Hybrid electromagnetic launcher with pneumatic assist - influence of input supply data upon final velocity missile

摘要

The purpose of this paper is to present simplified graphical representation of the missile velocity for the hybrid electromagnetic launcher with pneumatic assist. The presented simplified graphical method is oriented at describing clearly influence of supply data upon velocity of the missile in the form of the so-called control strategy trees in consecutive modules of the hybrid launcher: air-gun, coil-gun and rail-gun.