Designing and developing a atomic ballistic missile flight depends on the mission and the stress to which the missile is subject. Missile’s requests are
determined by: the organization of components; flight regime type,
engine configuration and aerodynamic performance of the rocket
flight. In this paper has been developed a ballistic missile with a
smooth fuselage type, 10 control surfaces, 8 directional surfaces for
cornering execution, 2 for maneuvers of execution to change the angle
of incidence and 4 stabilizers direction. Through the technology of
gluing and clamping of the shell and the use of titanium components,
mass of ballistic missile presented a significant decrease in weight
and a structure with high strength.