LAUNCH SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH

摘要

The present disclosure relates to a launch system (20) comprising a launch tube (100) comprising a plurality of conductive layers separated by one or more insulating layers and being configured for transmission of energy therethrough; and an electrical energy source (300); wherein the launch tube (100) is configured for propulsion of a launch vehicle (200) therethrough, and the launch system (20) is configured to be electroantimagnetic, preferably wherein the launch tube (100) is configured to be electroantimagnetic such that any magnetic field formed by passage therethrough of an electrical current of about 0.2 to about 2 million amps is at a strength of less than about 1.25 Tesla.