Massive destruction weapons processing

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 organisation 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 manoeuvres of execution to change the angle of incidence and 4 stabilisers 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.