Penetration of a cumulative jet of a pyrotechnic device into an obstacle of variable thicknes
. Penetration of a cumulative jet of a pyrotechnic device into an obstacle of variable thicknes. Space Science and Technology. 2025 ;31(2):02-02.
Space Energy, Power and Propulsion
Choice if gas-dynamic thrust vector control typr in ricket engine project developments
. Choice if gas-dynamic thrust vector control typr in ricket engine project developments. Space Science and Technology. 2025 ;31(2):01-01.
Assessment of the possibility of introducing a solid propellant accelerator P230 of the Ariane 5 rocket as a Helmholtz resonator
. Assessment of the possibility of introducing a solid propellant accelerator P230 of the Ariane 5 rocket as a Helmholtz resonator. Space Science and Technology. 2024 ;30(6):31-35.
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
. 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.
Determination of the optimum design of the means to ensure the fuel continuity by the method of numerical simulation
Determination of the optimum design of the means to ensure the fuel continuity by the method of numerical simulation. Космічна наука і технологія. 2024 ;30(3):40-52.
Version of loitering munitions classification based on the state-of-art and trends analysis
. Version of loitering munitions classification based on the state-of-art and trends analysis. Space Science and Technology. 2024 ;30(3):31-39.
Optimizing the design of a supersonic Planar Dual Bell Nozzle (PDBN)
. Optimizing the design of a supersonic Planar Dual Bell Nozzle (PDBN). Space Science and Technology. 2024 ;30(2):15-27.
Classification, main types of structures and purpose of capilary means to ensure fuel perfection
. Classification, main types of structures and purpose of capilary means to ensure fuel perfection. Space Science and Technology. 2024 ;30(1):14-30.
Research of supersonic flow in shortened nozzles of rocket engines with a bell-shaped tip
. Research of supersonic flow in shortened nozzles of rocket engines with a bell-shaped tip. Space Science and Technology. 2024 ;30(1):03-13.
Application of the test-particle statistical method for the simulation of rarefied plume in a vacuum
. Application of the test-particle statistical method for the simulation of rarefied plume in a vacuum. Space Science and Technology. 2023 ;29(4):012-023.