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The original manuscript was received by the editors on 16.04.2013
Contributors
Kozlov A. A. —
D.Sc.(Eng.), Professor of Engineering, Department of Rocket Engines,
Moscow Aviation Institute (National Research University), specializes in the field of
processes in liquid-propellant low-thrust rocket engines.
Moscow Aviation Institute (National Research University), Volokolamskoye shosse 4,
Moscow, 125993 Russian Federation.
Bogacheva D. Yu. — Research Assistant, Department of Rocket Engines, Moscow Aviation
Institute (National Research University), specializes in the field of processes in liquid-
propellant low-thrust rocket engines.
Moscow Aviation Institute (National Research University), Volokolamskoye shosse 4,
Moscow, 125993 Russian Federation.
Borovik I.N. — Ph.D. (Eng.), Associate Professor, Department of Rocket Engines, Moscow
Aviation Institute (National Research University), specializes in the field of mathematical
simulation of working processes in low-thrust rocket engines.
Moscow Aviation Institute (National Research University), Volokolamskoye shosse 4,
Moscow, 125993 Russian Federation.
The translation of this article from Russian into English is done by I.R. Shafikova,
a senior lecturer, Linguistics Department, Bauman Moscow State Technical University
under the general editorship of N.N. Nikolaeva, Ph.D. (Philol.), Associate Professor,
Linguistics Department, Bauman Moscow State Technical University.
ISSN 0236-3941. HERALD of the BMSTU. Series “Mechanical Engineering”. 2014. No. 1 89