DocumentCode
1895800
Title
The method of neutralization of propellant compartments of rockets and maneuvering spacecrafts after propellant damping out of tanks
Author
Rotova, Oksana G.
Author_Institution
Omsk State Tech. Univ., Russia
Volume
1
fYear
2003
fDate
6-6 July 2003
Firstpage
179
Abstract
The paper is devoted to the method of neutralization of propellant compartments of rockets and spacecrafts and the mathematical model of rocket fuel combustion process in two-dimensional turbulent flow is presented. For closure of the equation system the k-/spl epsi/ turbulence model is used.
Keywords
aerospace propulsion; combustion; flow simulation; rocket engines; turbulence; neutralization; propellant compartments; rocket fuel combustion process; rockets; spacecraft; two-dimensional turbulent flow;
fLanguage
English
Publisher
ieee
Conference_Titel
Science and Technology, 2003. Proceedings KORUS 2003. The 7th Korea-Russia International Symposium on
Conference_Location
Ulsan, South Korea
Print_ISBN
89-7868-617-6
Type
conf
Filename
1222432
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