An object of the present invention is to achieve a simple and safe nuclear fusion reactor. The nuclear fusion reactor comprises: a vessel serving as a reactor body; a metallic heating element that contains heavy hydrogen contained in the vessel as a solute; a heavy hydrogen gas contained in the vessel, the heavy hydrogen gas being in an amount that allows 0.005% to 5% of heavy hydrogen to be contained as a solute in the metallic heating element based on the atomic ratio; and a mechanism for irradiating the metallic heating element with an ion beam. Such configuration causes, in the metallic crystal of the metallic heating element, a channeling phenomenon which guides ion beams to interstitial atom nuclei, and an intra-metal nuclear fusion probability increasing phenomenon which is explained based on the binary nucleus model. As a result, a mild nuclear fusion that does not emit gamma rays and neutron rays occurs, and the nuclear energy can be efficiently converted into heat due to the intra-metal nuclear fusion chain reaction.

A method of controlling a plasma in a nuclear fusion reactor. The nuclear fusion reactor comprises sensors and plasma control inputs. An initial control model is provided, relating readings of at least a subset of the sensors to control of the plasma control inputs. A control loop is performed, comprising: operating the plasma control inputs in dependence upon the sensors according to the control model; determining correlations between readings of each of the sensors, and/or between readings of the sensors and states of the plasma control inputs; and adjusting the control model based on the determined correlations.

The invention is for a startup system for nuclear fusion engines in space. The combustion of hydrogen and oxygen produces heat that is used by a heat engine to produce electricity. This can be supplemented by electricity from other operating engines. The exhaust from the combustion is condensed and electrolyzed to produce hydrogen and oxygen once the engine is in operation. This provides a constant source of energy for future startups. The engine is started up at partial power in electricity generation mode and this power replaces the power from the combustion as it grows. The combustor uses the same heat engine as the nuclear engine uses for power generation.

The invention is for a startup system for nuclear fusion engines in space. The combustion of hydrogen and oxygen produces heat that is used by a heat engine to produce electricity. This can be supplemented by electricity from other operating engines. The exhaust from the combustion is condensed and electrolyzed to produce hydrogen and oxygen once the engine is in operation. This provides a constant source of energy for future startups. The engine is started up at partial power in electricity generation mode and this power replaces the power from the combustion as it grows. The combustor uses the same heat engine as the nuclear engine uses for power generation.

A method of controlling a plasma in a nuclear fusion reactor. The nuclear fusion reactor comprises sensors and plasma control inputs. An initial control model is provided, relating readings of at least a subset of the sensors to control of the plasma control inputs. A control loop is performed, comprising: operating the plasma control inputs in dependence upon the sensors according to the control model; determining correlations between readings of each of the sensors, and/or between readings of the sensors and states of the plasma control inputs; and adjusting the control model based on the determined correlations.

A plasma compression system comprises a plasma containment vessel, an annular rotating core inside the vessel, and a plurality of compression drivers fixedly mounted to an outer surface of the vessel wall. The annular rotating core contains a liquid medium and is rotatable to circulate the liquid medium and form a liquid liner with a cavity. The rotating core comprises an outer surface spaced from an inner surface of the vessel wall to define an annular gap, and a plurality of implosion drivers each comprising a pusher bore with a pusher piston slideable therein. Each pusher bore extends through the rotating core. The plurality of compression drivers compresses a compression fluid in the annular gap and creates a pressure pulse, such that when the rotating core rotates and the liquid medium fills the pusher bores, the pusher pistons are operable to push the liquid medium inwards to collapse the liquid liner and compress a plasma in the cavity.

A control system manipulates one or more of the shape, timing, and magnitude of a pressure pulse (plasma pulse trajectory) generated by a plasma compression system to implode a liquid liner surrounding a cavity containing plasma, thereby compressing the plasma. The liquid liner and cavity are created by rotating a liquid medium in a vessel. Compression drivers extend perpendicularly around the liquid medium's rotational axis. Multiple layers of compression drivers are stacked in an axial direction parallel to the rotational axis to form multiple pressure zones extending along the rotational axis. The control system separately controls each pressure zone, or groups of pressure zones, to generate individual pressure pulses each having a different pressure pulse trajectory in each pressure zone. The multiple individual pressure pulses collectively form a combined pressure pulse having a pressure pulse trajectory that varies along the rotational axis.

Methods, apparatus, devices, and systems for creating, controlling, conducting, and optimizing fusion activities of nuclei. In particular, the present inventions relate to, among other things, fusion activities that are conducted individually or collectively on a very small scale, preferably on the nano-scale or smaller such as pico to femto scales, for the utilization of energy produced from these activities in smaller devices and for aggregation into larger devices.

An ion generator including a vacuum chamber; an anode in the chamber, and two movable cathodes in the chamber whereby the distance of the cathodes relative to the anode can be varied. A servo actuated motor can be operably connected to each movable cathode to move the cathodes in the chamber and modify the plasma generated.

An ion generator including a vacuum chamber; an anode in the chamber, and two movable cathodes in the chamber whereby the distance of the cathodes relative to the anode can be varied. A servo actuated motor can be operably connected to each movable cathode to move the cathodes in the chamber and modify the plasma generated.