The invention belongs to the field of
propellant combustion testing, and discloses a modularized
solid-liquid mixed propulsion fuel
combustion testing device and method. The high-pressure
combustion chamber cavity comprises a movable cavity and a fixed cavity which are communicated with each other; the moving cavity comprises an
oxygen inlet transparent window, a transparent window cover plate, a vortex
injector, a moving cavity cover plate, an
electric ignition device and a modularized sample table; the
oxygen inlet transparent window is fixed at the front end of the vortex
injector, the transparent window cover plate is arranged at the front end of the transparent window, the high-speed camera is arranged on one side of the transparent window cover plate, the vortex
injector is connected with the modularized sample table, and the movable cavity cover plate with a hole is arranged between the vortex injector and the modularized sample table; and an
electric ignition device is arranged on the outer side of the vortex injector. The device is not influenced by the structure of the grain, is suitable for testing various complex grain shapes, can measure the instantaneous thickness of the grain and calculate the instantaneous retreat rate of
microsecond or above, is not influenced by any external factors during
data processing, is convenient and simple to process, and is accurate in result.