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
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;
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
