The invention provides a composite vibration component test system of a turbopump-feed liquid rocket engine structure, and relates to the field of a structural composite vibration component test method. The system comprises three vibration exciters, an excitation support device, a computer, three control instrument and signal generators, a response acquisition system, three power amplifiers, threeexcitation rods, three force transducers and an acceleration sensor. According to the system, a vibration response which is difficult to realize by one single vibration excitation source is excited for the engine structure by employing excitation of multiple groups of vibration exciters, vibration response frequency spectrum components simultaneously comprise frequency spectrum characteristics ofa plurality of excitation sources including an engine combustion chamber, a turbine pump, and a combustion gas generating device etc., an amplification rule or an attenuation rule of each vibration excitation load spectrum can also be reflected, the sensitive degrees of the engine structural vibration response to different excitation sources are obtained through a relation analysis of the structural vibration response frequency spectrum synthesis components and the excitation sources, the cost is low, the technical difficulty is moderate, and the system is applicable to the turbopump-feed liquid rocket engine structure.