New Generations of Rocket Engines

D. Sobolewski, M. Sobolewski, Marek Juliusz Sobolewski, Joanna Paulina Sobolewska, N. Sobolewska
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Abstract

The article, based on mathematical model of the space and particles revealed in "Theory of Space" (Sobolewski D. S., Theory of Space, 2016) (Sobolewski D. S., Theory of Space, 2017) and the description of the propagation of photons stated in publication entitled “Geometry of the Dark Matter and Preliminary Analysis of Alpha and Beta Photons’ Properties Based on Theory of Space” (Sobolewski, Sobolewski i Sobolewski, 2017), describes transverse waves propagating in space, including gravitational, fluctuating and matter waves. In particular, it focuses on waves of matter in which orientation of the spatial channels, connecting four-dimensional boundary hypersurfaces  and , had been stabilised. For this type of the wave of matter the minimum energy value for deformation of boundary hypersurfaces of the matter waves  has been appointed, which is smaller by several orders of magnitude than energy needed to change the orientation of vertical disturbances of space which connect four-dimensional boundary hypersurfaces and, The obtained results were used to introduce a new classification of rocket engines and to provide examples of their implementation. Furthermore, the article demonstrates first attempts to construct a rocket engine of the new type, including description of the principle of operation of the engine, which is subject of patent application entitled "HTS Photonic Rocket Engine" (Poland Patent nr P.421517, 2017), as well as presents an example of spacecraft shell implementation, which enables stabilization of orientation of its spatial channels. The Article thus reveals new perspectives for interplanetary travel through significant increase in spacecraft velocities, while simultaneously reducing the energy required to achieve them. In addition, the article describes interaction of photons  with the boundary hypersurface , while determining the change in photon frequency depending on its curvature .
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新一代火箭发动机
本文基于《空间理论》(Sobolewski D. S.,《空间理论》,2016)(Sobolewski D. S.,《空间理论》,2017)中揭示的空间和粒子的数学模型,以及题为《暗物质的几何和基于空间理论的α和β光子性质的初步分析》(Sobolewski, Sobolewski i Sobolewski, 2017)的出版物中对光子传播的描述,描述了在空间中传播的横向波,包括引力、波动和物质波。特别是,它关注的是连接四维边界超表面和的空间通道方向已经稳定的物质波。对于这种类型的物质波,确定了物质波边界超表面变形的最小能量值,它比改变连接四维边界超表面的空间垂直扰动的方向所需的能量小几个数量级,并利用所得结果介绍了一种新的火箭发动机分类,并提供了其实现的实例。此外,本文还展示了构建新型火箭发动机的首次尝试,包括描述了发动机的工作原理,这是专利申请的主题,名为“HTS光子火箭发动机”(波兰专利号P.421517, 2017),并提供了一个航天器外壳实现的例子,该外壳能够稳定其空间通道的方向。因此,这篇文章揭示了星际旅行的新视角,通过显著增加航天器速度,同时减少实现它们所需的能量。此外,本文描述了光子与边界超表面的相互作用,同时确定了光子频率随其曲率的变化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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