ROTATING COMBUSTION TEST APPARATUS OF SOLID ROCKET MOTOR

摘要

The present invention relates to an apparatus for testing the rotational combustion performance of a solid propulsion engine and a method for testing the rotational combustion performance of a solid propulsion engine using the same. The load moving forward during this rotation can be measured by the load cell and the rotational thrust performance can be accurately measured on the ground, so that the development of a solid propulsion engine optimized for rotational flight can be efficiently progressed, and safety during testing can be secured. Rotational thrust performance test can be performed at low cost.