SIMULATION TEST APPARATUS FOR LANDING ACCELERATION OF LIQUID-PROPELLED ROCKET

摘要

The present invention relates to a simulation test apparatus for a ground test of a liquid-propelled rocket, and more specifically, to a simulation test apparatus for landing acceleration of a liquid-propelled rocket for recognizing flight heat or flow characteristics of a propellant in a projectile due to a change in landing acceleration of the liquid-propelled rocket by simulating flight acceleration when the liquid-propelled rocket lands.;COPYRIGHT KIPO 2020