Rapid response satellite structure

The invention discloses a rapid response satellite structure. The rapid response satellite structure comprises a body structure and a propelling module. The body structure is composed of a carbon fiber frame (comprising a bottom plate), a lower partition plate, a middle plate, an upper partition plate, a side plate and a top plate; the propelling module is composed of a force bearing cylinder and a propelling modular bottom plate. By the adoption of the rapid response satellite structure, the problems that a research and assembly period is long, and the adaptation to a load is poor are solved. The rapid response satellite structure has the advantages of being simple in structure, light in weight, rapid to assemble, high in expansibility, high in adaptability and the like.