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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Main Authors: Leonid L. Minkov, Ernst R. Shrager, Elizaveta V. Pikushchak
Format: Article
Language:English
Published: Wiley 2014-01-01
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
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institution Kabale University
issn 1687-5966
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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