Author Details

Ryzhkov, V. V.

Issue	Section	Title	File
Vol 12, No 2 (2013)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block	(Rus)
Vol 13, No 5-2 (2014): Special Issue	ISSUE WITHOUT SECTION	Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants	(Rus)
Vol 13, No 5-3 (2014): Special Issue	ISSUE WITHOUT SECTION	Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel	(Rus)
Vol 15, No 4 (2016)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines	(Rus)
Vol 16, No 2 (2017)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines	(Rus)
Vol 17, No 3 (2018)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines	(Rus)
Vol 17, No 4 (2018)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft	(Rus)
Vol 18, No 2 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD	(Rus)
Vol 10, No 3-3 (2011): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Research of the possibility of thermal conditions LREST using an infrared thermal imaging system	(Rus)
Vol 18, No 3 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Сalculated analysis of the influence of operation and design factors on the parameters of oxygen-hydrogen low-thrust rocket engines	(Rus)
Vol 18, No 4 (2019)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems	(Rus)
Vol 20, No 4 (2021)	AIRCRAFT AND SPACE ROCKET ENGINEERING	The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies	(Rus)

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