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Fizika Goreniya i Vzryva, 2002, Volume 38, Issue 1, Pages 92–104 (Mi fgv1944)  

This article is cited in 5 scientific papers (total in 5 papers)

Probe method for sampling solid-propellant combustion products at temperatures and pressures typical of a rocket combustion chamber

A. G. Tereshchenkoa, O. P. Korobeinicheva, P. A. Skovorodkob, A. A. Paletskya, E. N. Volkova

a Institute of Chemical Kinetics and Combustion, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
b S.S. Kutateladze Institute of Thermophysics, Siberian Division of the Russian Academy of Sciences
Citations (5)
Abstract: The paper describes a new probe method for determining the quantitative composition of solid-propellant combustion products at temperatures of 2500–3200 K and pressures of 4-8 MPa under conditions typical of rocket motor conditions. A two-step probe is described, which allows a sample to be frozen without passing through the main shocks inside the sampler. The gas dynamics and the kinetics of chemical reactions were simulated to asses the correctness of sampling. It is shown that during sampling from a flame, the relative change in concentrations for most of the stable components does not exceed 3%, and for H$_2$ and O$_2$, it does not exceed 12%. The method permits additional operations with a sample, in particular, separation of CO and N$_2$ with subsequent analysis on a time-of-flight mass spectrometer. The CO and CO$_2$ concentrations in the combustion products of the model composite solid propellant – ammonium dinitramide (ADN) with polycaprolactone ($p$CLN) – were determined at a pressure of 4 MPa.
Keywords: Combustion Chamber, Combustion Product, Probe Method, Main Shock, Additional Operation.
Received: 12.03.2001
English version:
Combustion, Explosion and Shock Waves, 2002, Volume 38, Issue 1, Pages 81–91
DOI: https://doi.org/10.1023/A:1014066219589
Bibliographic databases:
Document Type: Article
UDC: 542.42: 533.6.011
Language: Russian
Citation: A. G. Tereshchenko, O. P. Korobeinichev, P. A. Skovorodko, A. A. Paletsky, E. N. Volkov, “Probe method for sampling solid-propellant combustion products at temperatures and pressures typical of a rocket combustion chamber”, Fizika Goreniya i Vzryva, 38:1 (2002), 92–104; Combustion, Explosion and Shock Waves, 38:1 (2002), 81–91
Citation in format AMSBIB
\Bibitem{TerKorSko02}
\by A.~G.~Tereshchenko, O.~P.~Korobeinichev, P.~A.~Skovorodko, A.~A.~Paletsky, E.~N.~Volkov
\paper Probe method for sampling solid-propellant combustion products at temperatures and pressures typical of a rocket combustion chamber
\jour Fizika Goreniya i Vzryva
\yr 2002
\vol 38
\issue 1
\pages 92--104
\mathnet{http://mi.mathnet.ru/fgv1944}
\elib{https://elibrary.ru/item.asp?id=17262243}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2002
\vol 38
\issue 1
\pages 81--91
\crossref{https://doi.org/10.1023/A:1014066219589}
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  • https://www.mathnet.ru/eng/fgv/v38/i1/p92
  • This publication is cited in the following 5 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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