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...

The thrust produced by a hybrid rocket motor (HRM) can be controlled varying the oxidizer flow rate to combustion chamber. This feature is useful in shaping profiles and optimizing vehicle flight trajectory, but propellant throttling solid-fuel hybrids limited liquid component only, complicating control scheme potentially destabilizing motor. While ability remains subject of considerable intere...

Hybrid rockets have many advantages over pure solid or liquid propellant rockets, but low fuel regression rates and correspondingly thrust hindered their application to operational systems. Paraffin-based fuels regress significantly faster than traditional polymeric formulations, such as HTPB, paraffin inclusion in HTPB represents a potential tool for performance augmentation hybrid rockets. A ...