Development of the pilot seat rocket motor propulsive charge of improved performances
Vladimir Kapor,
Miloš Filipović,
Milorad Savković,
Ljupka Nenadović,
The research and development
results of a new double base propulsive charge of the pilot seat rocket motor
with improved performances is presented in this paper. The comparative analysis
of performances pointed out the significant advantages of this new propulsive
charge with respect to the reference one. The realized ballistic performances of
the new propulsive charge allow a steadier and safer operating phase with higher
degree of security of the pilot seat rocket motor in the considered temperature
interval.
Key words: pilot seat, catapult seat, rocket
motor, propulsive charge, double base rocket propellant.