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. Choice if gas-dynamic thrust vector control typr in ricket engine project developments. Space Science and Technology. 2025 ;31(2):03-11.
. The influence of the entrance angle to the bell-shaped tip of a shortened round supersonic nozzle of a rocket engine on its impulse characteristics. Space Science and Technology. 2024 ;30(3):53-60.
. Research of supersonic flow in shortened nozzles of rocket engines with a bell-shaped tip. Space Science and Technology. 2024 ;30(1):03-13.

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