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MICRO-FUSION-POWERED AIR AND SPACE CRAFT

机译:微熔空气和空间工艺

摘要

A micro-fusion powered craft has a centrally located internal chamber with an upper dome and a bottom opening. The chamber is radially surrounding by the main body of the craft. Ports from a fuel supply in the main body inject a deuterium-containing micro-fusion fuel material as a dispersed cloud within the chamber. Ambient cosmic rays and muons penetrate the upper dome into the chamber and interact with the fuel to produce energetic reaction products. The downwardly directed portion of the reaction products exist the chamber through the bottom opening to produce upward reaction thrust, while the upwardly directed portion of the reaction products are stopped by the upper dome to produce applied upward thrust. The craft may have one or more side ports for dispersing fuel material externally in a desired direction that reacts with ambient cosmic rays and muons to produce reaction products, at least some of which are received by a side of the craft to produce lateral thrust.
机译:微融合动力飞行器具有位于中央的内部腔室,该内部腔室具有上部圆顶和底部开口。该腔室被飞行器的主体径向地包围。来自主体中燃料供应的端口将含氘的微融合燃料材料注入室内,作为分散的云。周围的宇宙射线和介子穿透上部圆顶进入燃烧室,并与燃料相互作用以产生高能的反应产物。反应产物的向下定向部分通过底部开口存在于腔室中以产生向上的反作用力,而反应产物的向上定向的部分被上部穹顶阻止以产生施加的向上的反作用力。该飞行器可以具有一个或多个侧端口,用于沿期望的方向在外部分散燃料材料,该燃料端口与周围的宇宙射线和介子反应以产生反应产物,其中至少一些被该飞行器的一侧接收以产生横向推力。

著录项

  • 公开/公告号US2020231309A1

    专利类型

  • 公开/公告日2020-07-23

    原文格式PDF

  • 申请/专利权人 JEROME DREXLER;

    申请/专利号US201916251524

  • 发明设计人 JEROME DREXLER;

    申请日2019-01-18

  • 分类号B64G1/40;B64G1/26;G21H7;G21B3;

  • 国家 US

  • 入库时间 2022-08-21 11:24:19

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