白丝美女被狂躁免费视频网站,500av导航大全精品,yw.193.cnc爆乳尤物未满,97se亚洲综合色区,аⅴ天堂中文在线网官网

System and method for producing electromagnetic thrust

專利號
US12160188B2
公開日期
2024-12-03
申請人
Jeffrey R. Ambroziak
發(fā)明人
Jeffrey R. Ambroziak
IPC分類
H02N11/00; B64G1/40
技術(shù)領(lǐng)域
wire,ns,craft,wires,flowing,magnetic,current,page,force,thrust
地域： CT CT Guilford

摘要

A method for producing thrust via the asynchronous transmission of current through two generally parallel wires.

說明書

1 2 3 4 5 6 7 8 9 10 11 12 13 14
CROSS REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of U.S. Provisional Patent Application 63/282,282, filed Nov. 23, 2021, entitled “SYSTEM AND METHOD FOR PRODUCING ELECTROMAGNETIC THRUST”, the entire disclosure of which is hereby incorporated herein by reference.

FIELD OF THE INVENTION

The present invention relates to systems and methods for producing electromagnetic thrust.

BACKGROUND

Various different technologies are commonly employed to launch rockets into low earth orbit, lunar orbit and on interplanetary missions as well as, in the case of Voyager, interstellar travel. Most commonly, liquid hydrogen and liquid oxygen are combined and ignited to create a controlled explosion pushing mass away from a craft resulting in an equal and opposite force forcing the mass of the craft into space. The great amount of energy released in such an explosion results in the rapid, if relatively brief, acceleration of the craft through the earth's atmosphere and into space. Additional thrusts may be applied to maneuver the craft, to perform subsequent burns of the engines and to slow the craft down when entering orbit around another body.

Because the fuel consumption required for a mission profile requiring achieving earth orbit is so great, there is not left over much fuel to hurl the craft towards a distant planet. Further, as the engines tend to remain dormant for months or even years before decelerating the craft, there exists the danger that the engines will not reignite.

權(quán)利要求

1
What is claimed is:1. A method for producing thrust comprising:transmitting through a first wire a first current defined by a first waveform comprising a positive current value, I1, for a first period of time, no current for a second period of time, a negative current value, ?I1, for a third period of time and no current for a fourth period of time, wherein the first period, the second period, the third period and the fourth period are all approximately equal in duration, wherein the first waveform repeats itself, and wherein the first wire is affixed to a substrate; andtransmitting through a second wire a second current defined by a second waveform comprising the first waveform time shifted by an amount of time approximately equal to the first period of time wherein the second wire is affixed to the substrate, is generally parallel to the first wire, and is separated by a distance, d;wherein each period of time is approximately equal to an amount of time required for light to travel the distance, d.2. The method of claim 1, wherein at least one of the first wire and the second wire comprise a superconductor.3. The method of claim 2, wherein the superconductor comprises metallic hydrogen.4. The method of claim 1, wherein at least one of the first current and the second current is produced by a nuclear reactor.5. The method of claim 1, wherein the nuclear reactor is a small modular reactor (SMR).6. The method of claim 1, wherein the substrate forms a part of a spacecraft.7. The method of claim 1, wherein both of the first wire and the second wire are bent to form at least a portion of a circle.
微信群二維碼
意見反饋