Magnetic suspension electromagnetic boost based aircraft launch system

Abstract

The invention provides a magnetic suspension electromagnetic boost based aircraft launch system. The system includes a track subsystem, a sled vehicle subsystem, an electromagnetic boost subsystem, anaircraft subsystem and an integrated command and control subsystem; the track subsystem is used for providing suspension force and guidance force required by launch tracks and systems for the aircraft subsystem; the sled vehicle subsystem is used for bearing the aircraft subsystem to realize launching on the track subsystem; the electromagnetic boost subsystem is used for providing propulsive force required by the driving of the sled vehicle subsystem and the aircraft subsystem; the aircraft subsystem is used for loading cargos or conveying passengers and can be operated on the track subsystem; and the integrated command and control subsystem is connected to the track subsystem, the sled vehicle subsystem, the electromagnetic boost subsystem and the aircraft subsystem through a network soas to monitor the real-time working states of each subsystem and issue control instructions. Thus, the two-stage-to-orbit aerospace aircraft launch system which can be completely and repeatedly usedcan be realized.

Description

technical field [0001] The invention relates to the technical field of magnetic levitation and electromagnetic propulsion, in particular to an aircraft launch system based on magnetic levitation electromagnetic boost. Background technique [0002] The traditional space launch mainly uses the infrastructure of the space launch site (including the technical area and the launch area) to support the launch of the launch vehicle. The traditional launch method is transferred from the technical area to the launch tower for launch, which requires the coordination of personnel, tooling, logistics, transportation, and a large amount of resources. The workload is large and the work is highly related. A problem in one link may even directly delay the entire launch task. The entire operation process lasts for several days, and the operating cost accounts for a large proportion of the total launch cost. [0003] The traditional launch tower is mainly suitable for the launch of carrier ro...

AI Technical Summary

Problems solved by technology

[0004] In addition, with the existing launch method, the launch platform and diversion surface are all within the direct damage range of the gas flame and its rebound flame, and the damage range of vibration and high-temperature radiation is relatively wide. All facilities near the launch location may be damaged by Vibration and high-temperature radiation cause loosening, deformation or even functional failure. Before the next launch, necessary measures must be taken to repair and maintain the launch facilities such as anti-ablation and reinforcement.

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