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.
LAUNCH SYSTEM AND METHOD FOR ECONOMICALLY EFFICIENT LAUNCH
STARTSYSTEM UND VERFAHREN FÜR EINEN ÖKONOMISCH EFFIZIENTEN START
SYSTÈME DE LANCEMENT ET PROCÉDÉ DE LANCEMENT ÉCONOMIQUEMENT EFFICACE
2018-10-03
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F41A Funktionsmerkmale oder Einzelheiten, die Handfeuerwaffen und Artillerie gemeinsam betreffen, z.B. Rohre , FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS / F41B WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE , Waffen zum Verschießen von Geschossen ohne Verwendung von Explosiv- oder Treibladungen / F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / F42C AMMUNITION FUZES , Munitionszünder |
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