Author Details

Делков, Александр Викторович

Issue	Section	Title	File
Vol 15, No 4 (2014)	Articles	Comparison of direct and reverse cycle of the thermal control system for the non-hermetic spacecrafts	(Rus)
Vol 15, No 1 (2014)	Articles	The problem of increasing the sensitivity of local control methods for tightness products of rocket and space technology	(Rus)
Vol 13, No 5 (2012)	Articles	DESIGN OPTIMIZATION OF THERMO-TECHNICAL SYSTEMS OPERATING IN A CLOSED CIRCUIT	(Rus)
Vol 24, No 1 (2023)	Section 2. Aviation and Space Technology	Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW	(Rus)
Vol 22, No 2 (2021)	Section 3. Technological Processes and Materials	Conversion use of models of working processes of rocket engine turbine installations in the application to local power engineering	(Rus) (Eng)
Vol 25, No 1 (2024)	Section 2. Aviation and Space Technology	Power engineering of the tangential supply device of the microturbine of the thermal control system of a promising spacecraft	(Rus) (Eng)
Vol 25, No 3 (2024)	Section 2. Aviation and Space Technology	Development of an experimental unit and methodology for ground-based experimental testing of two-phase thermoregulation systems for spacecrafts	(Rus) (Eng)