The operation of the ultra-high frequency (UHF) electromagnetic motor or thruster, is based on generating extremely short and powerful electrical, magnetic or electromagnetic field pulses and separating (unrooting) or disassociating said field pulses from the originating source, so that subsequently the emitting device and a device that is the objective or target, a support structure that supports both devices and another elements connected to said support structure are for an instant disassociated from the field, waiting for the pulsed field to reach the objective or target. At that moment, the element emits a field with a polarization that allows the exertion of a force that attracts or repels the field pulse, with respect to the objective or target and consequently with respect to the motor of which they form part as a unit, both the emitter and the target being joined by a support structure.

An electromagnetic propulsion system for the movement of spacecraft by means of ejection of the perturbed dark matter. In the present invention, to perturb and accelerate the dark matter, the electromagnetic energy generated by microwave generators is supplied to a number of position-adjustable electromagnetic vibrators that form a phased antenna array inside the waveguide. Since the dark matter permeates the Universe and its reserves are unlimited, it can be used as a working medium in the constant acceleration propulsion system for as long as the electric power supply lasts. Since the electromagnetic propulsion system has infinite reserves of the working medium, the specific impulse is also infinite. The speed of the dark matter jet approaches the speed of light.

An electromagnetic propulsion system for the movement of spacecraft by means of ejection of the perturbed dark matter. In the present invention, to perturb and accelerate the dark matter, the electromagnetic energy generated by microwave generators is supplied to a number of position-adjustable electromagnetic vibrators that form a phased antenna array inside the waveguide. Since the dark matter permeates the Universe and its reserves are unlimited, it can be used as a working medium in the constant acceleration propulsion system for as long as the electric power supply lasts. Since the electromagnetic propulsion system has infinite reserves of the working medium, the specific impulse is also infinite. The speed of the dark matter jet approaches the speed of light.

Numerous patents have been granted for methods to extract useful zero-point energy (ZPE). However, these methods utilize the Casimir force, which is orders of magnitude too small to power an electrical grid. The method and apparatus described here uses counter-rotating mercury based plasmas pulsed with a high frequency, high voltage discharge to create a coherence with the zero-point field, allowing for unlimited extraction of ZPE, which may ultimately replace polluting fossil fuel derived energy. Mainstream physics models gravity as a curvature of space (general relativity), but there are profound problems with this model. An alternative model of gravity advanced by some physicists models gravity (and inertia) as an induced effect resulting from the interaction of ZPE with subatomic charge. By creating a coherence with the zero-point field, this method causes an interference with this interaction, allowing gravity and inertia to be engineered or nullified, representing a breakthrough in propulsion.

The present disclosure provides a thruster device. The device includes a force-generating element mounted to a housing. The element is configured to generate a thrust force for propelling the housing. The element including a first electrode connected to a first input terminal of a power source. A second electrode is spaced apart by a predetermined distance from the first electrode and connected to a second input terminal of the power source. The second electrode includes a second longitudinal axis oriented parallelly to a first longitudinal axis. A dielectric medium is disposed between the electrodes. Upon receiving field emission condition, charged particles available at the first electrode accelerate towards the second electrode for generating a thrust force along a direction of movement of the charged particles. The thrust force is generated when the predetermined distance between the electrodes is shorter than a Rindler horizon defined by the charged particles during acceleration.

A magnetic field propulsion unit includes a first magnetic field generating device (“FMFGD”) generating a magnetic field; a second magnetic field generating device (“SMFGD”) generating a magnetic field; an energy supply unit providing the FMFGD and the SMFGD with electrical energy; and a control unit controlling the energy supply unit in accordance with a predefined switching scheme. The SMFGD is a rod-like antenna that lies in a plane in which also the FMFGD lies. The control unit is: supplying the SMFGD with electrical energy so that a second magnetic field surrounding the SMFGD is generated; supplying the FMFGD with electrical energy so that a first magnetic field surrounding the FMFGD is generated. The FMFGD is supplied with electrical energy a predetermined period of time after the SMFGD is supplied with electrical energy.

Levitation and Propulsion Unit-2 (LPU-2) is a thrust generating device able to generate resultant force to create motion without mass flow and/or momentum exchange. The technology primarily uses electromagnetic energy, permanent magnetic repulsive energy and kinetic energy, to generate internal resultant thrust or motion. This thrust generating device comprises of one or two rapid action enable and high driving force electromagnet moving magnet linear actuators with minimum moving parts. The technology mainly leverages on compression and expansion of compressed repulsive magnetic flux. Through regulation and systematic control of current to each electromagnet, the device is able to generate resultant force or motion without external interaction.

A filtering apparatus formed by a plurality of channel systems. Each of the channel systems include an inlet port formed on an inlet side of the plate; no more than one outlet port formed on an outlet side of the plate; and a channel formed in the plate, the channel coupled to the inlet port and to the outlet port, wherein the ratio of the product of the capture area of the inlet ports of a channel system with the first transmissivity associated with the inlet ports to the product of the capture area of the outlet ports of a channel system with the second transmissivity associated with the outlet ports is greater than one. The channel system is configured to interact with objects of interest on a scale which is smaller than a value several orders of magnitude larger than the mean free path of an object of interest. Some plate embodiments are configured to interact with particles, such as air molecules, water molecules, or aerosols. Other plate embodiments are configured to interact with waves or wavelike particles, such as electrons, photons, phonons or acoustic waves.

The planar electric motor for aerospace use is a one hundred percent electric thruster or motor and consists of a device capable of generating a thrust force on itself regardless of the environment around it even in vacuum or outer space. The impulse of the motor is produced by the interaction of the force fields generated by the current flowing through a primary conductor and a secondary conductor placed adjacent and parallel to the first conductor one, both being separated by means of an insulating material, the secondary conductor is interrupted, so that in order to complete the circuit, the charge carriers must jump the free space that constitute the secondary conductor breach, to achieve this the motor employs extremely brief high voltage pulses producing small impulses produce by the force of repulsion between both parallel currents that runs in opposite directions.

A propulsion system providing at least one of propulsion and lift comprising a source of a molecular beam or jet, a plasma generator coupled to the source, a plasma chamber coupled to the source and to the plasma generator to maintain a hydrogen plasma comprising free electrons and H+ ions, a microwave generator, a horn antenna, and a negatively charged, repulsive electrode to repel received electrons that have absorbed microwaves in a directional manner and gained reactionless kinetic energy in a directional manner.