@article{Kravchuk_Dmytro_Taranenko_Zirka_2021, title={Flight Range Extension of a Guided Aerial Bomb with a Rocket Engine during Climb Bombing}, volume={16}, url={https://www.aimt.cz/index.php/aimt/article/view/1462}, DOI={10.3849/aimt.01462}, abstractNote={<p>The possibility of a significant flight range extension of a guided aerial bomb during climb bombing due to the jet thrust created by a solid-propellant rocket engine was considered. By means of simulation, a comparative analysis of the range of a guided aerial bomb equipped (not equipped) with a solid-propellant rocket engine under typical flight conditions of the carrier aircraft during level flight and climb bombing was performed. It was demonstrated that the use of a solid-propellant rocket engine, whose mass is 20 % of the guided aerial bomb’s mass, allows to increase the horizontal range of its flight at least twice.</p> <p> </p>}, number={2}, journal={Advances in Military Technology}, author={Kravchuk, I.S. and Dmytro, Bashynskyi and Taranenko, V.V. and Zirka, M.V.}, year={2021}, month={Sep.}, pages={265–276} }