COMBUSTION FLAME GUIDE FOR ROCKET ENGINE TESTING EQUIPMENT

摘要

The present invention relates to a flame guidance system for a rocket engine combustion testing facility, including: a base frame installed below a rocket engine; a flame guidance member supported by the base frame to form a flow space inside; and a cooling part for supplying a coolant to the flow space inside the flame guidance member to cool the flame guidance member. According to the present invention, the flame guidance system for a rocket engine combustion testing facility reduces maintenance cost and time by allowing the exclusive replacement of a deformed or damaged flame guidance member when the flame guidance member is deformed or damaged by a flame of a rocket engine as a plurality of flame guidance members is connected together to guide a flame of the rocket engine.