Ignition by laser radiation and combustion of composite solid propellants with bimetal powders; Journal of Physics: Conference Series; Vol. 830 : Energy Fluxes and Radiation Effects 2016

ग्रंथसूची विवरण
Parent link:Journal of Physics: Conference Series
Vol. 830 : Energy Fluxes and Radiation Effects 2016.— 2017.— [012137, 7 p.]
निगमित लेखक: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра атомных и тепловых электростанций (АТЭС)
अन्य लेखक: Korotkikh A. G. Aleksandr Gennadievich, Arkhipov V. A., Glotov O. G., Zolotorev N. N.
सारांश:Title screen
The use of metal powder (usually aluminum) as a fuel in composite solid propellants (CSPs) for propulsion is the most energy efficient method that allows improvement of combustion characteristics of propellants in the combustion chamber and specific impulse. This paper presents the experimental data of the ignition and combustion processes of CSPs containing Alex aluminum nanopowder and mixtures of Alex/Fe and Alex/B nanopowders. It was found that the introduction of Alex/Fe in CSPs leads to 1.3–1.9 times decrease in the ignition time at q=55–220 W/cm{2} and to 1.3–1.4 times increase in the burning rate at p=2.2–7.5 MPa with respect to that for basic CSP with Alex. When introducing Alex/B in CSP, the ignition times are 1.2–1.4 fold decreased, and the burning rate is practically unchanged. However, the agglomeration is significantly enhanced, which is manifested through the increase in the agglomerate particles content in condensed combustion products by a factor of 1.8–2.2, at 1.6–1.7 fold increase of the agglomerates mean diameter for CSP with Alex/B.
भाषा:अंग्रेज़ी
प्रकाशित: 2017
श्रृंखला:Radiation physics and chemistry of condensed matter
विषय:
ऑनलाइन पहुंच:http://dx.doi.org/10.1088/1742-6596/830/1/012137
http://earchive.tpu.ru/handle/11683/39509
स्वरूप: MixedMaterials इलेक्ट्रोनिक पुस्तक अध्याय
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=654954

MARC

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200 1 |a Ignition by laser radiation and combustion of composite solid propellants with bimetal powders  |f A. G. Korotkikh [et al.] 
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330 |a The use of metal powder (usually aluminum) as a fuel in composite solid propellants (CSPs) for propulsion is the most energy efficient method that allows improvement of combustion characteristics of propellants in the combustion chamber and specific impulse. This paper presents the experimental data of the ignition and combustion processes of CSPs containing Alex aluminum nanopowder and mixtures of Alex/Fe and Alex/B nanopowders. It was found that the introduction of Alex/Fe in CSPs leads to 1.3–1.9 times decrease in the ignition time at q=55–220 W/cm{2} and to 1.3–1.4 times increase in the burning rate at p=2.2–7.5 MPa with respect to that for basic CSP with Alex. When introducing Alex/B in CSP, the ignition times are 1.2–1.4 fold decreased, and the burning rate is practically unchanged. However, the agglomeration is significantly enhanced, which is manifested through the increase in the agglomerate particles content in condensed combustion products by a factor of 1.8–2.2, at 1.6–1.7 fold increase of the agglomerates mean diameter for CSP with Alex/B. 
461 0 |0 (RuTPU)RU\TPU\network\3526  |t Journal of Physics: Conference Series 
463 0 |0 (RuTPU)RU\TPU\network\20593  |t Vol. 830 : Energy Fluxes and Radiation Effects 2016  |o 5th International Congress, 2–7 October 2016, Tomsk, Russian Federation  |o [materials]  |f National Research Tomsk Polytechnic University (TPU) ; eds. M. V. Trigub G. E. Osokin ; A. S. Konovod  |v [012137, 7 p.]  |d 2017 
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