This paper presents aerohydrodynamic modeling of air and surface pollution caused by toxic rocket fuel components. A numerical algorithm for solving this problem was developed and implemented in a software code in FORTRAN. Modeling of the dissimilation of rocket fuel dynamics for the case of the second-stage rocket "Proton-M" emergency fall was carried out using the developed software package. Finally, the modeling results were compared with a map of vegetation cover contamination in the region of the carrier-rocket second-stage fall.
| Published in | Applied and Computational Mathematics (Volume 2, Issue 3) |
| DOI | 10.11648/j.acm.20130203.14 |
| Page(s) | 92-95 |
| 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), 2013. Published by Science Publishing Group |
Aerohydrodynamic Modeling, Rocket Fuel Components, Heptyl, Environmental Investigation
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APA Style
Zhumagulov Bakhytzhan, Abdibekov Ualikhan, Karzhaubayev Kairzhan, Khikmetov Askar, Zhubat Kuanysch. (2013). Assessment of Earth Surface Pollution due to Residual Rocket Fuel. Applied and Computational Mathematics, 2(3), 92-95. https://doi.org/10.11648/j.acm.20130203.14
ACS Style
Zhumagulov Bakhytzhan; Abdibekov Ualikhan; Karzhaubayev Kairzhan; Khikmetov Askar; Zhubat Kuanysch. Assessment of Earth Surface Pollution due to Residual Rocket Fuel. Appl. Comput. Math. 2013, 2(3), 92-95. doi: 10.11648/j.acm.20130203.14
AMA Style
Zhumagulov Bakhytzhan, Abdibekov Ualikhan, Karzhaubayev Kairzhan, Khikmetov Askar, Zhubat Kuanysch. Assessment of Earth Surface Pollution due to Residual Rocket Fuel. Appl Comput Math. 2013;2(3):92-95. doi: 10.11648/j.acm.20130203.14
@article{10.11648/j.acm.20130203.14,
author = {Zhumagulov Bakhytzhan and Abdibekov Ualikhan and Karzhaubayev Kairzhan and Khikmetov Askar and Zhubat Kuanysch},
title = {Assessment of Earth Surface Pollution due to Residual Rocket Fuel},
journal = {Applied and Computational Mathematics},
volume = {2},
number = {3},
pages = {92-95},
doi = {10.11648/j.acm.20130203.14},
url = {https://doi.org/10.11648/j.acm.20130203.14},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.acm.20130203.14},
abstract = {This paper presents aerohydrodynamic modeling of air and surface pollution caused by toxic rocket fuel components. A numerical algorithm for solving this problem was developed and implemented in a software code in FORTRAN. Modeling of the dissimilation of rocket fuel dynamics for the case of the second-stage rocket "Proton-M" emergency fall was carried out using the developed software package. Finally, the modeling results were compared with a map of vegetation cover contamination in the region of the carrier-rocket second-stage fall.},
year = {2013}
}
TY - JOUR T1 - Assessment of Earth Surface Pollution due to Residual Rocket Fuel AU - Zhumagulov Bakhytzhan AU - Abdibekov Ualikhan AU - Karzhaubayev Kairzhan AU - Khikmetov Askar AU - Zhubat Kuanysch Y1 - 2013/07/20 PY - 2013 N1 - https://doi.org/10.11648/j.acm.20130203.14 DO - 10.11648/j.acm.20130203.14 T2 - Applied and Computational Mathematics JF - Applied and Computational Mathematics JO - Applied and Computational Mathematics SP - 92 EP - 95 PB - Science Publishing Group SN - 2328-5613 UR - https://doi.org/10.11648/j.acm.20130203.14 AB - This paper presents aerohydrodynamic modeling of air and surface pollution caused by toxic rocket fuel components. A numerical algorithm for solving this problem was developed and implemented in a software code in FORTRAN. Modeling of the dissimilation of rocket fuel dynamics for the case of the second-stage rocket "Proton-M" emergency fall was carried out using the developed software package. Finally, the modeling results were compared with a map of vegetation cover contamination in the region of the carrier-rocket second-stage fall. VL - 2 IS - 3 ER -