The present disclosure relates to a launch system, and methods of launching a 5 payload utilizing the launch system. The disclosure can provide for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location. The launch system can comprise: 1) a launch tube comprising a plurality of conductive layers separated by one or more insulating layers and being configured for transmission of energy therethrough; and 2) an electrical energy source; wherein 10 the launch tube is configured for propulsion of a launch vehicle therethrough, and the launch system is configured to be electroantimagnetic. An electrical energy source also can be provided. 11809219_1 (GHMatters) P101112.AU.2 20250 11013 1020 100 -135 113a / 230130 210 xx 115 220 240 260 113b 112
Launch vehicle and system and method for economically efficient launch thereof
2021-01-07
Patent
Elektronische Ressource
Englisch
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