The utility model relates to a
rocket engine vertical transportation packing box, which comprises a buffer base, a shell outer cover, a plurality of groups of pull rod components, a support component and a clamp component, an engine is vertically placed at the upper end of the buffer base, and the pull rod components are respectively connected between the middle part of a main body of the engine and the buffer base in an obliquely upward manner. The clamping hoop
assembly is arranged on the
throat portion of the engine in a clamped mode and connected with a
turbine pump of the engine through the connecting rod
assembly extending upwards in an inclined mode, at least one supporting
assembly is connected between the buffering base and the upper portion of the
throat portion of the engine in an inclined mode, and the supporting assemblies are connected with the supporting assemblies in an inclined mode. At least one supporting assembly is connected between the buffering base and a
turbine pump of the engine in an obliquely upward mode, the engine is covered with the shell outer cover, and the lower end of the shell outer cover is connected and assembled with the buffering base. The device has the advantages of being simple in structure, stable, reliable, small in occupied space, high in disassembly and assembly efficiency, high in universality and the like, and the requirements for vertical transportation and storage of
rocket engines can be met.