Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design

Volodymyr Chumakov; Oleksandr Stolarchuk

doi:doi:10.11648/j.ajae.20160303.14

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Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design

Volodymyr Chumakov, Oleksandr Stolarchuk

Published in American Journal of Aerospace Engineering (Volume 3, Issue 3)

Received: 3 December 2016 Accepted: 22 December 2016 Published: 7 January 2017

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Abstract

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.

Published in	American Journal of Aerospace Engineering (Volume 3, Issue 3)
DOI	10.11648/j.ajae.20160303.14
Page(s)	43-49
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), 2017. Published by Science Publishing Group

Keywords

Electromagnetic Aircraft Launch System, Coaxial Electrodynamic Railgun, Pulse-Dynamic Biasing System, Rotor, Traction Force

References

[1]	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.
[2]	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.
[3]	V. I. Chumakov, O. V. Stolarchuk, Pulse processes and systems: Manual for laboratory works, Sevastopol, Naval Academy by of P. S. Nakhimov, 2012, 70 p.
[4]	V. I. Chumakov, O. V. Stolarchuk, Evaluating the effectiveness of the railgun acceleration channel pulsed-dynamic biasing, Proceedings of Naval Academy by of P. S. Nakhimov, 2012, 1 (5), pp.135-144.
[5]	Arsenal of XXI century, 2009, No. 1.
[6]	http://army-news.ru/2014/04/rossiya-nachala-razrabotku-elektromagnitnoj-katapulty/.
[7]	https://lenta.ru/news/2016/11/09/emals/.
[8]	http://argumentiru.com/army/2016/04/426383.
[9]	V. I. Chumakov, O. V. Stolarchuk. Simulation and Comparative Analysis of Electrodynamic Railguns for Large Masses Acceleration, to be published.
[10]	http://ewh.ieee.org/soc/emcs/acstrial/newsletters/spring07/EMCSsupplement.pdf.
[11]	http://www.keybridgeti.com/videotraining/manualdl/25835.PDF.
[12]	http://www.caterpillar.com/.

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APA Style

Volodymyr Chumakov, Oleksandr Stolarchuk. (2017). Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. American Journal of Aerospace Engineering, 3(3), 43-49. https://doi.org/10.11648/j.ajae.20160303.14

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ACS Style

Volodymyr Chumakov; Oleksandr Stolarchuk. Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. Am. J. Aerosp. Eng. 2017, 3(3), 43-49. doi: 10.11648/j.ajae.20160303.14

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AMA Style

Volodymyr Chumakov, Oleksandr Stolarchuk. Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. Am J Aerosp Eng. 2017;3(3):43-49. doi: 10.11648/j.ajae.20160303.14

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@article{10.11648/j.ajae.20160303.14,
  author = {Volodymyr Chumakov and Oleksandr Stolarchuk},
  title = {Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design},
  journal = {American Journal of Aerospace Engineering},
  volume = {3},
  number = {3},
  pages = {43-49},
  doi = {10.11648/j.ajae.20160303.14},
  url = {https://doi.org/10.11648/j.ajae.20160303.14},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20160303.14},
  abstract = {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.},
 year = {2017}
}

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TY  - JOUR
T1  - Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design
AU  - Volodymyr Chumakov
AU  - Oleksandr Stolarchuk
Y1  - 2017/01/07
PY  - 2017
N1  - https://doi.org/10.11648/j.ajae.20160303.14
DO  - 10.11648/j.ajae.20160303.14
T2  - American Journal of Aerospace Engineering
JF  - American Journal of Aerospace Engineering
JO  - American Journal of Aerospace Engineering
SP  - 43
EP  - 49
PB  - Science Publishing Group
SN  - 2376-4821
UR  - https://doi.org/10.11648/j.ajae.20160303.14
AB  - 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.
VL  - 3
IS  - 3
ER  -

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Author Information

Volodymyr Chumakov

Independent Scholar, Kharkiv, Ukraine
Oleksandr Stolarchuk

Independent Scholar, Kharkiv, Ukraine

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APA Style

Volodymyr Chumakov, Oleksandr Stolarchuk. (2017). Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. American Journal of Aerospace Engineering, 3(3), 43-49. https://doi.org/10.11648/j.ajae.20160303.14

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ACS Style

Volodymyr Chumakov; Oleksandr Stolarchuk. Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. Am. J. Aerosp. Eng. 2017, 3(3), 43-49. doi: 10.11648/j.ajae.20160303.14

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AMA Style

Volodymyr Chumakov, Oleksandr Stolarchuk. Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design. Am J Aerosp Eng. 2017;3(3):43-49. doi: 10.11648/j.ajae.20160303.14

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@article{10.11648/j.ajae.20160303.14,
  author = {Volodymyr Chumakov and Oleksandr Stolarchuk},
  title = {Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design},
  journal = {American Journal of Aerospace Engineering},
  volume = {3},
  number = {3},
  pages = {43-49},
  doi = {10.11648/j.ajae.20160303.14},
  url = {https://doi.org/10.11648/j.ajae.20160303.14},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20160303.14},
  abstract = {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.},
 year = {2017}
}

Copy | Download

TY  - JOUR
T1  - Electrodynamic Launch System Takeoff-Elevating Platforms for Deck-Based Aircraft Carriers Concept Development and Design
AU  - Volodymyr Chumakov
AU  - Oleksandr Stolarchuk
Y1  - 2017/01/07
PY  - 2017
N1  - https://doi.org/10.11648/j.ajae.20160303.14
DO  - 10.11648/j.ajae.20160303.14
T2  - American Journal of Aerospace Engineering
JF  - American Journal of Aerospace Engineering
JO  - American Journal of Aerospace Engineering
SP  - 43
EP  - 49
PB  - Science Publishing Group
SN  - 2376-4821
UR  - https://doi.org/10.11648/j.ajae.20160303.14
AB  - 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.
VL  - 3
IS  - 3
ER  -

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