Multistage rocket transportation erecting vehicle

Abstract

The invention discloses a multi-stage rocket transportation erecting vehicle, and belongs to the technical field of spaceflight ground support equipment. The support vehicle comprises a transport vehicle, a support adjusting system, an erecting arm assembly, a main erecting oil cylinder, a support seat and a lifting system, one end of the erecting arm assembly is hinged to the tail of the transport vehicle, and an auxiliary supporting arm is arranged at the bottom of the other end of the erecting arm. The main erecting oil cylinder is arranged on the inner side of the erecting arm assembly; the supporting and adjusting system is installed on the erecting arm assembly and has the functions of supporting, locking and four-degree-of-freedom adjusting of the multiple stages of rocket bodies, and butt joint between the multiple stages of rocket bodies and between the rocket bodies and the supporting base is achieved. The supporting seat is connected to the tail part of the erecting arm assembly, so that the perpendicularity of the erected rocket body can be adjusted, and support can be provided; the lifting system is installed on the erecting arm and can send an operator to the front binding point and the rear binding point of the rocket to achieve rocket connection. The erecting vehicle can achieve transportation and transfer of rockets, the rockets are erected as a whole after arriving at a launching area, and erecting work before launching is completed rapidly.

Description

technical field [0001] The invention relates to the technical field of aerospace ground support equipment, in particular to a multi-stage rocket transportation erector. Background technique [0002] At present, the hoisting operation mode is adopted for the erection of domestic rockets before launch, especially for multi-stage rockets, the assembly process takes a long time, the operation process is complicated, the standardization and automation are low, the on-site command and coordination is difficult, and the safety of the hoisting process is affected. Human factors have a greater influence. This method also has problems such as low operating efficiency, long time of occupying the launching station, and the hoisting link is easily affected by wind force. Therefore, the erection link of rocket launch urgently needs standardized equipment that is simpler and faster, has standardized operating procedures, a high degree of automation, and more secure safety. For this reaso...

AI Technical Summary

Problems solved by technology

[0002] At present, the hoisting operation mode is adopted for the erection of domestic rockets before launch, especially for multi-stage rockets, the assembly process takes a long time, the operation process is complicated, the standardization and automation are low, the on-site command and coordination is difficult, and the safety of the hoisting process is affected. Human factors have a greater influence

This method also has problems such as low operating efficiency, long time occupation of the launch station, and the lifting link is easily affected by wind force.

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