A
servo mechanism load simulator comprises a base, side upright plates, elastic moment spring plate clamping boards, an elastic moment loading support, an elastic moment spring plate, a swing shifting fork, an elastic moment rotary shaft, an elastic moment sensor, ball bearings, a bearing cap, a bearing seat, a friction shaft, a small oil cylinder seat, friction moment loading small oil cylinders, friction sheets, a friction moment sensor, an installation seat, roller bearings, a main shaft, an
inertia basic disc, an
inertia balance weight disc, self-aligning roller bearings, an upper supporting lug, a supporting spring plate cover plate, a supporting spring plate base, a supporting spring plate, a lower supporting lug, a guide bar and a
servo mechanism to be measured. According to the
servo mechanism load simulator, the structural characteristics, comprising the
inertia load, the elastic moment load, the friction moment load and the supporting rigidity, of a
rocket engine
tail nozzle can be simulated; the elastic moment and the friction moment can be respectively measured through a
torque sensor. The servo mechanism load simulator has the advantages of being simple and compact in structure and capable of enabling the structural characteristics of the actual
rocket tail nozzle to well reappear.