earticle

영어

This work describes the flight trajectory characteristics of various ballistic missiles. The characteristics mainly depend on the range of the missile. There are four ways of adjusting the missile range: payload, specific impulse, loft angle changes, and fuel control. The operators of ballistic missiles can select one of these options. From this viewpoint, this work presents the flight trajectory characteristics of ballistic missiles depending on the operational parameters. The characteristics analysis algorithm that was used in this paper was the same as that used by the authors in their earlier paper.