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  5. Estimation of possibilities the models jet - projectile with separated guided head trajectory correction

Estimation of possibilities the models jet - projectile with separated guided head trajectory correction

A.A. Zhuravlev, Y.M. Osipov, S.V. Orlov
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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.
Keywords: missile, rocket part, controlled head end, the aerodynamic coefficient, the stock wind resistance, flexibility, aeroballistic trajectory
Reference:
Zhuravlov, O.O., Osipov, Yu.M. and Orlov, S.V. (2016), "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, Vol. 4(49), pp. 38-41.