Title:
SPACE NUCLEAR FUSION ROCKET (ENGINE) ENERGY SYSTEM OF KAZUTORA YOSHINO
Document Type and Number:
Japanese Patent JP2018048555
Kind Code:
A
Abstract:
This invention relates to a spaceship which travels by injecting a jet. It is necessary to sufficiently secure a cross section (contact cross section area) of a D(deuterium) particle flux. That is, an ion gas is created of D2O, or a plasma is created of D2, a positive ion (D(deuterium) particle, (D+ion)), and a negative ion (electron, (OD-ion)) are separated from each other by using a magnetic field (and electrical field), high-density D(deuterium) particle flux beams are created by using D(deuterium) particles in a high magnetic field (and electrical field), and accelerated by an accelerator, and the D(deuterium) particle flux beams are made to collide with each other, thus creating a nuclear fusion reaction. A gradient is applied to the energy of the nuclear fusion, a reactant (helium (He)) is made to possess directionality, and a propulsion force (propulsion energy) is obtained by jet injection.SELECTED DRAWING: Figure 1
Inventors:
YOSHINO KAZUTORA
Application Number:
JP2013004163A
Publication Date:
March 29, 2018
Filing Date:
January 15, 2013
Export Citation:
Assignee:
YOSHINO KAZUTORA
International Classes:
F03H1/00; G21B1/00; G21B3/00