environment and allows it to fire stably during operations.
The power supply design technology requires power transmission and power control to generate the power needed for operations by attaching the power transmission and generator to the PTO, which is the external vehicle engine power withdrawal device.
The soft starter design technology requires programming and power control to ensure the soft starting and stopping of equipment to control the hydraulic pump motor which generates the hydraulic pressure needed for system operations.
