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US20120110978 |
Absolute universal engine, one from ground to orbit
This invention relates to absolute universal engine for aviation, from ground to orbit and space, by total integration of all modes of operation, turbo fan subsonic, turbo jets supersonic, turbo... |
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US20060070371 |
Electric dipole moment propulsion system
A spacecraft propulsion system utilizing a rotating octagon of trapezoidal electrically charged flat panels to create an electric dipole moment that generates lift on the hull. |
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US20090165437 |
Drive device on the basis of a gel-type propellant and method for conveying propellant
In order to make a drive device available on the basis of a gel-type propellant, in particular, for a flying object, comprising at least one tank for gel-type propellant, a combustion chamber and... |
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US20080134663 |
Heat Transfer Thruster
A heat transfer thruster by which performance can be enhanced by realizing optimal temperature distribution for heating propellant without complicating the structure. In the heat transfer... |
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US20060112673 |
Photoelectric propulsion drive
This invention is a device(s) that will utilize the power of photons to transfer their energy to electrons in turn transferring their energy to another object of mass that the casing(s) of the... |
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US20110000185 |
Fusion energy process
This invention relates to a nuclear fusion reaction process utilizing a B-11 isotope ion spherical plasma. Said spherical plasma will be formed on roof of a ferromagnetic chromium steel hulled... |
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US20060168937 |
Magnetic monopole spacecraft
A spacecraft propulsion system that utilizes a dual method of providing lift on the hull by means of magnetic monopoles and electromagnetic spacetime curvature pressure. |
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US20100024385 |
PULSED PLASMA THRUSTER AND METHOD OF OPERATION THEREOF
A pulsed plasma thruster and method of operation are provided. The pulsed plasma thruster comprises solid propellant material. A main discharge source provides a pulsed discharge across the... |
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US20100058734 |
METHOD OF ENHANCING MICROTHRUSTER PERFORMANCE
Coaxial micronozzle designs are presented. Initial coaxial micronozzle designs utilizing center-body geometries to better exploit pressure thrust show a potential threefold increase in specific... |
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US20060144035 |
Photon spacecraft
A spacecraft propulsion system utilizing photon particles to create negative energy over the hull in order to generate a lift force on the hull. |
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US20090120056 |
Microthruster, in particular for use as a position adjustment thruster, thruster and method for producing a microthruster
Microthruster includes a combustion chamber comprising a substrate material, a fuel inlet, and a gas outlet. A first resistance heater is arranged in the combustion chamber. A catalyst is... |
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US20150210406 |
Fuel-Free Spacecraft Propelling System Based on Spatial Atomic Oxygen and Propelling Method
A fuel-free spacecraft propelling system having an open-ended outer cylinder of a propelling device and an atomic oxygen collecting device is disclosed. The latter is arranged at the... |
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US20070113535 |
Dual-plasma-fusion jet thrusters using DC turbo-contacting generator as its electrical power source
New [GerTh-DawShien. V] dual-plasma flying object and [GerTh-DawShien. VI] dual-plasma-fusion flying object provide the electric start system to start their warm-up process to their steady-states,... |
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US20120304618 |
METHOD AND APPARATUS FOR SMALL SATELLITE PROPULSION
In a propulsion system, an electrohydrodynamic (EHD) body force is used to control the flow of a propellant through a micro channel, expansion slot, plenum chamber, or other flow region and... |
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US20150040536 |
EXTERNALLY POWERED HYBRID PROPULSION SYSTEM
A hybrid propulsion system for a vehicle comprises a propellant tank for providing a supply of propellant, a propellant heater, and an exhaust nozzle. The propellant tank is in fluid communication... |
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US20150211499 |
ELECTROTHERMAL DEVICE FOR A PROPULSION SYSTEM, ESPECIALLY FOR A TURBOJET, PROPULSION SYSTEM COMPRISING SUCH AN ELECTROTHERMAL DEVICE, AND ASSOCIATED METHOD
An electrothermal device (1, 100) includes a primary chamber (2) having an anode nozzle (6) provided with an inlet passage (7), a cathode tip (9) at least partially inserted into the inlet passage... |
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US20080163605 |
PULSED PLASMA THRUSTER AND METHOD OF MAKING
A pulsed plasma thruster (PPT) and a method of making the pulsed plasma thruster are disclosed. The PPT includes no moving parts and is able to achieve a small size. The PPT is also designed to... |
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US20150000251 |
System, Method and Apparatus for Lean Combustion with Plasma from an Electrical Arc
The present invention provides a plasma arc torch that can be used for lean combustion. The plasma arc torch includes a cylindrical vessel, an electrode housing connected to the first end of the... |
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US20100242475 |
Systems and Methods of Thermal-Electric Power Generation Including Latent Heat Utilization Features
Systems and methods are disclosed related to utilization of energy including utilization of latent energy from electricity generating processes. According to one exemplary implementation, steam is... |
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US20090056304 |
Solar energy augmented jet aircraft
A solar energy augmented jet aircraft uses solar energy as the energy source for dielectric heating of a jet engine exhaust gas stream thereby increasing thrust. |
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US20060042224 |
Dual-plasma jet thruster with fuel cell
New [GerTh. I] & [DawShien. II] dual-plasma jet thrusters provide the electric start system to start their warm-up processes, automatically. After their warm-up processes done and the operation... |
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US20140013724 |
ELECTROMAGNETIC THRUSTER
Systems and methods for electromagnetic thrusting are disclosed. An electromagnetic thrusting system includes an axially-asymmetric resonant cavity including a conductive inner surface, the... |
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US20070000231 |
Cooling apparatus for vehicle electrical packaging unit
A cooling apparatus for a vehicle electrical packaging unit that includes an inverter for a vehicle drive motor, a DC-DC converter for a vehicle control power source, and an electrical power... |
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US20150252795 |
Electrostatic Thruster
The electrostatic thruster is an electrostatic propulsion device which produces a force by making the grounded conductors and the charged conductor composing the device experience a stronger... |
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US20170175565 |
Hybrid Propulsion System
An aeronautical propulsion system includes a fan having a plurality of fan blades and an electric motor drivingly connected to the fan for rotating the plurality of fan blades. A chemically... |
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US20170129628 |
Thermal-nucleak powered rocket using non-cryogenic propellant
The invention comprises a space ship, which commutes between earth orbit and lunar orbit, and is powered by a rocket engine, using superheated steam, or other non-cryogenic propellant, where the... |
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US20170082124 |
Directed Energy Deposition to Facilitate High Speed Applications
The present invention relates to methods, apparatuses, and systems for controlling the density of a fluid near a functional object in order to improve one or more relevant performance metrics. In... |
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US20160327029 |
LOW PRESSURE DIELECTRIC BARRIER DISCHARGE PLASMA THRUSTER
Some embodiments of the invention include a thruster system comprising a thruster and a pulsing power supply. The thruster may include a gas inlet port; a plasma jet outlet; and a first electrode.... |
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US20160305320 |
Circular propulsion jet compressor-engine
Circular propulsion jet compressor-engine, through a circular combustion chambers propellants spheroidal geometry set, generates a tangential push the turning radius and therefore resulting... |
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US20160169214 |
PLASMA ACTUATING PROPULSION SYSTEM FOR AERIAL VEHICLES
A plasma propulsion nozzle incorporates a cylinder having an inlet and an outlet. A plurality of substantially cylindrical planarly disbanded electrodes with sandwiched dielectric spacers is... |
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US20160146197 |
BATTERY POWERED VEHICLE PROPULSION SYSTEM
A vehicle propulsion system includes an air heating chamber that receives inlet air from an air intake chamber and provides thrust through an exhaust chamber. A battery powered pulse generator... |
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US20160086680 |
Positron Systems for Energy Storage, Production and Generation
A positron based system is disclosed which extracts electric power from matter-antimatter annihilation reactions between electrons and positrons. In one embodiment, for storage and distribution of... |
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US20160076450 |
Solar Jet Turbofan Aircraft Engine
The Solar Jet Turbofan Aircraft Engine is a system and method for utilizing electrical heating elements to heat compressed air within a jet engine's “Heating Chamber” in order to increase or... |
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US20160047364 |
METHOD AND SYSTEM FOR A PROGRAMMABLE AND FAULT TOLERANT PULSED PLASMA THRUSTER
A system and method provides a fault-tolerant multi-channel pulsed plasma thruster system utilizing a control unit and an embedded real time application manipulating low-level timing events with... |
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US20160032906 |
PLASMA DRIVE
A plasma drive includes a plurality of plasma thrusters arrayed in each of at least one array of plasma thrusters. Plasma thrust may be generated sequentially or in a pulse from each array.... |
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US20150373826 |
ION ACCELERATORS
An ion accelerator includes: an inner magnet having a channel extending through it in an axial direction; an outer magnet extending around the inner magnet, the magnets having like polarities so... |
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US20150052874 |
MICRO-CATHODE THRUSTER AND A METHOD OF INCREASING THRUST OUTPUT FOR A MICRO-CATHODE THRUSTER
A magnetically enhanced micro-cathode thruster assembly provides long-lasting thrust. The micro-cathode thruster assembly includes a tubular housing, a tubular cathode, an insulator, an anode and... |
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US20140084115 |
FLIGHT CONTROL USING DISTRIBUTED MICRO-THRUSTERS
A method and apparatus to control movement of a vehicle using a plurality of thrust-producing devices formed in at least one control surface is disclosed. A supply of power to the plurality of... |
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US20140075917 |
FAULT TOLERANT CONTROL SYSTEM FOR DISTRIBUTED MICRO-THRUSTERS
A control system for controlling the operation of a plurality of micro thrusters arranged in a plurality of parallel horizontal rows and a plurality of parallel vertical columns, the control... |
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US20130014486 |
Fiber laser powered thruster
A fiber laser powered, optical to thermal conversion thruster with improved practicality and operational and design flexibility. |
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US20120167548 |
PLASMA THRUSTERS
A plasma thruster includes a plasma chamber having first and second axial ends, the first of which is open, an anode located at the second axial end, and a cathode. The cathode and anode are... |