Development of a mathematical model for the process of rocket fuel bubbling with liquid nitrogen
To achieve an optimum temperature of rocket fuel, its negative temperature and the amount of its purification from impurities are necessary. For this purpose, a mathematical model of the temperature dependence inside the bubbler has been developed in this article.
Vybornov N. A., ...
The choice of structural materials for thermo thruster on clean monopropellant
... Anflo K. Spacecraft system level design with regard to incorporation of a new green propulsion system // 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. P. 2011—6129.
Goza D., Nesterenko A., Rumyantsev A.
low-thrust liquid rocket engine; thermocatalytic thruster; environmentally clean monopropellant; green propellant; combustion chamber