Author Details

Ryzhkov, V. V.

Issue Section Title File
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 PDF
(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 PDF
(Rus)
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 PDF
(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 PDF
(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 PDF
(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 PDF
(Rus)
Vol 17, No 3 (2018) AIRCRAFT AND SPACE ROCKET ENGINEERING Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines PDF
(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 PDF
(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 PDF
(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 PDF
(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 PDF
(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 PDF
(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 PDF
(Rus)

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies