TY  - JOUR
T1  - Hydrogen-Oxygen Rocket Engine Design Using CFD-Modeling
AU - Zubanov, Vasiliy AU - Egorychev, Vitaliy AU - Shabliy, Leonid 
JO  - Research Journal of Applied Sciences
VL  - 9
IS  - 10
SP  - 660
EP  - 663
PY  - 2014
DA  - 2001/08/19
SN  - 1815-932x
DO  - rjasci.2014.660.663
UR  - https://makhillpublications.co/view-article.php?doi=rjasci.2014.660.663
KW  - CFD-modeling
KW  -liquid-propellant rocket engine
KW  -burnout
KW  -calculation model
KW  -spacecraft
AB  - This study describes designing process of rocket engine with thrust 25 N for system of orientation and starting of spacecraft instead of prototype with defect of burnout chamber which was not fixed during of development tests. The new version of the engine has been designed and additional research with CFD-modeling has been performed to completely exclude burnout possibility.
ER  -