The invention relates to the technical field of tactical
missile shell section structures, in particular to a
stringer housing which comprises a housing and a
stringer, wherein the housing is rotary and comprises a covering
skin and end frames located at both ends of the covering
skin and integrally formed together with the covering
skin; the
stringer is connected with an inner wall of the housing in an axial direction of the housing. The housing of the invention is a rotary structure; the end frames and the covering skin form an integrated structure which has no projecting structure, can be completed by lathing, greatly shortens the
processing cycle, and greatly improves the
processing efficiency; positions of an upper end frame and a lower end frame are designed according to the size of an interface; the positions of the end frame and the covering skin adopt smooth transition, can be completed by lathing, greatly improve the
processing efficiency, and reduce
stress concentration. The stringer housing provided by the invention reduces the assembling difficulty and strength, effectively improves the assembling efficiency, also effectively reduces the weight of the
missile structure, and improves the
missile performance; the housing has high form-
position tolerance grade, ensures aerodynamic shape of the missile, has attractive appearance, has no obvious splicing joints, and reduces the probability of appearance of
rework events caused by appearance defects.