Optimum Disposition of Metal Particles in the Propellant Grain
Using the dispersed metal in solid propellants to increase the temperature of combustion products leads to such a problem as the specific impulse loss due to the incomplete combustion of metal particles in the exhaust products. A redistribution of metal loaded into the propellant grain is one of the...
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Format: | Article |
Language: | English |
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Wiley
2014-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2014/958758 |
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author | Leonid L. Minkov Ernst R. Shrager Elizaveta V. Pikushchak |
author_facet | Leonid L. Minkov Ernst R. Shrager Elizaveta V. Pikushchak |
author_sort | Leonid L. Minkov |
collection | DOAJ |
description | Using the dispersed metal in solid propellants to increase the temperature of combustion products leads to such a problem as the specific impulse loss due to the incomplete combustion of metal particles in the exhaust products. A redistribution of metal loaded into the propellant grain is one of the methods to decrease the specific impulse loss. This paper reports on the ways to obtain the optimum metal particle disposition for the case-bounded propellant grain of tube cross-sectional type. Three different approaches to analyze the metal combustion efficiency are discussed. The influence of the dynamic nonequilibrium of two-phase flow on the optimum metal particles disposition in the propellant grain of tube cross-sectional type is investigated. |
format | Article |
id | doaj-art-65074978c5e0492d90849a882d522dd1 |
institution | Kabale University |
issn | 1687-5966 1687-5974 |
language | English |
publishDate | 2014-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
spelling | doaj-art-65074978c5e0492d90849a882d522dd12025-02-03T07:24:45ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742014-01-01201410.1155/2014/958758958758Optimum Disposition of Metal Particles in the Propellant GrainLeonid L. Minkov0Ernst R. Shrager1Elizaveta V. Pikushchak2Department of Physics and Engineering, Tomsk State University, 36 Lenin Avenue, Tomsk 634050, RussiaDepartment of Physics and Engineering, Tomsk State University, 36 Lenin Avenue, Tomsk 634050, RussiaDepartment of Physics and Engineering, Tomsk State University, 36 Lenin Avenue, Tomsk 634050, RussiaUsing the dispersed metal in solid propellants to increase the temperature of combustion products leads to such a problem as the specific impulse loss due to the incomplete combustion of metal particles in the exhaust products. A redistribution of metal loaded into the propellant grain is one of the methods to decrease the specific impulse loss. This paper reports on the ways to obtain the optimum metal particle disposition for the case-bounded propellant grain of tube cross-sectional type. Three different approaches to analyze the metal combustion efficiency are discussed. The influence of the dynamic nonequilibrium of two-phase flow on the optimum metal particles disposition in the propellant grain of tube cross-sectional type is investigated.http://dx.doi.org/10.1155/2014/958758 |
spellingShingle | Leonid L. Minkov Ernst R. Shrager Elizaveta V. Pikushchak Optimum Disposition of Metal Particles in the Propellant Grain International Journal of Aerospace Engineering |
title | Optimum Disposition of Metal Particles in the Propellant Grain |
title_full | Optimum Disposition of Metal Particles in the Propellant Grain |
title_fullStr | Optimum Disposition of Metal Particles in the Propellant Grain |
title_full_unstemmed | Optimum Disposition of Metal Particles in the Propellant Grain |
title_short | Optimum Disposition of Metal Particles in the Propellant Grain |
title_sort | optimum disposition of metal particles in the propellant grain |
url | http://dx.doi.org/10.1155/2014/958758 |
work_keys_str_mv | AT leonidlminkov optimumdispositionofmetalparticlesinthepropellantgrain AT ernstrshrager optimumdispositionofmetalparticlesinthepropellantgrain AT elizavetavpikushchak optimumdispositionofmetalparticlesinthepropellantgrain |