Author Details
Боровик, И. Н., Московский авиационный институт (национальный исследовательский университет), Russian Federation
| Issue | Section | Title | File |
| Vol 13, No 1 (2014) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling |
 (Rus) |
| Vol 13, No 1 (2014) | AIRCRAFT AND SPACE ROCKET ENGINEERING | Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets |
(Rus) |