Wpływ warunków zrzutu na ruch zasobnika w pobliżu nosiciela i parametry upadku

Peculiar feature of the container flight, dropped from the subsonic aircraft were studied. Container dynamics at the dropping point as well as influence of the initial conditions on the flight parameters near the impact point were evaluated. Container was considered as a rigid object having six degrees of freedom. Exemplary numerical calculations were performed. It was found that the small divergence from the assumed dropping conditions lead to the significant deviation of the impact point.