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The goals of this research are to test the relationships of appropriate nonline of site (NLOS) missile flight performances and conditionally created their tactical ranges, spaces zones and shooting time during employment on the surface targets. Flight maneuver of distance remote controlled NLOS missile is tested with the conditionally joint constrains coming from flight kinematics with turbo-jet engine of NLOS missile and manner of target motion, typical of rapid reaction attacks. The constraints of maneuverability and flight, in the cruise phase, are considered as the mass point motion to create both unguided (searching) and guided navigated kinematical trajectories, which was designed by the appropriate guidance law. Research used numerical methods to simulate NLOS missile and targets motions in horizontal plane by controlling line of target (LOT) referred at the appropriate flight height. This generates borders of target impact and launching areas, establishes NLOS missile operation time, as well as masses variations for the expected manner of battle flight. .

Engagement areas of missiles in the proportional navigated flight powered by air breathing engines