Author Details

Толстопятов, Михаил Игоревич

Issue	Section	Title	File
Vol 14, No 4 (2013)	Articles	HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE	(Rus)
Vol 13, No 5 (2012)	Articles	ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER	(Rus)
Vol 24, No 2 (2023)	Section 2. Aviation and Space Technology	To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines	(Rus)
Vol 24, No 2 (2023)	Section 3. Technological Processes and Materials	Simulation model of the system for ensuring the intraclimatic characteristics of clean industrial premises of space industry enterprises	(Rus)
Vol 23, No 2 (2022)	Section 2. Aviation and Space Technology	Dynamics of the flow in the sections of the elements of the supply path of the turbopump unit of the LRE	(Rus)
Vol 23, No 3 (2022)	Section 2. Aviation and Space Technology	Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines	(Rus)
Vol 25, No 4 (2024)	Section 2. Aviation and Space Technology	Dynamic flow parameters in natural curvilinear coordinates for a current line in a rotating channel	(Rus) (Eng)
Vol 26, No 1 (2025)	Section 2. Aviation and Space Technology	Design and testing of injectors manufactured using additive technologies for a low-thrust liquid rocket engine	(Rus) (Eng)