Kharkiv National Air Force University
Command of the Air Force of Ukraine, Vinnytsia
The edition of guided aviation munitions (GAM), equipped a turbojet engine and aviation bomb is offered in the article.
The estimation of the expected mass, geometrical and aerodynamic performance characteristics of GAM is given. The calcula- tion of GAM flight trajectories on maximal distances are presented at the different motion parameters of aerial vehicles.
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