This facility is used to verify that the test item withstands and functions properly under the static acceleration environment imposed during launch and flight by applying the centrifugal acceleration. The test item dedicated to this static test includes subsystem and component of launch vehicle, satellite and aircraft. The acceleration is generated by the rotary motion of a cantilever arm. The test object is installed on the mounting table at one end of the arm, and the acceleration of the test object is controlled by the rotating speed. The measurement signals are monitored and recorded in the measurement room via measurement rack at the center of the rotation. | |||
Rotation Radius | 7,250mm | |
Range of Acceleration | 0.2∼546m/s2(0.02∼55.7G) | |
Rotation Speed Range | 1.6∼82.9r/min | |
Direction of Rotation | Turn clockwise | |
Max. Load Capacity | 400kg (Smaller than 81,900kg•m/s2) |