American Journal of Aerospace Engineering

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On Optimal Trajectory in Space Flight

Received: 18 July 2015    Accepted: 21 March 2016    Published: 12 April 2016
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Abstract

Are investigated a trajectory of new type in distant, space flights unlike usual trajectories of direct flight to heavenly object (Moon) it is supposed to use asymmetry of a gravitational field and to carry out flight bypassing the most power gravitational impact on the spacecraft. It leads to economy of power for 20-30%.

DOI 10.11648/j.ajae.20160302.11
Published in American Journal of Aerospace Engineering (Volume 3, Issue 2, April 2016)
Page(s) 6-12
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

The Theory of Vortex Gravitation, Space Flights with an Optimum Trajectory

References
[1] S. Orlov. Foundation of vortex gravitation, cosmology and cosmogony. Global journal of science Frontier research. Physic and Space Science Volume 12 issue 1 Version 1.0 January 2012 https://globaljournals.org/GJSFR_Volume12/3-Foundation-of-vortex-gravitation-cosmology.pdf
[2] L V Kiknadze, Yu G Mamaladze. Classical hydrodynamics for physicists-experimentalists. Tbilisi University Press. Tbilisi, Georgia. 1979. Page 136.
[3] A P Gulyaev. Astronomy calendar. Cosmosinform. Moscow, Russia. 1993. Page 285.
Author Information
  • Petrozavodsk State University, Petrozavodsk, Russia

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    Sergey Orlov. (2016). On Optimal Trajectory in Space Flight. American Journal of Aerospace Engineering, 3(2), 6-12. https://doi.org/10.11648/j.ajae.20160302.11

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    ACS Style

    Sergey Orlov. On Optimal Trajectory in Space Flight. Am. J. Aerosp. Eng. 2016, 3(2), 6-12. doi: 10.11648/j.ajae.20160302.11

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    AMA Style

    Sergey Orlov. On Optimal Trajectory in Space Flight. Am J Aerosp Eng. 2016;3(2):6-12. doi: 10.11648/j.ajae.20160302.11

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  • @article{10.11648/j.ajae.20160302.11,
      author = {Sergey Orlov},
      title = {On Optimal Trajectory in Space Flight},
      journal = {American Journal of Aerospace Engineering},
      volume = {3},
      number = {2},
      pages = {6-12},
      doi = {10.11648/j.ajae.20160302.11},
      url = {https://doi.org/10.11648/j.ajae.20160302.11},
      eprint = {https://download.sciencepg.com/pdf/10.11648.j.ajae.20160302.11},
      abstract = {Are investigated a trajectory of new type in distant, space flights unlike usual trajectories of direct flight to heavenly object (Moon) it is supposed to use asymmetry of a gravitational field and to carry out flight bypassing the most power gravitational impact on the spacecraft. It leads to economy of power for 20-30%.},
     year = {2016}
    }
    

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