The invention discloses a method for testing the multi-
target line quasi dynamic
combustion performance of a
solid propellant, comprising the following steps: (1) testing static burning rates of a
solid propellant to be tested under various pressures from low pressure to
high pressure, so as to obtain the relation curve of the average
combustion rate and pressure, the relation curve of the maximum effective
combustion rate and the test pressure, and the relation curve of the minimum effective combustion rate and the test pressure; (2) performing a combustion pressurization test for a
solid propeller sample under a close state, so that the pressure reaches the
pressure range to be tested; (3) drilling 6-10 target holes on the covered solid
propeller sample, and enabling the target lines and an ignition wire to pass through the target holes; (4) predetermining an initial pressure and an initial temperature, igniting the solid
propeller sample in a close
combustion chamber, and recording the fusing time of each
target line during the combustion procedure of the solid propeller sample; and (5) obtaining the dynamic relation of the combustion length, pressure, temperature and time during the combustion procedure of the solid propeller via analysis, and calculating the combustion rate, combustion rate
pressure index and combustion rate
temperature sensitive coefficient of the solid propeller sample in a certain
pressure range. The method disclosed by the invention is suitable for fast detecting performance, controlling quality and the like for each batch of products during the production procedure of the solid propeller, and can shorten the research and production period of the solid propeller and reduce the cost.