The invention provides a carrier rocket empennage glue riveting assembly technology method. The carrier rocket empennage glue riveting assembly technology method comprises the steps that an assembly is preassembled on an assembly profile frame through an empennage part, honeycombs are cut in a single assembly form, after the part is subjected to surface treatment, riveting assembly of a skeleton is completed on a rivet face by secondarily utilizing a profile frame, and a glue applying film is pasted to a rivet pulling face for preheating curing; the honeycombs are assembled into the skeleton on the rivet face, and the rivet pulling face and the honeycombs are in positioning connection in a rivet positioning form; and after the assembly is assembled, through a cured mold bed, the assembly and the mold bed are positioned and fixed through a profile face and a three-point positioning mode, and placed into an autoclave to be cured and formed under the vacuum, high temperature and high pressure conditions, on-line process monitoring is conducted, the assembly and the mold bed are moved out of the autoclave after curing is completed, the strength of a test sheet with a furnace is detected, and other riveting operation on the rivet pulling face is conducted. According to the carrier rocket empennage glue riveting assembly technology method, by utilizing tool equipment such as the assembly profile frame, the cured mold bed and the autoclave, riveting assembly of a carrier rocket empennage can be completed, reliable bonding of an interlayer structure is achieved, and the strength index meets requirements.