The article deals with the aerodynamic characteristics of model-driven warhead after its separation from the missile unit missile systems of volley fire. Aeroballistic calculated trajectory controlled head. Determine its maneuvering capabilities and the possible range for a given flight distance sighting range.
missile, rocket part, controlled head end, the aerodynamic coefficient, the stock wind resistance, flexibility, aeroballistic trajectory
"Otsinka manevrenykh mozhlyvostei modelnoi holovnoi chastyny, shcho upravliaietsia, pislia yii vidokremliuvannia v poloti vid reaktyvnoho snariada" [Estimation of possibilities the models jet - projectile with separated guided head trajectory correction],
Scientific Works of Kharkiv National Air Force University,