Author Details

Морозов, И. И.

Issue	Section	Title	File
Vol 8, No 3-2 (2009): Special Issue	AIRCRAFT AND SPACE ROCKET ENGINEERING	Mathematical modelling and parametric research of flow of the twisted turbulent single-component stream of the propulsive mass in the trance- and supersonic areas of Laval nozzles	(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 17, No 3 (2018)	AIRCRAFT AND SPACE ROCKET ENGINEERING	Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines	(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 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)