Effect of the thermophysical properties of the material of a local energy source on conditions and characteristics of ignition of metallized composite propellants; Russian Journal of Physical Chemistry B; Vol. 10, iss. 6

Detalhes bibliográficos
Parent link:Russian Journal of Physical Chemistry B: scientific journal.— , 1982-
Vol. 10, iss. 6.— 2016.— [P. 946–952]
Autor principal: Glushkov D. O. Dmitry Olegovich
Autor Corporativo: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
Outros Autores: Kuznetsov G. V. Geny Vladimirovich, Strizhak P. A. Pavel Alexandrovich
Resumo:Title screen
Solid-phase ignition of metallized composite propellants by a single particle heated to a high temperature under conditions of an ideal thermal contact has been numerically studied. The effect of the thermophysical properties of the material of a local energy source on the conditions and characteristics of ignition of composite propellants has been analyzed. It has been found that sources with a high heat storage capacity exhibit shorter ignition delay times for metallized propellants (by 10-60%) and lower initial temperatures required to initiate the combustion process (by 170 K). In addition, it has been found that the presence of particles of metals (boron, aluminum, magnesium, lithium) in the propellant composition leads to an increase in the effective thermal conductivity of the propellant. The cumulative effect of the thermophysical properties of the materials of the “particle heated to a high temperature-metallized composite propellant” system leads to an increase in the ignition delay times (by 25-65%) and the heat penetration depth of the near-surface layer of the propellant (by 25-40%) at the time of combustion initiation compared with metal-free compounds.
Режим доступа: по договору с организацией-держателем ресурса
Idioma:inglês
Publicado em: 2016
Assuntos:
Acesso em linha:http://dx.doi.org/10.1134/S1990793116060208
Formato: Recurso Electrónico Capítulo de Livro
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=653763

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200 1 |a Effect of the thermophysical properties of the material of a local energy source on conditions and characteristics of ignition of metallized composite propellants  |f D. O. Glushkov, G. V. Kuznetsov, P. A. Strizhak 
203 |a Text  |c electronic 
300 |a Title screen 
320 |a [References: p. 951-952 (35 tit.)] 
330 |a Solid-phase ignition of metallized composite propellants by a single particle heated to a high temperature under conditions of an ideal thermal contact has been numerically studied. The effect of the thermophysical properties of the material of a local energy source on the conditions and characteristics of ignition of composite propellants has been analyzed. It has been found that sources with a high heat storage capacity exhibit shorter ignition delay times for metallized propellants (by 10-60%) and lower initial temperatures required to initiate the combustion process (by 170 K). In addition, it has been found that the presence of particles of metals (boron, aluminum, magnesium, lithium) in the propellant composition leads to an increase in the effective thermal conductivity of the propellant. The cumulative effect of the thermophysical properties of the materials of the “particle heated to a high temperature-metallized composite propellant” system leads to an increase in the ignition delay times (by 25-65%) and the heat penetration depth of the near-surface layer of the propellant (by 25-40%) at the time of combustion initiation compared with metal-free compounds. 
333 |a Режим доступа: по договору с организацией-держателем ресурса 
461 |t Russian Journal of Physical Chemistry B  |o scientific journal  |d 1982- 
463 |t Vol. 10, iss. 6  |v [P. 946–952]  |d 2016 
610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
610 1 |a ракетные двигатели 
610 1 |a источники энергии 
610 1 |a математическое моделирование 
610 1 |a теплофизические свойства 
610 1 |a ракетные топлива 
610 1 |a metallized composite solid propellant 
610 1 |a local energy source 
610 1 |a material of particles 
610 1 |a mathematical simulation 
610 1 |a ignition 
700 1 |a Glushkov  |b D. O.  |c specialist in the field of power engineering  |c Professor, Director of the ISHFVP of the Tomsk Polytechnic University, Doctor of Technical Sciences  |f 1988-  |g Dmitry Olegovich  |3 (RuTPU)RU\TPU\pers\32471  |9 16419 
701 1 |a Kuznetsov  |b G. V.  |c Specialist in the field of heat power energy  |c Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences  |f 1949-  |g Geny Vladimirovich  |3 (RuTPU)RU\TPU\pers\31891  |9 15963 
701 1 |a Strizhak  |b P. A.  |c Specialist in the field of heat power energy  |c Doctor of Physical and Mathematical Sciences (DSc), Professor of Tomsk Polytechnic University (TPU)  |f 1985-  |g Pavel Alexandrovich  |3 (RuTPU)RU\TPU\pers\30871  |9 15117 
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