By a known longitudinal scatter of terminal point of self-control phase of a missile, how to find out its intervals of initial altitude that is necessary to definite tactical and technical index, launch mode, combat use, is an inevitable problem to weapon system of a missile based on moving launch plate.

The initial trajectory numerical simulation of air launched missile;

Influence on initial trajectory of large electric power torpedo caused by battery activated outside tube;

Analysis of effects of torpedo′s weighing property on initial trajectory

Aerodynamic characteristics and initial ballistic interference on a missile by a helicopter s rotor down-wash in hovering;