The invention discloses a pipeline integrated
attitude control rocket engine thrust
test structure and a working method thereof, and belongs to the technical field of sensing measurement and control. The testing structure is composed of a front
fixed frame, a rear
fixed frame, a rear movable frame, a middle-layer movable frame, a front movable frame, a straight connecting beam, a front-end inclined connecting beam, a
propellant supply pipeline, a rear-end inclined connecting beam, a sensitive beam, a
thin film sensor and a supporting thin beam. The thrust generated by
rocket eruption enables the engine and the adapter frame to displace, then a series of structures from the front movable frame to the rear movable frame are driven to move step by step in the horizontal direction, strain function film
layers of the four film sensors on the sensitive beam are deformed, and finally a differential
Wheatstone bridge is formed by the circuit board for testing. According to the invention, the film sensor and the
propellant supply pipeline are integrated on the
test structure, and the S-shaped
propellant supply pipeline, the circular truncated cone type movable frame structure and the layered overall structure are designed, so that the sensitivity of the test sensor is remarkably improved while the high rigidity of the test device is ensured.