Experimental study on the ignition and combustion characteristics of TMEDA and WFNA in hypergolic fuel systems; Acta Astronautica; Vol. 236

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Parent link:Acta Astronautica.— .— Amsterdam: Elsevier Science Publishing Company Inc.
Vol. 236.— 2025.— P. 735-745
Další autoři: Vysokomornaya O. V. Olga Valeryevna, Pleshko Andrey Olegovich A. O., Paushkina K. K. Kristina Konstantinovna, Nadymova N. P. Nadezhda Pavlovna, Nigay A. G. Aleksandr Gerasimovich, Glushkov D. O. Dmitry Olegovich
Shrnutí:Title screen
An experimental study of the patterns and characteristics of ignition and combustion of hypergolic fuels with liquid components has been carried out. The experiments used tetramethylethylenediamine C6H16N2 (fuel) and highly concentrated nitric acid HNO3 (oxidizer). The initial volume of fuel and oxidizer droplets was 10 μl. The height of the fuel droplet fall relative to the oxidizer droplet varied from 5 to 20 cm. During the experimental studies, the following characteristics were determined: ignition delay times, burnout areas, and flame temperatures. The characteristics of the components interaction were also recorded using the Schlieren method. When varying the height of the fuel droplet fall, the ignition delay times change in the range of 42.4–54.9 s, the average values of the burnout areas change from 0.42 to 7.59 cm3. Moreover, the greater the height of the fuel droplet fall onto an oxidizer droplet on a plate, the shorter the ignition delay times and the larger the burnout areas
Текстовый файл
AM_TPU_network
Jazyk:angličtina
Vydáno: 2025
Témata:
On-line přístup:https://doi.org/10.1016/j.actaastro.2025.07.046
Médium: Elektronický zdroj Kapitola
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=682910

MARC

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330 |a An experimental study of the patterns and characteristics of ignition and combustion of hypergolic fuels with liquid components has been carried out. The experiments used tetramethylethylenediamine C6H16N2 (fuel) and highly concentrated nitric acid HNO3 (oxidizer). The initial volume of fuel and oxidizer droplets was 10 μl. The height of the fuel droplet fall relative to the oxidizer droplet varied from 5 to 20 cm. During the experimental studies, the following characteristics were determined: ignition delay times, burnout areas, and flame temperatures. The characteristics of the components interaction were also recorded using the Schlieren method. When varying the height of the fuel droplet fall, the ignition delay times change in the range of 42.4–54.9 s, the average values of the burnout areas change from 0.42 to 7.59 cm3. Moreover, the greater the height of the fuel droplet fall onto an oxidizer droplet on a plate, the shorter the ignition delay times and the larger the burnout areas 
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610 1 |a Fuel 
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610 1 |a Ignition delay time 
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701 1 |a Vysokomornaya  |b O. V.  |c physicist  |c Associate Professor of Tomsk Polytechnic University, Candidate of Physical and Mathematical Sciences  |f 1984-  |g Olga Valeryevna  |9 17501 
701 1 |a Pleshko  |g Andrey Olegovich  |b A. O.  |f 1998-  |c specialist in the field of heat and power engineering and thermal engineering  |c Assistant of assistant of the department Tomsk Polytechnic University  |9 88770 
701 1 |a Paushkina  |b K. K.  |c specialist in the field of heat and power engineering  |c Engineer of Tomsk Polytechnic University, assistant  |f 1998-  |g Kristina Konstantinovna  |3 (RuTPU)RU\TPU\pers\33561  |9 22949 
701 1 |a Nadymova  |b N. P.  |g Nadezhda Pavlovna 
701 1 |a Nigay  |b A. G.  |c specialist in the field of informatics and computer technology  |c engineer of Tomsk Polytechnic University  |f 1992-  |g Aleksandr Gerasimovich  |9 20167 
701 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  |9 16419 
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