Article information

2008 , Volume 13, ¹ 1, p.42-47

Gusachenko L.K., Miloshevic H., Rychkov A.D., Shokin Y.I.

Modeling of sold-propellant rocket microengines

Numerical modeling is used to investigate a domain of stable operation of solid-propellant rocket micro engines, which are used in various control systems of spacecrafts. It was established that this domain differs significantly from the on of the mid-flight engines.

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Author(s):
Gusachenko L.K.
Address: Russia, Novosibirsk
E-mail: gusachen@kinetics.nsc.ru

Miloshevic Hranislav
Dr. , Professor
Office: Faculty of natural science and mathematics
Address: 38220, Serbia, Kosovska Mitrovica, I.L. Ribar bb
Phone Office: (38111) 2146464
E-mail: ytlad@eunet.rs

Rychkov Aleksandr Dmitrievich
Dr. , Professor
Position: Leading research officer
Address: 63009, Russia, Novosibirsk, I.L. Ribar bb
Phone Office: (383) 330 86 56
E-mail: rych@ict.nsc.ru

Shokin Yuriy Ivanovich
Dr. , Academician RAS, Professor
Position: Scientific Director of the Institute
Office: Federal Research Center for Information and Computational Technologies
Address: 630090, Russia, Novosibirsk, Ac. Lavrentiev ave., 6
Phone Office: (383) 334 91 10
E-mail: shokin@ict.nsc.ru
SPIN-code: 6442-4180


Bibliography link:
Gusachenko L.K., Miloshevic H., Rychkov A.D., Shokin Y.I. Modeling of sold-propellant rocket microengines // Computational technologies. 2008. V. 13. ¹ 1. P. 42-47
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