When the emitter is flying in the air, it is easy to be disturbed by the external load, which causes the path deviation in the flight process. Therefore, dynamic performance of the emitter needs to be considered in the design stage. In order to study the influence of the positions of lumped masses on the dynamic characteristics of the emitter, a finite element model of a typical emitter is established. The first 20 orders free vibration modes of the emitter are calculated with different distributions of the lumped masses. Then, the optimal distribution of the lumped masses is obtained, which provides the theoretical basis for the structural optimization of the emitters.