Propellants' combustion tests with laboratory rocket motor and ballistic pendulum method

摘要

This paper presents new research methodology of propellants for evaluate their effectiveness for treatments associated with the intensification of oil and gas. Ballistic pendulum method is the traditional measurement of the work ability of explosives. In turn, for propellants properties testing laboratory rocket motor method is known. Using laboratory rocket motor installed in a mortar ballistic pendulum, the energetic parameters (eg., maximum pressure of the gaseous products, pressure impulse, burning rate, work ability) for selected propellants were determined.