Matches 1 - 41 out of 41


Match Document Document Title
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...
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.
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...
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...
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...
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...
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.
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...
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...
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.
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...
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...
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,...
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...
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...
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...
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...
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...
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...
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.
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...
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...
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...
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...
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...
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...
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...
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....
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...
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...
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...
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...
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...
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...
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....
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...
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...
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...
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...
US20130014486 Fiber laser powered thruster  
A fiber laser powered, optical to thermal conversion thruster with improved practicality and operational and design flexibility.
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...

Matches 1 - 41 out of 41