oscillations may have a negative influence on the unguided rocket firing precision, it is necessary to evaluate the exactly influence of the disturbance factors on the rocket movement upon the launcher. This study presents the equations of the rocket movement upon the launcher under the disturbance factors action, taking into consideration that the rocket is the integrated part of the rocket-la...

To better understand the characteristics of coupled heat transfer in liquid rocket engines, a calculation scheme is proposed this paper. This can simulate processes, including combustion and flow thrust chamber, radiation transfer, conduction wall, coolant cooling channel, gas film chamber wall. The numerical method used each physical area, data between computing module, strategy on coupling in...