Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design
American Journal of Aerospace Engineering
Volume 3, Issue 3, December 2016, Pages: 43-49
Received: Dec. 3, 2016;
Accepted: Dec. 22, 2016;
Published: Jan. 7, 2017
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Volodymyr Chumakov, Independent Scholar, Kharkiv, Ukraine
Oleksandr Stolarchuk, Independent Scholar, Kharkiv, Ukraine
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The results of the development of the deck-based takeoff-elevating platforms of electrodynamic launch system are given. The research results of electrodynamic railguns with pulsed-dynamic biasing of acceleration channel and their modifications are used as the basis for the development and design. Comparative characteristics of the developed systems EMALS criteria are shown.
Electromagnetic Aircraft Launch System, Coaxial Electrodynamic Railgun, Pulse-Dynamic Biasing System, Rotor, Traction Force
To cite this article
Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design, American Journal of Aerospace Engineering.
Vol. 3, No. 3,
2016, pp. 43-49.
Copyright © 2016 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/
) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
V. I. Chumakov, O. V. Stolarchuk, Railgun System with Pulse-Dynamic Biasing of the Muzzle, Proceedings of 16th International Symposium on Electromagnetic Launch Technology (EML 2012) Beijing, China, 15-19 May, 2012, p.854, DOI: 10.1109/EML.2012.6324994.
Volodymyr Chumakov, Oleksandr Stolarchuk. Hypersonic Electrodynamic Railguns with Pulse-Dynamic Biasing System. Engineering and Applied Sciences. Vol. 1, No. 3, 2016, pp. 59-65. doi: 10.11648/j.eas.20160103.13.
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Arsenal of XXI century, 2009, No. 1.
V. I. Chumakov, O. V. Stolarchuk. Simulation and Comparative Analysis of Electrodynamic Railguns for Large Masses Acceleration, to be published.