On Optimal Trajectory in Space Flight
American Journal of Aerospace Engineering
Volume 3, Issue 2, April 2016, Pages: 6-12
Received: Jul. 18, 2015; Accepted: Mar. 21, 2016; Published: Apr. 12, 2016
Views 4532      Downloads 228
Author
Sergey Orlov, Petrozavodsk State University, Petrozavodsk, Russia
Article Tools
Follow on us
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%.
Keywords
The Theory of Vortex Gravitation, Space Flights with an Optimum Trajectory
To cite this article
Sergey Orlov, On Optimal Trajectory in Space Flight, American Journal of Aerospace Engineering. Vol. 3, No. 2, 2016, pp. 6-12. doi: 10.11648/j.ajae.20160302.11
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.
ADDRESS
Science Publishing Group
1 Rockefeller Plaza,
10th and 11th Floors,
New York, NY 10020
U.S.A.
Tel: (001)347-983-5186